Page 1: ...AS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN REVISION 3 TO THE BASIC MANUAL INCORPORATES TEMPORARY REVISION 1 DATED 3 OCTOBER 1994 COPYRIGHT 1996 CESSNA AIRCRAFT COMPANY WICHITA KANSAS USA D2068 3 13 REVISION 3 2 JANUARY 1996 RGI 100 5 01 ...
Page 2: ...ystem operational test FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 1 For Paper Publications file this cover sheet behind the publication s title page to identify the inclusion of the Temporary Revision into the manual Insert the new pages into the publication at the appropriate locations and remove and discard the superseded pages 2 For Aerofiche Publications draw a line with permanent red ink...
Page 3: ...with corrugated skins FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications File this cover sheet behind the publication s title page to identify the inclusion of the Temporary Revision into the manual Insert the new pages into the publication at the appropriate locations Draw a line with a permanent red ink marker through any superceded information For Aerofiche Publications Draw...
Page 4: ...ru 3 25 1 ii thru iv 3 3 26 thru 3 28 0 1 1 3 4 1 1 1 2 thru 1 3 0 4 2 thru 4 3 0 1 4 thru 1 14 1 4 4 thru 4 8 1 1 15 2 5 1 thru 5 2 1 1 16 3 5 3 0 1 17 thru 1 21 2 5 4 thru 5 5 1 1 22 Blank 2 5 6 0 2 1 3 5 7 thru 5 9 1 2 2 thru 2 3 0 5 10 thru 5 12 0 2 4 thru 2 7 1 5 12A 1 2 8 3 5 12B Blank 1 2 9 thru 2 14 1 5 13 thru 5 16 0 2 15 thru 2 18 0 5 17 1 2 19 thru 2 20 1 5 18 thru 5 25 0 2 21 thru 2 23...
Page 5: ... 34 Blank 0 14 34 Blank 0 11A 1 thru 11A 2 1 15 1 3 11A 3thru 11A 0 0 15 2 thru 5 14 0 11A 11 15 14Athru 0 11A 12thru 11A 15 15 14B Blank 0 11A 16 15 15 thru 15 17 0 11A 1thru A 1518 11A 19 1 15 18A thru 15 18C 0 11A 20 15 18D 11A 21 15 19 thru 15 19 0 11A 22 thru 11A 25 0 15 20 thru 15 21 3 11A 26 Blank 15 02 12 1 12 2 thru 12 6 0 12 7 thru 12 82 2 15 24A thru 15 24 12 9 thru 12 10 12 11 15 28 0 ...
Page 6: ...8 6A thru 18 6D 0 20 94B Blank 0 18 7 thru 18 12 0 20 95 thru 20 98 0 18 12A 0 20 98A 0 18 12B Blank 0 20 98B Blank 0 18 13 thru 18 35 0 20 99 thru 20 128 0 18 36 Blank 0 20 128A 0 19 1 1 20 128B Blank 0 19 2 thru 19 6 0 20 129 thru 20 140 0 20 1 thru 20 2 3 20 140A thru 20 140C 0 20 3 thru 20 82 0 20 140D Blank 0 20 82A 0 20 141 thru 20 143 0 20 82B Blank 0 20 144 0 C Revision 3 ...
Page 7: ...BOCHARGED 2B19 11A 1 12 FUEL SYSTEM 2D1 12 1 13 PROPELLERS AND PROPELLER GOVERNORS 2E13 13 1 14 UTILITY SYSTEMS 2F3 14 1 15 INSTRUMENTS AND INSTRUMENT SYSTEMS 2G19 15 1 16 ELECTRICAL SYSTEMS 2I9 16 1 17 ELECTRONIC SYSTEMS DELETED 18 STRUCTURAL REPAIR 3A3 18 1 19 PAINTING 3C3 19 1 20 WIRING DIAGRAMS 3C15 20 1 WARNING When performing any inspection or maintenance that re quires turning on the master...
Page 8: ...er and serial number MODEL SERIAL POPULAR NAME YEAR MODEL BEGINNING ENDING SKYLANE 1977 182Q 18265176 18265965 SKYLANE II 1978 182Q 18263479 18265966 18266590 1979 182Q 18266591 18267300 1980 182Q 18267301 18267715 REIMS CESSNA 1977 F182P F18200026 F18200064 SKYLANE REIMS CESSNA SKYLANE II FSKYLANE 1978 F182Q F18200065 F18200094 F SKYLANE II 1979 F182Q F18200095 F18200129 1980 F182Q F18200130 F182...
Page 9: ...ervice information which may be reissued by Cessna thereby automatically amending this publication and is communicated to the field through Cessna s Authorized Service Stations and or through Cessna s subscription services WARNING ALL INSPECTION INTERVALS REPLACEMENT TIME LIMITS OVERHAUL TIME OMMENDED BY CESSNA ARE SOLELY BASED ON THE USE OF NEW REMANU FACTURED OR OVERHAULED CESSNA APPROVED PARTS ...
Page 10: ...re not in cluded in this manual When an STC installation is incorporated on the airplane those portions of the airplane affected by the installation must be inspected in accordance with the inspection program published by the owner of the STC Since STC installations may change systems interface operating characteristics and component loads or stresses on adjacent structures Cessna provided inspect...
Page 11: ...braced monoplanes of all metal bladed all metal constant speed McCauley propeller semimonocoque construction The aircraft are of conventional design consisting of five basic units 1 4 AIRCRAFT SPECIFICATIONS Leading par i e fuselage wing stabilizers flight control sur ticulars of these aircraft with dimensions based on faces and landing gear The landing gear is of con gross weight are given in fig...
Page 12: ...ure 49 psi NOSE GEAR STRUT PRESSURE Strut Extended 55 psi to 60 psi WHEEL ALIGNMENT Camber 5 to 7 Toe In 0 to 06 AILERON TRAVEL Up 20 2 Down 15 2 WING FLAP TRAVEL 0 to 40 1 2 THRU 1981 0 0 t o 3 8 0 1 1982 ON RUDDER TRAVEL Measured Parallel to Water Line Right 24 0 1 Left 24 0 1 RUDDER TRAVEL Measured Perpendicular to Hinge Line Right 27 13 0 1 Left 27 13 0 1 ELEVATOR TRAVEL Relative to Stabilizer...
Page 13: ...ING 39 00 9785 871 85 96 Il T9796 5r 100 56 7850 17 00 7 40 23 62 56 53 71 9785 87 100 s50 8 12 56 118 70 Figure 1 2 Refere s 136 00 154 00 STANDARI WI 172 0 190 00 19N7 8 208 00 0 00 124 00 156 00 185 50 209 00 45 A 1 I92 00 8 12 0 79 00 56 70 Figure 1 2 Reference Stations 1 3 ...
Page 14: ...applied b Screws attached to nutplates should be 1 Calibrate torque wrench periodically to assure tightened firmly but with no specific torque value accuracy and recheck frequently c Bolts nuts and screws used in control 2 When using a torque wrench adapter which systems and installations where required torque changes distance from torque wrench drive to adapter would cause binding or interfere wi...
Page 15: ...RENCH HANDGRIP ADAPTER DRIVE CENTERLINE CENTERLINE PREDETERMINED ADAPTER TORQUE CENTERLINE HOSE CLAMP ADAPTER EXAMPLE Y Unknown 10 1 5 11 5 E 1 5 In Y 117 In Lbs OPEN END WRENCH ADAPTER DRIVE CENTERLINE CENTERLINE PREDETERMINED WRENCH TORQUE DRIVE WRENCH CENTERLINE FLARE NUT WRENCH ADAPTER EXAMPLE SPANNER WRENCH ADAPTER T 135 In Lbs y 135 x 10 _ 1350 15882 Y Unknown L 10 0 In Lbs 10 1 5 8 5 E 1 5 ...
Page 16: ...50 500 270 300 1 2 20 770 950 450 550 12 20 480 690 290 410 9 16 18 1100 1300 650 800 916 18 800 1000 480 600 5 8 18 1250 1550 750 950 58 18 1100 1300 660 780 3 4 16 2650 3200 1600 1900 34 16 2300 2500 1300 1500 7 8 14 3550 4350 2100 2600 78 14 2500 3000 1500 1800 1 14 4500 5500 2700 3300 1 14 3700 4500 2200 3300 1 1 8 12 6000 7300 3600 4400 1 1 8 12 5000 7000 3000 4200 1 1 4 12 11000 13400 6600 8...
Page 17: ...OR nut are given in Table 1 3 TUBE JAM NUT CONNECTOR OUTSIDE THREAD DIAMETER w o JAM NUT Inches Torque Limits Torque Limits HOSE ALUMINUM STEEL 1 8 5 16 24 35 50 50 55 MIN MAX MIN MAX 3 16 3 8 24 65 80 65 20 30 75 85 1 4 7 16 20 85 105 95 1053 16 25 35 95 105 5 16 1 2 20 105 125 125 135 1 4 50 65 135 150 3 8 9 16 18 120 150 155 165 5 16 7 90 170 200 1 2 3 4 16 240 280 280 3053 8 110 130 270 300 5 ...
Page 18: ...ght Threaded Fittings Line 1 8 SAFETYING PROCEDURES The use of safety 2 Copper that is cadium plated and dyed yellow wire cotter pins lockwashers and self locking nuts is used for shear and seal wiring applications is to prevent relative movement of critical components a Shear applications are those where it is subject to vibration torque tension etc which could necessary to break or shear wire to...
Page 19: ...uld use double twist method of lockwiring e When locking is required on electrical connectors which use threaded coupling rings or 3 Lockwiring by the double twist method is on plugs which employ screws or rings to fasten really one wire twisted on itself several times and is individual parts of plug together they shall be accomplished by the following steps see Figure 1 lockwired with 0 020 inch ...
Page 20: ...IN CLOSELY SPACED CLOSED RIGHT HAND THREADED PARTS GEOMETRICAL PATTERN SINGLE WIRE METHOD SHOWN REVERSE DIRECTION FOR LEFT HAND THREADS SINGLE FASTENER APPLICATION CASTELLATED NUTS ON DRILLED STUDS DOUBLE TWIST METHOD DOUBLE TWIST METHOD Figure 1 4 Lockwire Safetying Sheet 1 of 2 1 10 Revision 1 ...
Page 21: ...gh bolt B Bend other end around bolt if necessary bend wire across head of bolt Twist wires counterclockwise 1 2 inch or six twists Clip ends Bend pigtail back againt part BOLT B CLOCKWISE DOUBLE TWIST METHOD COUNTERCLOCKWISE CLOCKWISE COUNTERCLOCKWISE CLOCKWISE MULTIPLE FASTENER APPLICATION DOUBLE TWIST METHOD bELECTRICAL CONNECTION DOUBLE TWIST METHOD Figure 1 4 Lockwire Safetying Sheet 2 of 2 R...
Page 22: ... Table 1 5 Cotter Pin 1 3 8 0 116 Temperature and Use 1 1 2 0 116 2 Cotter pins shall be new upon each applica tion 3 When nuts are to be secured to fastener with Table 1 6 Cotter Pin cotter pins tighten nut to low side minimum of Minimum Size applicable specified or selected torque range unless otherwise specified and if necessary continue tight 7 In pin applications install cotter pin with ening...
Page 23: ...TO PROVIDE CLEARANCE PRONG MAY BE CUT HERE PREFERRED METHOD ALTERNATE METHOD CASTELLATED NUT ON BOLT TANGENT TO PIN MAXIMUM MINIMUM COTTER PIN COTTER PIN LENGTH LENGTH PIN APPLICATION Figure 1 5 Installation of Cotter Pins Revision 1 1 13 ...
Page 24: ...ples are pulleys lev with fingers only ers linkages and cam followers NOTE NOTE Do not use tool as locking clip could be dis Self locking nuts can be used when threaded torted parts are held by a positive locking device that requires shearing or rupture before torsional 3 Locking clips are for one time use only and loads can act on threaded parts shall not be re used 4 Both locking clips may be in...
Page 25: ...MODEL 182 T182 SERIES SERVICE MANUAL LOCKING CUP BARREL BARREL LOCKING CLIP LOCKING CLIP CABLE TERMINAL Detail A Figure 1 6 Safetying Turnbuckle Assemblies Revision 2 1 15 ...
Page 26: ...s by a Carefully examine any cable for passing a cloth along length of cable This will detect corrosion that has a broken wire in a section not in broken wires if cloth snags on cable Critical areas for contact with wear producing airframe components wire breakage are those sections of cable which pass such aspulleys fairleads rub blocks etc It may be through fairleads across rub blocks and around...
Page 27: ...Y WIPING CLOTH ALONG CABLE BROKEN WIRE DETECTED VISUALLY WHEN CABLE WAS REMOVED AND BENT NORMAL TECHNIQUE FOR BENDING CABLE AND CHECKING FOR BROKEN WIRES DONOT BEND INTO LOOP SMALLER THAN 50 CABLE DIAMETERS Figure 1 7 Cable Broken Wire Inspection Revision 2 1 17 ...
Page 28: ...storage temperatures rise above temperatures in excess of 95 F Containers shall be 40F but are not warmer than 20 F the materials tightly closed prior to being placing them into the may be stored for a maximum ofone week above 30 F proper storage environment For proper storage plus time at 40 F or colder for a combined total not to environment refer to Table 1 7 and the following exceed four weeks...
Page 29: ...udiness for appearance application time tack free time cure e Class VII Cyanoacrylic Base Adhesives time and adhesion Verify that product is still liquid with no visible signs 7 Type I Class B sealants should be checked of contamination for appearance applicatiion time cure time tack free Class VIII Pressure Sensitive Materials time and adhesion In addition Class B 2 and B 4 Open containers and in...
Page 30: ... Months RTV 157 40TO 80F 12 Months 6 Months 6 Months RTV 158 40TO 80 F 12 Months 6 Months 6 Months RTV 159 40 TO 80 F 12 Months 6 Months 6 Months RTV732 40 TO 80 F 12 Months 6 Months 6 Months RTV 102 40 TO 80 F 12 Months 6Months 6 Months RTV 103 40 TO 80 F 12 Months 6 Months 6 Months RTV 106 40 TO 80 F 12 Months 6 Months 6 Months RTV 108 40 TO 80 F 12 Months 6 Months 6 Months RTV 109 40 TO 80 F 12...
Page 31: ...nths 2 Months PR1422 40 TO 80F 6 Months 2 Months 2 Months PR1440 40 TO 80F 6 Months 2 Months 2 Months GC435 40 TO 80F 6 Months 2 Months 2 Months Pro Seal 567 40 TO 80 F 6 Months 2 Months 2 Months PR810 40 TO 80 F 6 Months 2 Months 2 Months Pro Seal 700 40 TO 80 F 6 Months 2 Months 2 Months GC 1900 40 TO 80 F 6 Months 2 Months 2 Months PR366 40 TO 80OF 6 Months 2 Months 2 Months Pro Seal 735 40 TO ...
Page 32: ...Engines B14 2 4 Hydraulic Brake System 1B22 2 12 Flyable Storage CLEANING 1B22 2 12 Continental Engines B14 2 4 General Description 1B22 2 12 Returning Aircraft to Service 1B15 2 5 Windshields and Windows 1B23 2 13 Temporary Storage 1B15 2 5 Materials Required 1B23 2 13 Inspection During Storage 1B16 2 6 Waxing B23 2 13 Returning Aircraft to Service 1B16 2 6 Preventive Maintenance 1B23 2 13 Indefi...
Page 33: ...r outboard em aircraft on the ground Beginning with 1982 the tow pennage surfaces When pushing on the tail bar is stowed under the rear seat using two clips cone always apply pressure at a bulkhead to one attached to the center leg of the seat and one avoid buckling the skin secured to the floorboard under the left side of the seat When no tow bar is available press down at the horizontal stabiliz...
Page 34: ... aircraft tail and attach tail stand to tie down ring BE SURE that tail stand weighs enough to keep tail down under all conditions and is strong enough to support aircraft weight c Raise jacks evenly until desired height is reached ICAUTIONi When using the universal jack point flexibility of the gear strut will cause the main wheel to slide in board as the wheel is raised tilting the jack The jack...
Page 35: ...addition Operating Handbook the pitot tube static air vents air vents openings in the engine cowling and other similar openings 2 7 PARKING Parking precautions depend prin shall have protective covers installed to prevent entry cipally on local conditions As a general precaution of foreign material If at the end of thirty 30 days set parking brake or chock the wheels and install the aircraft will ...
Page 36: ...be verify that cabin door latch is open reinstalled in the same aircraft from which it 6 DO NOT stand within arc of propeller was removed If the battery is returned to blades while turning propeller service in a different aircraft appropriate d The airplane should be flown for thirty 30 record changes must be made and notification minutes reaching but not exceeding normal oil sent to the Cessna Cl...
Page 37: ...tative mixture consists of tion the pitot tube static source vents air vents one part compound MIL C 6529C Type I openings in the engine cowling and other similar mixed with three parts new lubricating oil openings should have protective covers installed to of the grade recommended for service prevent entry of foreign material o Attach a warning placard to the propeller to the effect that the prop...
Page 38: ...pray each cylinder without rotating crank move nozzle or spray gun from top to bottom of cyl inder The corrosion preventive mixture is harm NOTE ful to paint and should be wiped from Type IImay be painted surfaces immediately thoroughly mixin one part compound MIL C 6529 Type I Esso RustBan 628 Cos o Attach a warning placard on the throttle control moline No 1223 or equivalent with three knob to t...
Page 39: ...sump Install or close drain valve and ing oil Placard the propeller to the effect that it safety Service engine with oil per figure 24 should not be moved while the engine is in storage g Service and install the induction air filter p Prepare airframe for storage as outlined in para graph 2 11 steps a through f NOTE 2 15 INSPECTION DURING STORAGE Air The corrosion preventive mixture will planes wi...
Page 40: ...nts for all grounding wires during refuel Mixing of the EGME compound with the fuel ing procedures is extremely important because concentra tion in excess of that recommended 0 15 2 20 USE OF FUEL ADDITIVES FOR COLD percent by volume maximum will result in WEATHER OPERATION Strict adherence to recom detrimental affects to the fuel tanks such mended preflight draining instructions will eliminate as...
Page 41: ...vironmental Protection Agency cleaning and inspection of the carburetor should be advises that mechanic and other workers accomplished at each 100 hour inspection and any who handl engine oil are advised to time water in the fuel is suspected minm skin contact with used oil and a With the fuel valve OFF remove carburetor promptly remove used oil from the skin In a drain plug and clean off any seal...
Page 42: ... unfiltered air to enter the induc quick drain valve in oil sump Push up on quick tion system Any filter that appears doubtful drain valve until it locks open and allow oil to drain shall have a new filter installed in its place through hose into container c Without Quick Drain Valve Remove oil drain d After washing rinse filter with clear water un plug from engine sump and allow oil to drain into...
Page 43: ...n air pres move dampener rod to place piston to the end of the sure barrel opposite the filler plug f Remove filler plug and fill shimmy dampener 2 28 NOSE GEAR SHOCK STRUT The nose gear with hydraulic fluid shock strut requires periodic checking to ensure that NOTE the strut is filled with hydraulic fluid and is inflated to the correct air pressure To service the nose gear Be sure that the shimmy...
Page 44: ...lace airplane inside hangar or in shaded area and allow to cool from heat of sun s direct rays 2 33B WAXING b Using clean preferably running water flood a Hand polishing wax should be applied to acrylic surface Use bare hands with no jewelry to feel and surfaces The wax has an index of refraction nearly dislodge any dirt or abrasive materials the same as transparent acrylic and tend to mask any c ...
Page 45: ...x livery of the airplane In the event that polishing or pose a flame within 100 feet of the cleaning area buffing is required within the curing period it is Compressed air used for cleaning agent application recommended that the work be done by someone ex or drying should be regulated to the lowest practical perienced in handling uncured paint Any Cessna pressure Use of a stiff bristle brush rathe...
Page 46: ...ns shall be accomplished at each 100 hour inspection 2 45 NOSE GEAR TORQUE LINKS Lubricate nose gear torque links every 50 hours When operating 2 38 UPHOLSTERY AND INTERIOR cleaning pro from a dirt strip or in extremely dusty areas more longs upholstery fabrics and interior trim To clean frequent lubrication of the torque links is required the interior proceed as follows a Empty all ash trays and ...
Page 47: ...s thereto must be used except as noted in paragraph 2 23 herein Refer to Continental Aircraft Engine Service Bulletin M82 8 and any superseding bulletins revisions or supplements thereto for further recom mendations Oil capacities for the aircraft are given in the following chart To minimize loss of oil through the breather fill to specified oil level on dipstick for normal operation flight of les...
Page 48: ...W 40 225 SAE 30 or 210 SAE 20W 30 The overlap of oil grades is based on a mid range of ambient ground temperature vs maximum oil inlet temperature Aviation grade ashless dispersant oil conforming to Avco Lycoming Service Instruction No 1014 and all revisions and supplements thereto MUST BE USED Oil capacities for the aircraft are given in the following chart For extended flight fill to FULL mark o...
Page 49: ...ore first flight of the day 12 FUEL STRAINER Drain off any water and sediment before first flight of the day 7 OIL DIPSTICK Check on preflight Add oil as necessary Refer to paragraph 2 23 for details Check that filler cap is tight and oil filler is secure 8 PITOT AND STATIC PORTS Check for obstructions before first flight of the day 6 OXYGEN CYLINDER Check for anticipated requirements before each ...
Page 50: ...RBURETOR DRAIN PLUG Check for thread sealant residue in float chamber Refer to paragraph 2 22 12 FUEL STRAINER Disassemble and clean strainer bowl and screen 16 INDUCTION AIR FILTER Clean filter per paragraph 2 24 Replace if damaged 17 ENGINE OIL SYSTEM If engine is equipped with LONG external oil filter change oil and filter each 100 hours or every 6 months 1 VACUUM RELIEF VALVE FILTER Replace ea...
Page 51: ...level and fill as required with hydraulic fluid 16 INDUCTION AIR FILTER Replace each 500 hours or annually Refer to paragraph 2 24 2 VACUUM SYSTEM CENTRAL AIR FILTER Replace each 500 hours Refer to paragraph 2 25 AS REQUIRED 10 GROUND SERVICE RECEPTACLE Connect to 24 volt DC negative ground power unit Refer to Section 16 Figure 2 4 Servicing Sheet 5 of 5 2 20 Revision 1 ...
Page 52: ...Products of most reputable manufacturers meet or exceed these specifications LUBRICANTS PG SS G 659 POWDERED GRAPHITE GR MIL G 81322A GENERAL PURPOSE GREASE GH MIL G 23827A AIRCRAFT AND INSTRUMENT GREASE GL MIL G 21164C HIGH AND LOW TEMPERATURE GREASE OGMIL L 7870A GENERAL PURPOSE OIL PL VV P 236 PETROLATUM GP NO 10 WEIGHT NON DETERGENT OIL OL VV L 800A LIGHT OIL ALSO REFER TO PARAGRAPH 2 45 ALSO ...
Page 53: ...FER TO INSPECTION Q ICHART IN THIS SECTION AND RUDDER BARS AND PEDALS TO SECTION 9 OF THIS MANUAL ELEVATOR TRIM TAB ACTUATOR 01 PARKING BRAKE 3 BATTERY TERMINALS WING STRUT ATTACH HANDLESHA UPPER BOLT HOLE TYPICAL X L CABIN DOOR WINDOW G i INSERT GROOVES CL WING STRUT ATTACH UPON INSTALLATION NEEDLE BEARINGS Figure 2 5 Lubrication Sheet 2 of 3 2 22 ...
Page 54: ...er seacoast conditions Wipe with a clean dry cloth Lubricate unsealed pulley bearings rod ends Oilite bearings pivot and hinge points and any other friction point obviously needing lubrication with general purpose oil every 1000 hours or oftener if required Paraffin wax rubbed on seat rails will ease sliding the seats fore and aft Lubricate door latching mechanism with MIL G 81322A general purpose...
Page 55: ...gram that best suits the operation of the airplane the following is provided a If the airplane is flown less than 200 hours annually the following conditions apply 1 If flown for hire a An airplane operating in this category must be inspected each 100 hours of operation 100 HOUR and each 12 calendar months of operation ANNUAL 2 If not flown for hire a An airplane operating in this category must be...
Page 56: ... compliance of any operation scheduled the next operation in sequence retains a due point from the time the late operation was originally sched uled 2 In the event of early compliance of any operation scheduled that occurs 10 hours or less ahead of schedule the next phase due point may remain where originally set 3 In the event of early compliance of any operation scheduled that occurs more than 1...
Page 57: ...nals 7 STRUCTURAL FASTENERS Inspect for correct torque in accordance with applicable torque values Refer to Bolt Torque Data during installation or when visual inspection indicates the need for a torque check NOTE Torque values listed are not to be used for checking tightness of installed parts during service 8 FILTERS SCREENS AND FLUIDS Inspect for cleanliness and the need for replacement at spec...
Page 58: ...al d Engine response to changes in power e Any unusual engine noises f Fuel selector and or shutoff valve operate engine on each tank or cell position and OFF position long enough to ensure shutoff and or selector valve functions properly g Idling speed and mixture proper idle cut off h Alternator and ammeter i Suction gage j Fuel flow indicator 2 After the inspection has been completed an engine ...
Page 59: ...tput Check cumulative time and useful life of batteries in accordance with FAR Part 91 207 Refer to Section 16 Emergency Locator Transmitter Checkout Interval B 7 Instrument Panel Shock Mounts Ground Straps and Covers Inspect for deterioration cracks and security of attachment B 8 Pilot s and Copilot s Inertia Reels Inspect for security of installation proper operation and evidence of damage B 9 S...
Page 60: ... support C 6 Wing Access Plates Check for damage and security of installation C 7 Vertical and Horizontal Stabilizers Tips and Tailcone Inspect externally for skin damage and condition of paint C 8 Vertical and Horizontal Stabilizers and Tailcone Structure Inspect bulkheads spars ribs and skins for cracks wrinkles loose rivets corrosion or other damage Inspect vertical and horizontal stabilizer at...
Page 61: ...rrosion or other damage and security of attachment E Aileron Control System Section 6 E 1 Ailerons and Hinges Check condition security and operation E 2 Aileron Structure Control Rods Hinges Balance Weights Bellcranks Linkage Bolts Pulleys and Pulley Brackets Check condition operation and security of attachment E 3 Ailerons and Cables Check operation and security of stops Check cables for tension ...
Page 62: ...nt and proper operation through full travel Check pulleys cables sprockets bearings chains bungees and turnbuckles for condition and security Check electric trim controls for operation as applicable H 4 Elevator Trim Tab Stop Blocks Inspect for damage and security H 5 Elevator Trim Tab Actuator Clean lubricate D H 6 Elevator Trim Tab Actuator Free Play limits inspection Refer to Section 9 9 for cl...
Page 63: ...or F damage and service per paragraph 2 24 J 10 Induction Airbox Valves Doors and Controls Remove air filter and inspect hinges doors seals and attaching parts for wear and security Check operation Clean and inspect air filter and re oil if flock coated J 11 Alternate Induction Air System Check for obstructions operation and security J 12 Alternator Check brushes leads commutator or slip ring G fo...
Page 64: ...ine Cylinders Rocker Box Covers and Pushrod Housings Check for fin damage cracks oil leakage security of attachment and general condition J 31 Turbocharger if applicable M a Inspect turbocharger mounting bracket ducting linkage and attaching parts for general con dition linkage or damage and security of attachment b Check waste gate actuator controller oil and vent lines overboost relief valve and...
Page 65: ...n 1 K 9 Fuel quantity indicating system operational test is required Each every 12 months Refer to Section 15 for detailed 1 accomplishment instructions L Propeller and Propeller Governor Section 13 L 1 Proper Mounting Check for security of installation L 2 Propeller Blades Inspect for cracks dents nicks scratches erosion corrosion or other damage L 3 Spinner Check general condition and attachment...
Page 66: ... general condition and markings for legibility N 7 Instrument Lines Fittings Ducting and Instrument Panel Wiring Check for proper routing support and security of attachment N 8 Static System Inspect for security of installation cleanliness and evidence of damage N 9 Navigation Indicators Controls and Components Inspect for condition and security N 10 Airspeed Indicator Vertical Speed Indicator and...
Page 67: ... Inspect wiring mounting condition and wire routing 8 Switches Check operation terminals wiring and mounting for conditions security and interference O 9 Instrument Panel and Control Pedestal Inspect wiring mounting and terminals for condition and security Check resistance between stationary panel and instrument panel for proper ground O 10 External Power Receptacle and Power Cables Inspect for co...
Page 68: ...partment and magneto to engine timing should be inspected and checked If magneto to engine timing is correct within plus zero degrees to minus two degrees internal timing need not be checked If timing is out of tolerance remove magneto and set internal timing then install and time to the engine Re fer to Section 11 or 11A and the magneto manufacturers service instructions for magneto timing proce ...
Page 69: ...er to Cessna for the supplier s product C In addition to these time limits the components listed herein are also inspected at regular time intervals set forth in the Inspection Charts and may require overhaul replacement before the time limit is reached based on service usage and inspection results 2 Cessna Established Replacement Time Limits A The following component time limits have been establi...
Page 70: ...st Every 15 years 6 Years or at vacuum pump replacement whichever occurs first 500 hours Note 10 500 hours or 10 years whichever occurs first Note 10 Supplier Established Replacement Time Limits A The following component time limits have been established by specific suppliers and are reproduced as follows Table 2 Supplier Established Replacement Time Limits COMPONENT REPLACEMENT OVERHAUL TIME ELT ...
Page 71: ... latest revision for time limits Note 7 Refer to Cessna Service Bulletin SEB94 7 Revision 1 Dukes Inc Service Bulletin NO 0003 or latest revision Note 8 Refer to the applicable McCauley or Hartzell Service Bulletins and Overhaul Manual for replacement and overhaul information Note 9 The air filter may be cleaned refer to Section 2 of this service manual for servicing instructions For airplanes equ...
Page 72: ...eration 1 the FIRST 50 HOUR ITEMS listed in the inspection Time Limits Charts in 2 59 must also be performed After these FIRST 50 HOUR items have been accomplished they have permanent inspection time limits which are covered in the Operations Schedules b ALL OTHER AIRCRAFT To quality other aircraft which have more than 50 hours time in service for the Progressive Inspection Program conduct a COMPL...
Page 73: ...MODEL 182 T182 SERIES SERVICE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK 2002 Cessna Aircraft Company Temporary Revision Number 3 7 October 2002 2 40B ...
Page 74: ...plane flight log book for use as a quick reference for pilots and maintenance personnel in determining when inspections are due and that they are performed within prescribed flight time intervals b Use the Progressive Care Program Component Overhaul and Replacement Log pro vided herein for each airplane This log is to be kept with the airplane maintenance records and serves as a periodic reminder ...
Page 75: ...RESSIVE CARE PROGRAM MODEL 182 T182 AIRPLANES COMPONENT OVERHAUL AND REPLACEMENT RECORD REPLACEMENT NEXT OVERHAUL COMPONENT DATE REASON FOR REPLACEMENT PART NUMBER AIRPLANE SERIAL NUMBER HOURS DATE NUMBER X X X X X X X X X X X 2 42 Revision 2 ...
Page 76: ...rst Inspection Due Column was filled out to show the total flying time at which each of the four 4 operation inspections would be due 2 As each inspection was performed the total flying time was recorded in the Inspection Ac complished column The next Inspection Due space for that particular operation is also filled in at this time These times will always be 200 hours from the last due point provi...
Page 77: ...n and security of attachment E 5 Aileron Controls Check freedom of movement and proper operation through full travel with and without flaps extended F 1 Flaps Check tracks rollers and control rods for security of attachment Check operation F 2 Flap Actuator Threads Clean and lubricate Refer to paragraph 2 46 for detailed instructions G 1 Elevator Control Check freedom of movement and proper operat...
Page 78: ...ation and security J 13 Alternator Mounting Bracket and Electrical Connections Check condition and security Check alternator belts for condition and proper adjustment Refer to Paragraph 1642 for belt tension J 15 Oil Cooler Check for obstructions leaks and security of attachment J 16 Exhaust System Inspect for cracks and security Air leak check exhaust system Refer to Section 11 and 11A Paragraphs...
Page 79: ...e impellers for damage J 33 Engine Baffles and Seals Check condition and security of attachment J 34 Engine Oil Change Short Oil Filter approximately 4 8 inches a Replace Filter b Add recommended grade aviation oil to replace oil lost in existing filter Without Oil Filter Drain oil sump and oil cooler inspect and clean screens and refill with recommended grade aviation oil J 35 Long Oil Filter app...
Page 80: ...ase leaks L 8 Propeller Anti ice Slip Rings Brushes and Boots Inspect for condition and security Perform operational check M 2 Heater Components Inlets and Outlets Inspect all lines connections ducts clamps seals and gaskets for condition restriction and security M 4 Pitot Tube and Stall Warning Vane Check for condition and obstructions M 5 Pitot Tube Heater Element Perform operational check N 3 V...
Page 81: ...agnetos Inspection lubrication and overhaul procedures I J 21 Magnetos Check external condition security and electrical J leads for condition Check timing to engine and internal timing if engine timing requires adjustment J 22 Magnetos Timimg Procedures and intervals K J 28 Hoses Metal Lines and Fittings Inspect for signs of oil and L fuel leaks Check for abrasions chafing security proper routing ...
Page 82: ...s for 400 EACH condition and security 1 M 8 Oxygen Cylinder Inspect for condition check hydrostatic test EACH date and perform hydrostatic test if required 5 N 4 Vacuum System Air Filter Inspect for damage deterioration Q and contamination Clean or replace if required NOTE Smoking will cause premature filter clogging N 5 Vacuum System relief Valve Inspect for condition and security R N 10 Airspeed...
Page 83: ... contact breaker point compartment and magneto to engine timing should be inspected and checked If magneto to engine timing is correct within plus zero degrees to minus two degrees internal timing need not be checked If timing is out of tolerance remove magneto and set internal timing then in stall and time to the engine Refer to Section 11 or 11A and the magneto manufacturers service instructions...
Page 84: ...operation as applicable B 14 Portable Hand Fire Extinguisher Inspect for proper operating pressure condition security of installation and servicing date B 15 Seat Tracks and Stops Inspect seat tracks for condition and security of installation Check seat track stops for damage and correct location Ensure inspection of seat rails for cracks EACH 50 HOURS Refer to Section 3 B 17 Fuel Line and Selecto...
Page 85: ... attachment and for evidence of wear Check friction locks for proper operation J 4 Cowl Flap Controls Check freedom of movement through full travel J 8 Induction System Check security of clamps tubes and ducting Inspect for evidence of leakage J Alternate Induction Air System Check for obstructions operation and security J 13 Alternator Mounting Bracket and Electrical Connections Check condition a...
Page 86: ...dition and attachment L 7 Propeller Governor and Control Inspect for oil and grease leaks L 8 Propeller Anti ice Slip Rings Brushes and Boots Inspect for condition and security Perform operational check M 4 Pitot Tube and Stall Warning Vane Check for condition and obstructions M 5 Pitot Tube Heater Element Perform operational check N 1 Vacuum System Inspect for condition and security N 2 Vacuum Sy...
Page 87: ... Magnetos Inspection lubrication and overhaul procedures J 21 Magnetos Check external condition security and electrical J leads for condition Check timing to engine and internal timing if engine timing requires adjustment J 22 Magnetos Timimg Procedures and intervals K J 28 Hoses Metal Lines and Fittings Inspect for signs of oil and L fuel leaks Check for abrasions chafing security proper routing ...
Page 88: ...s for 400 EACH condition and security 1 M 8 Oxygen Cylinder Inspect for condition check hydrostatic test EACH date and perform hydrostatic test if required 5 N 4 Vacuum System Air Filter Inspect for damage deterioration Q and contamination Clean or replace if required NOTE Smoking will cause premature filter clogging N 5 Vacuum System relief Valve Inspect for condition and security R N 10 Airspeed...
Page 89: ... contact breaker point compartment and magneto to engine timing should be inspected and checked If magneto to engine timing is correct within plus zero degrees to minus two degrees internal timing need not be checked If timing is out of tolerance remove magneto and set internal timing then in stall and time to the engine Refer to Section 11 or 11A and the magneto manufacturers service instructions...
Page 90: ...her damage Inspect vertical and horizontal stabilizer attach bolts for looseness Retorque as necessary Check security of inspection covers fairings and tips E 1 Ailerons and Hinges Check condition security and operation E 2 Aileron Structure Control Rods Hinges Balance Weights Bellcranks Linkage Bolts Pulleys and Pulley Brackets Check condition operation and security of attachment E 3 Ailerons and...
Page 91: ...and Cowl Faps Inspect for cracks dents and other damage security of cowl fasteners and cowl mounted landing lights for attachment Check cowl flaps for condition security and operation J 2 Engine Inspect for evidence of oil and fuel leaks Wash engine and check for security of accessories J 3 Engine Propeller Controls and Linkage Check general condition freedom of movement through full range Check f...
Page 92: ...d security J 27 Engine Primer Check for leakage operation and security J 28 Hoses Metal Lines and Fittings Inspect for signs of oil and fuel leaks Check for abrasions chafing security proper routing and support and for evidence of deterioration J 29 Cold and Hot Air Hoses Check condition routing and security J 30 Engine Cylinders Rocker Box Covers and Pushrod Housings Check for fin damage cracks o...
Page 93: ...operation Disassemble flush and clean screen and bowl L 1 Propeller Mounting Check for security of installation L 2 Propeller Blades Inspect for cracks dents nicks scratches erosion corrosion or other damage L 3 Spinner Check general condition and attachment L 4 Spinner and Spinner Bulkhead Remove spinner wash and inspect for cracks and fractures L 7 Propeller Governor and Control Inspect for oil ...
Page 94: ... of starter brushes brush leads and commutator J 20 Magnetos Inspection lubrication and overhaul procedures I J 21 Magnetos Check external condition security and electrical J leads for condition Check timing to engine and internal timing if engine timing requires adjustment J 22 Magnetos Timimg Procedures and intervals K J 28 Hoses Metal Lines and Fittings Inspect for signs of oil and L fuel leaks...
Page 95: ...tilation System Inspect clamps hoses and valves for 400 EACH condition and security I M 8 Oxygen Cylinder Inspect for condition check hydrostatic test EACH date and perform hydrostatic test if required 5 N 4 Vacuum System Air Filter Inspect for damage deterioration Q and contamination Clean or replace if required NOTE Smoking will cause premature filter clogging N 5 Vacuum System relief Valve Insp...
Page 96: ... contact breaker point compartment and magneto to engine timing should be inspected and checked If magneto to engine timing is correct within plus zero degrees to minus two degrees internal timing need not be checked If timing is out of tolerance remove magneto and set internal timing then in stall and time to the engine Refer to Section 11 or 11A and the magneto manufacturers service instructions...
Page 97: ...of attachment B 8 Pilot s and Copilot s Inertia Reels Inspect for security of installation proper operation and evidence of damage B 9 Seats Seat Belts and Shoulder Harnesses Check general condition and security Check operation of seat stops and adjustment mechanism Inspect belts for condition and security of fasteners B 10 Windows Windshield Doors and Seals Inspect general condition Check latches...
Page 98: ...rosion or other damage and security of attachment G 3 Elevator Control System Inspect pulleys cables sprockets bearings chains and turnbuckles for condition security and operation H 2 Elevator Trim System Check cables push pull rods bellcranks pulleys turnbuckles fairleads rub strips etc for proper routing condition and security H 3 Trim Controls and Indicators Check freedom of movement and proper...
Page 99: ...ge security of attachment and evidence of wear Check waste gate return spring for condition and security J 33 Engine Baffles and Seals Check condition and security of attachment J 34 Engine Oil Change Short Oil Filter approximately 4 8 inches a Replace Filter b Add recommended grade aviation oil to replace oil lost in existing filter Without Oil Filter Drain oil sump and oil cooler inspect and cle...
Page 100: ... Panel VHF Nav Com s ADF Transponder DME and Compass System Inspect for deterioration cracks and security of instrument panel mounts Inspect for security of electrical connections condition and security of wire routing N 13 Avionics Operating Controls Inspect for security and proper operation of controls and switches and ensure that all digital segments will illuminate properly N 14 Remote Mounted...
Page 101: ...odel and SN Airplane Time INSPECTION COMPLETED BY O 9 Instrument Panel and Control Pedestal Inspect wiring mounting and terminals for condition and security Check resistance between stationary panel and instrument panel for proper ground Q 1 Brakes Test toe brakes and parking brake for proper operation 2 68 Revision 3 ...
Page 102: ...starter brushes brush leads and commutator J 20 Magnetos Inspection lubrication and overhaul procedures J 21 Magnetos Check external condition security and electrical J leads for condition Check timing to engine and internal timing if engine timing requires adjustment J 22 Magnetos Timing Procedures and intervals K J 28 Hoses Metal Lines and Fittings Inspect for signs of oil and L fuel leaks Check...
Page 103: ...ntilation System Inspect clamps hoses and valves for 400 EACH condition and security 1 M 8 Oxygen Cylinder Inspect for condition check hydrostatic test EACH date and perform hydrostatic test if required 5 N 4 Vacuum System Air Filter Inspect for damage deterioration Q and contamination Clean or replace if required NOTE Smoking will cause premature filter clogging N 5 Vacuum System relief Valve Ins...
Page 104: ...ct breaker point compartment and magneto to engine timing should be inspected and checked If magneto to engine timing is correct within plus zero degrees to minus two degrees internal timing need not be checked If timing is out of tolerance remove magneto and set internal timing then in stall and time to the engine Refer to Section 11 or 11A and the magneto manufacturers service instructions for m...
Page 105: ...clamps and expansion joints for cracks condition and security Air leak check exhaust system 16 Turbocharger if applicable a Inspect mounting brackets ducting linkage and attaching parts for general condition leak age or damage and security of attachment b Check waste gate actuator controller oil and vent lines overboost relief valve and compres sor housing for leakage apparent damage se curity of ...
Page 106: ...plugs to top 25 Carburetor Drain and flush carburetor bowl and clean inlet strainer Check general condition and se curity 26 Engine Oil Change Short Oil Filter approximately 4 8 inches a Replace filter b Add recommended grade aviation oil to re place oil lost in existing filter Without Oil Filter Drain oil sump and oil cooler in spect and clean screens and refill with recom mended grade aviation o...
Page 107: ...on test PROPELLER 1 Spinner Check general condition and attachment 2 Spinner and Spinner Bulkhead Remove spinner wash and inspect for cracks and fractures 3 Propeller Blades Inspect for cracks dents nicks scratches erosion corrosion or other damage 4 Propeller Anti Ice Slip Rings Brushes and Boots Inspect for condition and security Perform opera tional check 5 Propeller Mounting Check for security...
Page 108: ...d retorque as required 6 Fuel Tank or Bladder Drains Drain water and sedi ment 7 Pitot Tube and Stall Warning Vane Check for con dition and obstructions 8 Pitot Tube Heater Element if installed Perform operational check 9 Fuel Tank Vent Lines and Vent Valves Check vents for obstruction and proper positioning Check valves for operation 10 Aileron Structure Control Rods Hinges Balance Weights Bellcr...
Page 109: ...nd security 17 Flaps Check tracks rollers and control rods for se curity of attachment Check operation 18 Flap Actuator Threads Clean and lubricate 19 Fuel System Inspect plumbing and components for mounting and security 20 Fuel Bladders Check for leaks and security condi tion of fuel caps adapters and placards 21 Integral Fuel Tanks Check for evidence of leakage and condition of fuel caps and pla...
Page 110: ...ng 5 Tires Check tread wear and general condition Check for proper inflation 6 Wheels Brake Discs and Linings Inspect for wear cracks warps dents or other damage Check wheel through bolts and nuts for evidence of looseness 7 Brakes Master Cylinders and Parking Brake Check master cylinders and parking brake mechanism for condition and security Check fluid level and test op eration 8 Brakes Test toe...
Page 111: ...er Inspect the rudder skins for cracks and loose rivets rudder hinges for condition cracks and security hinge bolts hinge bearings hinge attach fittings and bonding jumper for evidence of dam age and wear failed fasteners and security Inspect the rudder hinge bolts for proper safetying of nuts with cotter pins Inspect balance weight for loose ness and the supporting structure for damage 9 Rudder T...
Page 112: ...SS DIRECTIVES 1 Check that all applicable Cessna Service Bulletins Service Newsletters and Supplier Service Notices are complied with 2 Check that all applicable Airworthiness Directives and Federal Aviation Regulations are complied with 3 Ensure all Maintenance Record Entries required by Federal Aviation Regulations are completed before returning the airplane to service OPERATION NO 4 COMPLETED A...
Page 113: ... Adjustment F8 3 14 Fixed 1E22 3 4 Rear Passengers Seat 1F83 14 Description 1E22 3 4 Description F8 3 14 Removal Installation 1E22 3 4 Removal Installation 1F20 3 24 Cleaning and Waxing 1E22 3 4 Auxiliary Seat 1F20 3 24 Windshield Window Installation Description 1F20 3 24 Techniques 1E22 3 4 Removal Installation 1F20 3 24 Repair 1E22 3 4 Seat Repair 1F20 3 24 Surface Patch 1E22 3 4 Cabin Upholster...
Page 114: ...ut of and held inplace by retaining strips lower retainers e Clean sealer from inner sidewalls and bottom of 3 13 REMOVAL AND INSTALLATION retainers a Remove upholstery as necessary to expose retainer strips inside cabin 3 6 INSTALLATION b Drill out rivets as necessary to remove re a If new windshield is to be installed remove pro tainers on both sides and lower edge of window tective cover and cl...
Page 115: ...R ANGLE THAN STOP MATERIAL STOP BEVELED EDGE DRILLED PATCH AND HOLE DURING CEMENTING PRESSURE SHOULD BE TRIMMED NEED BE APPLIED ONLY ON TOP C R FhN cfi I WITH TAPERED EDGES SURFACE TAPER ASSURES EQUAL CR ACKEFC I PRESSURE ON ALL SIDES s n FCE PATCH HEAT EDGES OF ll o e PATCH UNTIL SCRFACE PATCH FOR CRACKS SOFT AND FORCE IT INTO HOLE HOLD IT IN PLACE UNTIL COOL AND HARD TO ASSURE PERFECT FIT AFTER ...
Page 116: ...or excessively chipped are not to be located in the pilot s line of vision dur ing landing or normal flight Whenever possible a coolant such as a plastic drill a SURFACE PATCH If a surface patch is to be ing wax should be used to lubricate the drill bit Installed trim away the damaged area and round all Cessna recommends Reliance drill wax or Johnson corners Cut a piece of plastic of sufficient si...
Page 117: ... therstrip to allow for drainage Position splice with Polishing can be accomplished by hand but notch at door low point and apply a thin even coat of will require a considerably longer period of EC 1300L adhesive 3 M Company or equivalent to time to attain the same result as produced both surfaces Allow to dry until tacky before press by a buffing wheel ing into place on door Do not stretch weathe...
Page 118: ...of windshield and window when felt seal 3 is used 5 3 6 2 4 11 are 32 DetailB Detail A 1 Inner Retainer 2 Windshield 3 Pelt Seal Detl C 4 Outer Retainer 5 Cabin Top Skin 6 Overhead Cabin Window B 7 Fuselage Structure A Q 7 2 TAINING FIXED WINDOWS 2 NOTE 3 6 Revision 1 I de ofwnsil n idw 3 6 Revision I ...
Page 119: ...3 Door Outer Skin F etail E F 18 NOTES A Openable window may be installed in RH cabin door 19 Forming of the door flanges by striking with soft mallet etc is NOT permissible since damage 20 to bonded areas may occur 23 Trim cutout in inner pan if necessary to maintain 23 10 inch minum clearance with door stop arm Spray cabin door and window seals with MS 122 Miller Stephenson Chem Corp or equivale...
Page 120: ... clutch components are matched upon assembly The clutch mechanism if defec tive should be replaced as a 22 unit 17 Y E A 6 71 2726 24 15 r Sy 16 i 2j7f ROTARY CLUTCH 18 16 1 Top Bolt Guide 10 Bolt Adjust Screw 20 Outside Handle 2 Bolt 11 Pull Bar 21 Pin 3 Side Bolt Guide 12 Spring 22 Mounting Structure 4 Base Bolt Guide 13 Pin 23 Shim 5 Latch Base Plate 14 Inside Handle 24 Rotary Clutch 6 Abrasive...
Page 121: ...Beginning with 18267716 See bolts and moving screw 28 in the slot to raise or figure 3 5 lower forward end of the handle 3 36 INSTALLATION OF LOCK ASSEMBLY ON 3 33 DOOR LATCHES Beginning with 18267716 LATCH ASSEMBLY Beginning with 18267716 and See figure 3 5 T18267717 See figure 3 5 a Assemble locking arm 2 with pin assembly 5 3 34 DESCRIPTION The cabin door latch consists by placing one washer 4 ...
Page 122: ...E tion This adjustment will ensure that when the 3 39 RIGGING CABLE ASSEMBLY Beginning door is opened from the outside the bolt with 18267716 See figure 3 5 will engage the latch catch and the exterior a Pull excess slack out of cable 32 Attach handle will stay open until the door is closed clamp 33 and nut 31 to cable so that it aligns with again 193 inch hole in door pan and attach Refer to para...
Page 123: ...Pin 32 Cable Assembly 43 Clamp Bolt 44 Push Rod Assembly 55 Inside Handle 56 Arm Rest 57 Support 58 Shaft Assembly 59 Plate Assembly 60 Door Latch Assembly 61 Shim 62 Escutcheon Figure 3 5 Cabin Door Latch Beginning with 18267716 Sheet 1 of 3 3 11 ...
Page 124: ...4 Latch Base Assembly 2 Lock Washer 23 Sprin 3 Pin 24 Cam Assembly BoltWasher 17 Washer 5 Pin 18 Spring 6 Push C otter Pin 19 atch Cover 7 PuUlBar 20 Outside Handle 8 Pin 21 Lock Washer 9 Cotter Pin 22 Latch Base Assembly 10 Lock Washer 23 Pin 11 Pin 24 Cam Assembly 12 Bolt 25 Washer 13 Push Rod 46 Latch Cover Figure 3 5 Cabin Door Latch Beginning with 18267716 Sheet 2 of 3 3 12 ...
Page 125: ...Shim 30 875 inch Access Hole 48 Shim 54 Doubler 54 31 Self Locking Clip 49 Striker Plate Cover On Nut 32 Cable Assembly 51 53 33 Clamp 52 34 S1450 2A4 062 Washer 35 Screw 36 Screw 50 37 Washer 38 Nut 40 Casing 41 Tumblers 42 Cover Assembly 49 49 jl i LOOKING AFT AT Is I I LH REAR DOORPOST 48 0 47 8 1I A 281 ft l 29 30 I Detail A 34 j 6 41 433 42 4 24 39 40 41 43 44 45 Figure 3 5 Cabin Door Latch B...
Page 126: ...ealant General Electric Waterford NY It is extremely important that pilot s seat h Operate lock several times to ensure that all com stops are installed since acceleration ponents function properly and deceleration could possibly permit seat to become disengaged from seat rails NOTE and create a hazardous situation especially during take off and landing Steps f g and h apply to LH door only 3 49 M...
Page 127: ...et 17 Lower Hinge Bracket A 18 Door Sll 17I 19 RetainerStrip 17 1 y T 10 An9 B 9 i o 2 _ _ l cl 3 4 Detail D 25 inch notch 1e 3 DetailC 5 4 a Do not clue outt ends of weatherstr p k4 t together Refer tc paragraph 3 2T for removal and installatior of weatnerstr p As required for proper sealing of door Typical entire perimeter Figure 3 6 Baggage Door Installation 3 15 ...
Page 128: ... Trim 11 Seat Back Pocket 13 12 Bolt 13 Seat Frame 14 Seat Belt Retainer 15 Seat Adlust Bracket 19 16 Roll Pin 17 Seat Roller Kit 18 Seat Adlust Pin 16 13 Seat Adlust Spring r 14 20 Seat Ad ust Handle 21 Seat Bottom 22 Cu shion 23 Cover 24 Seat BaciK WARNING 3rommet I e 4 a m 2 6 aeti er I _ m LAW etm emaTm FRONT S I eN CLEAR VIo EW O THE PILOT FRONT SEAT INSTALLATION N CLEAR VIEWOF THE PILOT Figu...
Page 129: ...om 24 Seat Back 26 Vertical Adjustment Handle 27 Fore Aft Adjustment Handle 28 Articulating Adjustment Handle 29 Adjustment Screw 30 Bellcrank 31 Trim 24 32 Spacer 30 33 Channel 34 Torque Tube 35 Seat Structure 29 36 Roller 37 Link 28 27 19 Detail A 3 14 26 INFINITELY ADJUSTABLE FRONT SEAT INSTALLATION 36 Figure 3 7 Seat Installation Sheet 2 of 7 3 17 ...
Page 130: ...OARD SEAT RAILS 2 2 Cotter Pin 3 Seat Stop 4 Pin IT IS EXTREMELY IMPORTANT THAT PILOT S SEAT STOPS ARE INSTALLED SINCE ACCELERATION AND DECELER ATION COULD POSSIBLY PERMIT SEAT TO BECOME DISENGAGED FROM SEAT RAILS AND CREATE A HAZARDOUS SIT UATION ESPECIALLY DURING TAKEOFF AND LANDING Figure 3 7 Seat Instllation Sheet 3 of 7 3 18 Revision 1 ...
Page 131: ...ICE MANUAL 21 Seat Bottom 24 Seat Back 37 Spring 38 Bushing 24 39 Recline Cam 40 Recline Handle 41 Control Shaft 42 Recline Pawl 38 38 41 40 402 _ REAR SEAT 1977 THRU 1979 Detail A Figure 3 7 Seat Installation Sheet 4 of 7 3 19 ...
Page 132: ... 33 23 f23 A 23 22 REAR SEAT 1980 THRU 1981 1 Mechanical Control 22 Cushion 2 Adjusting Nut 23 Cover 3 Mechanical Lock 24 Seat Back 4 Control Wire 32 Spacer 5 Head Rest 43 Link 21 Seat Bottom 44 Seat Fitting Figure 3 7 Seat Installation Sheet S of 7 3 20 ...
Page 133: ...MODEL 182 T182 SERIES SERVICE MANUAL REAR SEAT BEGINNING WITH 1982 MODELS Figure 3 7 Seat Installation Sheet 6 of 7 3 20A ...
Page 134: ...MODEL 182 T182 SERIES SERVICE MANUAL 46 Detail A 35 47 21 Seat Bottom 24 Seat Back 35 Seat Structure 45 Bracket 46 Tongue 47 Hinge Bracket AUXILIARY SEAT Figure 3 7 Seat Installation Sheet 7 of 7 3 20B ...
Page 135: ...olstery material as required to expose rivets retaining old cam assembly c Drill out existing rivets and insert new cam assembly 2 Position seat back so pawl 3 en gages first cam slot as illustrated d Position cam so each slot bottom aligns with the 2 50 radius as illustrated e Clamp securely in this position and check travel of cam Pawl must contact bottom of each cam slot Using existing holes in...
Page 136: ... 1 Shoulder Harness 2 Harness Tray E 3 Washer 4 Spacer YJ 5 Cover 6 Bolt 7 Nut 10 8 Spacer 9 Seat Belt 6 10 Seat Frame X 11 Seat Fitting 9 Am 4 7 8 7 7 9 Detail D 1 10 v 2 1 Detail E Detail C Detail A 1977 THRU 1979 MODELS Figure 3 9 Seat Belt and Shoulder Harness Installation Sheet 1 of 2 3 22 ...
Page 137: ... S 004 f13 A 13 14 3 Washer 4 Spacer 12 5 Cover 12 6 Bolt 7 Nut 9 Seat Belt 11 Floorboard Bracket 12 Inertia Reel Assembly 13 Trim 14 Attach Plate 11 BDetail B Detail A Figure 3 9 Seat Belt and Shoulder Harness Installation Sheet 2 of 2 3 23 ...
Page 138: ...dures which may be used as a guide in removal and upholstery side panels Automotive type spring installation of cabin upholstery Major work if clips attach most door panels A dull putty knife possible should be performed by a mechanic experi makes an excellent tool for prying clips loose enced in upholstery replacement However if the When installing side panels do not over tighten work must be per...
Page 139: ...is 3 70 GLIDER TOW HOOK A glider tow hook now available which repositions the belt buck mounted in place of the tail tie down ring is available le shoulder harness connection Repositioning through 18265965 and F18200064 of the buckle is recommended to prevent inad vertent loosening of the seat belt Refer to Service Information Letter SE82 43 3 71 REAR VIEW MIRROR See figure 3 14 A rear view mirror...
Page 140: ...2 SERIES SERVICE MANUAL 1 Cargo Tie Down Ring 2 Battery Bracket 3 Nutplate 4 Seat Rail 5 Cargo Tie Down Ring Lug Slide Assembly For tie down ring installation Figure 3 11 Cargo Tie Downs Installation SHOP NOTES 3 26 ...
Page 141: ...MODEL 182 T182 SERIES SERVICE MANUAL Figure 3 12 Cargo Net Installation 2 I 34 1 Cover 4 5 5 2 Mirror 3 Grommet 4 Nut 5 Washer 6 g6 Deck Skin Thru 18266591 Figure 3 13 Rear View Mirror Installation 3 27 ...
Page 142: ...ion of web or lower flange is cracked index 2 b Any crack in crown of rail is in any direction other than right angle to length of rail c Number of cracks on any one rail exceeds four or any two cracks index 1 are closer than one inch NOTE Use of seat rail cargo tie downs is not permissible on seat rails with cracks Figure 3 14 Seat Rail Inspection 3 28 ...
Page 143: ...hment eccentric accomplished if four men are available to handle the bushings See figure 4 1 these bushings are used wing Otherwise the wing should be supported with to rig out wing heaviness a sling or maintenance stand when the fastenings are h Remove nuts washers bushings and bolts loosened attaching wing spars to fuselage a Remove wing root fairings and fairing plates b Remove all wing inspect...
Page 144: ...is approximately half the length of the aft bushing 16 1 Nut 7 Nut 13 Flap 2 Washer 8 Rub Strip 14 Aileron 3 Bolt 9 Moulding 15 Wing Tip 4 Bolt 10 Fairing 16 Navigation Strobe Light 5 Bushing 11 Screw 17 Stall Warning Unit 6 Washer 12 Inspection Plate 18 Fuel Cell Figure 4 1 Wing Installation Sheet 1 of 2 4 2 ...
Page 145: ...UE 300 LB IN MIN 690 LB IN MAX Detail B 1 Fairing 5 Wing Tip 9 Bolt 2 Lower Rear Fairing 6 Navigation and Strobe Lights 10 Eccentric Bushings 3 Wing Flap 7 Courtesy Light 11 Washers 4 Aileron 8 Fuel Filler Cap 12 Nut Figure 4 1 Wing Installation Sheet 2 of 2 4 3 ...
Page 146: ...70 or P 672 d Remove nut bolt and spacer used to attach strut or Tuck 92T to wing then remove strut from aircraft e Reverse preceding steps to install strut Be sure to insert soundproofing panel in wing 4 11 REPAIR before replacing wing root fairings ings the following applies 1 If groove exceeds 010 inch in depth and is k Install wing root fairings less than 75 inch from a rivet center the strut ...
Page 147: ... out Hinge brackets at the fin rear spar attach the rudder lined in paragraph 4 19 to install the horizontal stabilizer Rig elevator elevator trim and rudder systems as outlined in Sections 8 9 and 10 consecu 4 14 REMOVAL The vertical fin may be removed tively Check operation of tail navigation light and without first removing the rudder However for flashing beacon access and ease of handling the ...
Page 148: ... applied over epoxy primer but NOTE if the surface has been painted the paint shall be removed from the bond area This shall be Should boot be attached off course pull it done by wiping the surfaces with a clean lint up immediately with a quick motion and re free rag soaked with solvent and then wiping position properly the to evaporate with a clean dry lint free rag Press or roll entire surface o...
Page 149: ...ly 2 Upper Rudder Hinge 3 Center Rudder Hinge 4 Lower Rudder Hinge 5 Bolt 6 Washer 7 Nut 2 8 Bolt 9 Fairing Detail A NOTE Attach Bolt Torques 70 100 inch lbs 140 225 inch lbs Detail B 5 7 7 S 6 Detail C Detail D Figure 4 3 Vertical Fin Revision 1 4 7 ...
Page 150: ... boots 1 Nutplate 7 Bracket 13 Upper Left Fairing 2 Washer 8 Bolt 14 Abrasion Boot 3 Bolt 9 Elevator Pylon Bracket 15 Lower Left Moulding 4 Bracket 10 Elevator Inboard Hinge 16 Lower Right Moulding 5 Nut 11 Elevator Outboard Hinge 17 Forward Left Fairing 6 Washer 12 Upper Right Fairing 18 Forward Right Fairing Figure 4 4 Horizontal Stabilizer 4 8 Revision 1 ...
Page 151: ...g Bungee 112 5 28 McCAULEY Two piece Wheel Description 1I2 5 28 Disassembly 1H4 5 8 Removal 182 1I2 5 28 Inspection Repair 1H5 5 9 Installation 182 112 5 28 Reassembly 1H5 5 9 Removal T182 thru Installation 1H5 5 9 18268055 1135 29 Removal of Main Wheel Axle 1H13 5 15 Installation T182 thru Installation of Main Wheel 18268055 1I3 5 29 Axle 1H13 5 15 Removal T182 Beginning Alignment 1H13 5 15 with ...
Page 152: ...brake lines are routed through it becomes free swiveling up to a maximum travel of the fairings to each main wheel Brake fairings and 30 degrees right or left of center Through use of the main wheel speed fairings am installed on these air brakes the aircraft can be pivoted about the outer craft Disc type brakes and tube type tires are in wing strut fitting A speed fairing is installed on the nose...
Page 153: ...below gear forging with lacquer thinner h Using a punch drive attaching pin 2 upward i Allow the adhesive to cure thoroughly according out of inboard forging 26 to the manufacturer s recommendations before flex i Pull strut outboard of forgings 24 and 26 ing the strut or applying loads to the step j Paint the strut and step bracket after curing NOTE is completed To replace bushing from outboard fo...
Page 154: ... A surfaces only INBOARD Apply Y8560 Polyurethane tape 3M Co St Paul Minnesota where fairing 6 will cause chafing 1 Snap Ring 10 Fitting 17 Cotter Pin 24 Outboard Forging 2 Strut Attach Pin 11 Shim 18 Hub Cap 25 Plug Button 3 Upper Fairing 12 Axle 19 Back Plate 26 Inboard Forging 4 Brake Line 13 Torque Plate 20 Brake Cylinder 27 Cover Plate 5 Step Tread 14 Lower Fairing 21 Bracket 28 Spacer 6 Stru...
Page 155: ...ANUAL Detail A BEGINNING WITH 18265391 1 Doubler 6 Mounting Plate 2 Speed Fairing 7 Axle 3 Scraper 8 Torque Plate 4 Axle Nut 9 Access Door 5 Stiffener 10 Plug Button Figure 5 2 Main Landing Gear Fairing Revision 1 5 5 Revision 1 5 5 ...
Page 156: ...ular gear strut See figure 5 4 6 Reverse the preceding steps to install tubu lar gear strut fairing 5 15 DESCRIPTION The aircraft may be equipped with either Cleveland or McCauley two piece wheel 5 12 MAIN WHEEL SPEED FAIRING REMOVAL and tire assemblies or McCauley three piece with See figure 5 2 hub and capscrews wheel and tire assemblies Sep a Remove wheel brake fairing item 14 figure 5 1 arate ...
Page 157: ... fit in the wheel brake disc in the inner wheel half using the thru halves and should not be removed unless new bolts to guide the disc Assure that brake disc is bearing cups are to be installed To remove seated in wheel half bearing cup heat wheel half in boiling water b Insert tube in tire aligning index marks on tire for 15 minutes Using an arbor press if and tube available press out the bearin...
Page 158: ...ners into wheel hub NOTE The bearing cups are a press fit in the wheel Grease seal retainer hub and should not be removed unless a new seal retainers inboard 12 are not inter part is to be part is to be installed To remove the bear ing cup heat wheel hub in boiling water for are 30 minutes or in an oven not to exceed 121 C Grease seal retainer outboard 2 grease 250 F Using an arbor press if availa...
Page 159: ...e failure of the bolts with re hardened grease dust or dirt sultant wheel failure b Inspect wheel halves 6 for cracks or damage f Prior to torquing nuts 10 inflate tube with c Inspect bearing cones 5 cups 27 retaining approximately 10 15 psi air pressure to seat tire rings 1 grease seal retainers 2 grease seal felts 3 and grease seal retainers 4 for wear or damage d Inspect thru bolts 24 and nuts ...
Page 160: ...7 6 Outer Wheel Half 17 Brake Bleeder 7 Tire 18 O Ring CLEVELAND WHEEL 8 Tube 19 Piston 1977 THRU 1980 9 Inner Wheel Half 20 Thru Bolt 10 Bearing Cup 21 Brake Lining 11 Brake Disc 22 Back Plate Figure 5 4 Main Wheel and Brake Assembly Sheet 1 of 4 SHOP NOTES 5 10 ...
Page 161: ... Tube 10 Wheel Hub 18 11 Bearing Cup Race 12 Inboard Grease Seal Retainer 22 13 Inboard Grease Seal Felt 2 14 Brake Disc 20 15 Torque Plate MC CAULEY WHEEL 16 Pressure Plate SERIAL 18265176 THRU 17 Anchor Bolt 18265328 n 18 Brake Cylinder 182619 19 Bleeder Valve 0 20 O Ring Piston 21 Brake Piston 22 Brake Lining 23 Capscrew 24 Back Plate Figure 5 4 Main Wheel and Brake Assembly Sheet 2 of 4 5 11 ...
Page 162: ...sher 1112 10 Nut 11 Brake Disc 13 12 Torque Plate 13 Pressure Plate 14Out 14 Anchor Bolt 15E Elbow 15 1 a Brake Cylinder 263 of 5 1217 Bolt Bol 18 Bleeder Screw 19 Dust Cover 20 Bleeder Fitting 25 21 Piston 0 Ring 4 22 Brake Piston 23 23 Lining 24 Thru Bolt 25 Washer 22 17 26 Pressure Plate Outboard 21 1 27 Bearing Cup 20 TORQUE TO 100 110 IN LB 18 TORQUE TO 80 90 IN LB 19 Figure 5 4 Main Wheel an...
Page 163: ...13 Pressure Plate 14 Anchor Bolt 15 Elbow 16 Brake Cylinder 17 Bolt 18 Bleeder Screw 19 Dust Cover 20 Bleeder Fitting 21 Piston O Ring 22 Brake Piston 23 Lining 24 Thru Bolt 13 25 Washer 14 26 Pressure Plate Outboard 21 27 Bearing Cup TORQUE TO 100 110 IN LB TORQUE TO 80 90 IN LB 24 MC CAULEY WHEEL BEGINNING WITH 1981 MODELS 21 Figure 5 4 Main Wheel and Brake Assembly Sheet 4 of 4 Revision 1 5 12A...
Page 164: ...gainst outboard flanges of wheel NEGATIVE CAMBER POSITIVE CAMBER 7 CARPENTER S SQUARE P FORWARD INBOARD STRAIGHTEDGE NOTE Setting toe in and camber within these tolerances while the cabin and fuel tanks are empty will give approximately zero toe in and zero camber at gross weight Ideal setting is zero toe in and zero camber at normal operating weight Therefore if normally operated at less than gro...
Page 165: ... 028 2046 DOWN FWD 028 2 46 DOWN AFT 006 2 44 0441139 5 UP FWD 125 0010 UP AFT 117 0 25 DOWN FWD 117 025 DOWN AFT 125 0010 0441139 6 UP FWD 253 0 21 UP AFT 235 0 51 DOWN FWD 235 0 51 DOWN AFT 253 0 21 0541157 3 AFT 12 _ 007 FWD 12 007 1241061 0441139 6 05411 0457 0441139 6 0 0 0 1 1 0 0441139 5 1 1 I 2 1 1157 1 0 1 1 2 2 0 0541157 3 0 0 1 2 1 Max number of shims SHIM NO to be used with shims in co...
Page 166: ...the tire is marked with a red dot on the tire sidewall and the heavy weight point of the tube is marked with NOTE a contrasting color line usually near the inflation valve stem When installing a new tire place these When removing axle from strut attach fitting marks adjacent to each other If a wheel becomes note number and position of wheel alignment unbalanced during service it may be statically ...
Page 167: ...alternate method of removal was used nose gear described in the note in the preceding para d Remove air filler valve core and deflate strut graph reversal of removal procedures will completely and telescope strut to its shortest length have to be followed forging Be sure the strut is deflated completely b Install four bolts attaching lower forging to fuse before removing bolt at top of strut lage ...
Page 168: ...arrel l t between torque link attachment 7ll 0H Xliil fittings showing or approximately 2 30 inch after bouncing De 13 viation from these dimensions are cause to check and service the strut A MAXIMUM EXTENSION 1 Bolt 1 Bolt 4 85 15 I 2 Bolt 3 Upper Forging 4 Bolt 5 Upper Strut 6 Steering Bungee 7 Lower Forging 8 Upper Torque Link 9 Bolt 10 Lower Torque Link 11 Torque Link Fitting 12 Nose Gear Fork...
Page 169: ...tated Back off nut to the tow bar spacers 2 to strut nearest castellation and install cotter pins e Slide speed fairing up and remove nose wheel d If shock strut was deflated service after installa Loosen scraper as necessary tion has been completed Refer to servicing instruc f Rotate speed fairing 90 degrees and work fairing tions in Section 2 down over the fork to remove e Adjust wheel scraper c...
Page 170: ...ube c Place wheel half 6 into tire and tube side op posite valve stem aligning base of valve stem in valve slot With washer 5 under head of thru bolt Serious injury can result from attempt 8 insert bolt through wheel half 6 ing to separate wheel halves with tire and d Place wheel half 6 into other side of tire and tube inflated tube aligning valve stem in valve slot e Install washers 5 and nuts 4 ...
Page 171: ...ns gear shock strut after it has been removed given in paragraph 5 13 from the aircraft and the speed fairing and the nose wheel have been removed In many 5 43 WHEEL BALANCING Since uneven tire wear cases separation of the upper and lower is usually the cause of wheel unbalance replacing the strut will permit inspection and parts in tire will probably correct this condition Tire and stallation wit...
Page 172: ...se parts is not recommended except for installation of Hydraulic fluid will drain from strut as lower new parts strut is pulled from upper strut m Remove retaining ring securing steering arm g Use a straight sharp pull to separate upper and assembly on upper strut Remove steering arm lower struts Invert lower strut and drain remaining shims and washer hydraulic fluid n Push orifice support from up...
Page 173: ...ction B B 21 7 Valve 13 Lower Strut 24Link 2 R Ring 14 Packing 2Support Ring Rg2 3 Orifice Piston Support 15 Scraper Ring 4 UpperStrut 16 Retaininng25 Forki 5 Decal 17 Lock Ring 26 Bolt o e 23 6 Steering Torque Arm 18 Nut 27 Bolt 7 Screw 19 Nut 28 Torque Link Fitting 8 Retaining Ring 20 Metering Pin 29 Back Up Ring 9 Steering Collar 21 O Ring 30 O Ring 10 Washer 22 Base Plug 31 O Ring 11 Lock Ring...
Page 174: ... BracketI 6 Nose Gear Drag Fitting 7 Drag Link 8 LH Gear Panel Wall 9 Stop Support 10 Stop Bolt HIMS i I 5 inches 4 If loose pivot bolts are found during routine inspection refer to Service Letter SE82 37 for parts list and I instructions for replacement of bolts and bushings Serial Effectivity 18267717 THRU 18268182 B B Figure 5 10 Nose Gear Shock Strut Assembly Model T182 5 23 ...
Page 175: ...asher 14 Race 39 Upper Torque Link 5 Bearing 15 Gasket 40 Centering Block 6 Bearing 16 Head and Tube Assembly 41 Squat Switch 7 Actuator Attach Fitting 17 O Rng 42 8 Shimmy Dampener 18 Barrel Assembly 43 Lower Torque Link Attach Clamp19 Collar Assembly 4 Bushing 9 Shimmy Dampener 20 Snap Ring 45 Spacer Attach Clevis Bolt 21 Gasket 46 Attach Clevis Bolt 21 Gasket 46 Pivot Bolt 10 Trunnion22 Back Up...
Page 176: ...from strut in upper strut 4 c Remove torque links 39 and 43 e Install O ring 24 and metering pin 20 with O d Remove bellcrank 1 collar 2 and valve 3 ring 21 in base plug 22 secure with nut from top of strut assembly e Remove flat snap ring 20 and collar 19 from NOTE lower end of outer barrel 18 f Remove wire lock ring 28 from groove at upper If base plug is to be replaced new part will end of lowe...
Page 177: ...semblies c Tighten nuts 7 snugly then tighten to align next 5 52 TORQUE LINKS See figure 5 12 castellation with cotter pin hole in bolt d Check upper torque link 6 and lower torque link 5 53 DESCRIPTION Torque links keep the lower 9 for looseness If looseness is apparant remove strut aligned with the nose gear steering system but nuts 7 and bolts and install washers 3 as necessary permit shock str...
Page 178: ...PER MODEL 182 See figure 5 13 SHIMMY DAMPER MODEL T182 See figure Refer to figure during disassembly and assembly of 5 13A Refer to figure during disassembly and re shimmy damper During reassembly install all new assembly of shimmy damper During reassembly in O rings Lubricate all parts with clean hydraulic stall all new packings back up rings and O rings fluid When damper is completely assembled ...
Page 179: ... seal the fuselage entrance of the steering bun bungee assembly is connected to the steering bell gee A sprocket operated screw mechanism to pro crank on the nose gear strut by a bearing end assem vide rudder trim is incorporated at the aft end of the bly and to the rudder bar assembly by a barrel nut bungee Refer to Section 10 of this manual for the and two snap rings rudder trim system 5 68 REMO...
Page 180: ...de in determining system component b Connect rod end assembly 6 to rudder bar relationship and for removal and installation of sys assembly 7 ter components c Connect bearing end assembly 3 to steering bellcrank 2 on nose gear strut 5 75 RIGGING OF NOSE WHEEL STEERING SYS TEM Since the nose wheel steering system is 5 72 REMOVAL Model T182 beginning with directly connected to the rudder control sys...
Page 181: ...e Wheel Steering System Model T182 5 30 3 Bearing End Assembly 10 Boot 4 Retainer 11 Barrel Nut 5 Clamp 12 SnapRing 6 Rod End Assembly 13 Flex Shaft 7 Rudder Bar Assembly 14 Pin If loose pivot bolts are found during routine inspections refer to Service Letter SE 82 37 for parts list and instru ctions for replacement of bolts and bushings Serial effectivity T18267716 Thru T18268182 Figure 5 15 Nose...
Page 182: ... clearance per paragraph O seal and piston 5 84 Internal damage to hose and O rings Replace damaged parts Flush due to use of wrong type of hydrau system with denatured alcohol Fill lic fluid and bleed brake system Pressure leak in system Tighten connection repair or replace faulty parts Brake linings worn out Replace linings Oil or grease on brake linings or Clean linings with carbon tetrachlo ne...
Page 183: ...g and drill 1 16 hole 30 from vertical if plug is not vented DO NOT DAMAGE LOCK O SEAL 16 15 THRU 18266590 ASSEMBLY OF PISTON 1 Clevis 7 Body 13 Piston Spring 2 Jamb Nut 8 Reservoir 14 Piston 3 Piston Rod 9 O Ring 15 Lock O Seal 4 Cover 10 Cylinder 16 Compensating Sleeve 5 Setscrew 11 Piston Return Spring 17 Filler Plug 6 Cover Boss 12 Nut 18 Screw Figure 5 16 Brake Master Cylinder Sheet 1 of 2 5 ...
Page 184: ...ed so 4 Cover pressure cannot build up in the 5 Piston reservoir during brake operation 6 Back up Ring Remove plug and drill 1 16 hole 7 Packing 30 from vertical as shown in 8 Spring view A A if plug is not vented L 1 9 Cylinder Body BEGINNING WITH 18266591 Figure 5 16 Brake Master Cylinder Sheet 2 of 2 5 33 ...
Page 185: ...exible hose used at the brake piston spring 13 into piston and slide assembly up mater cylinders A separate line is used to connect on bottom threaded portion of piston rod 3 each brake master cylinder to its corresponding c Run nut 12 up threads to spring 13 Tighten wheel brake cylinder nut 12 enough to obtain 0 040 0 005 inch clearance between top of piston and bottom of Lock O Seal as shown in ...
Page 186: ...y Bleeding with a clean hydraulic pressure 5 97 INSTALLATION OF WHEEL BRAKE source connected to the wheel cylinder is a Place brake assembly in position with pressure recommended plate in place a Remove brake master cylinder filler plug and NOTE screw flexible hose with appropriate fitting into the filler hole at the top ofthe brake master cylinder If torque plate was removed install as the b Imme...
Page 187: ...i i F re 5 17 PkiDe Brake System B Figure 5 17 Parking Brake System THICKNESS CESSNA WHEEL NO CLEVELAND NO McCAULEY NO DISC NO MINIMUM ORIGINAL ALLOWABLE C163001 0104 40 113 164 04000 0 218 0 205 C163002 0101 D 30063 B 30007 0 218 0 190 C163003 0102 D 30580 B 30195 0 218 0 190 C163004 0104 D 30291 6 B 30440 0 218 0 190 C163005 0101 D 30600 1 C 30615 1 0 218 0 190 C163006 0101 D 30600 1 C 30615 1 0...
Page 188: ... full stop braking ap guide during removal and installation ofcomponents plications from 30 to 35 knots Do not allow the brake discs to cool substantially between stops 5 105 INSPECTION AND REPAIR OF SYSTEM COMPONENTS Inspect lines for leaks cracks dents 5 102 PARKING BRAKE SYSTEM See figure chafing improper radius security corrosion deterio 5 17 ration obstructions and foreign matter Check brake ...
Page 189: ... control wheels 6 2 DESCRIPTION The aileron control system is to the ailerons 6 3 TROUBLE SHOOTING NOTE Due to remedy procedures in the following trouble shooting chart it may be necessary to re rig system refer to para graph 6 18 TROUBLE PROBABLE CAUSE REMEDY LOST MOTION IN CONTROL Loose control cables Check cable tension Adjust WHEEL cables to proper tension Broken pulley or bracket Check visual...
Page 190: ...te 10 at is mounted in a bearing block 21 on firewall 31 and instrument panel does not move fore and aft but rotates with the con trol wheel The four bearing roller assemblies 3 NOTE on the end of the control wheel tube reduce friction as the control wheel is moved fore and aft for ele To ease removal of control wheel tube assem vator system operation A sleeve weld assembly 5 bly 13 snap ring 9 ma...
Page 191: ...cer Detail C 4 Bushing 6 Turnbuckle Carry Thru iCAUTIONt 7 Bellcrank 8 Turnbuckle Direct MAINTAIN SPECIFIED CONTROL CABLE TENSION CABLE TENSION 40 LBS 10 LBS ON AILERON CARRY THRU CABLE AT AVERAGE TEMPER ATURE FOR THE AREA REFER TO FIGURE 1 1 FOR TRAVEL Figure 6 1 Aileron Control System 6 3 2 2 4 Bushing ...
Page 192: ...terconnect Cable Adjustment Terminal 16 28 Roll Pin 17 A 0 002 MAX 29 Interconnect Cable PER SIDE 30 Interconnect Cable 1 AA Turnbuckle VIEW A A 31 Firewall 32 Washer 18 18 33 Retainer 34 Adjustment Nut 21 22_ J 17 2 S 22 i 2 24 20 29 0 26 4 2723 28 Y NOTE x 2 S C r 3 F Used only on aircraft 25 NOTE equipped with single controls Allow 0 030 minimum _ 15 Washers 32 are of clearance between bear 5 W...
Page 193: ... 39 Terminal Block 2 41 42 43 44 40 Map Light Assembly 41 Pad 49 45 4637 48 35 36 13 40 NOTE Torque bolt 50 to 30 pound inches 3 00 50 THRU 1977 MODEL YEAR 42 Mike Switch 42 43 Plug 36 44 Insulator 45 45 Plug 46 Bracket 47 Cable 52 48 Setscrew 49 NEutchen 50 Bolt 2 51 Knob 52 Escutcheon 38 49 13 50 46 40 BEGINNING WITH 1978 MODEL YEAR Figure 6 2 Control Column Installation Sheet 2 of 2 6 5 ...
Page 194: ... Section 2 for lubrication re 12 Using care pull control tube assembly 15 quirements aft and remove quadrant 24 13 Reverse the preceding steps for reinstalla 6 8 AILERON BELLCRANK See figure 6 3 tion Safety wire all items previously safetied check rigging of aileron and elevator control systems 6 9 REMOVAL and rig if necessary in accordance with paragraph a Remove access plate inboard of each bell...
Page 195: ...to Service Letter SE83 18 for specific serials effected 1 Remove cotter pins 5 from both ends of hinge 1 2 Push drill rod 7 or number 43 drill bit into hinge pin hole beyond holes from which cotter pins 5 were removed 3 Bend one leg of cotter pin 5 back and attempt to install the other leg past drill rod 7 or number 43 drill bit If leg of cotter pin 5 GOES replace hinge 7 If NO GO condition exists...
Page 196: ...d install access b Install brass washers 11 between lower end of plates fairings and upholstery removed in step a bellcrank 8 and wing structure to shim out excess clearance 6 14 AILERONS See figure 6 3 c Install bellcrank pivot bolt 4 d Position bellcrank stop bushing 7 and install 6 15 REMOVAL attaching bolt 6 a Disconnect push pull rod 12 at aileron e Connect control cables to bellcrank b Remov...
Page 197: ...e safety wire and relieve cable tension at h Remove bar from control wheels and check de turnbuckles 6 and 8 gree of travel as specified in figure 1 1 If travel is b Disconnect push pull rods at bellcranks 7 not within specified limits readjust push pull rods c Adjust interconnect cable turnbuckle index 30 and cables as necessary figure 6 2 and adjustment terminals index 27 fig i Ensure all turnbu...
Page 198: ... cables and push pull rods c With flaps full UP mount an inclinometer on one Electrical power to the motor is controlled by two flap and set to 0 Lower flaps to full DOWN position microswitches mounted on a floating arm assembly and check flap angle as specified in figure 1 1 Check by a camming lever and a follow up control As the approximate mid range percentage setting against flap control lever...
Page 199: ...e Follow up control dis Secure control or replace connected or slipping if defective BINDING IN SYSTEM AS FLAPS Cables not riding on pulleys Open access plates and observe ARE RAISED AND LOWERED pulleys Route cables correctly over pulleys Bind in drive pulleys Check drive pulleys in motion Replace drive pulleys found defective Broken or binding pulleys Check pulleys for free rotation or breaks Rep...
Page 200: ...9 Rub Strip 10 Turnbuckle 11 Retract Cable f 12 Direct Cable NOTE 2 4 Detail C ICAT Shaded pulleys used in MAINTAIN SPECIFIED CONTROL this system only CABLE TENSION CABLE TENSION 30 LBS 10 LBS AT AVERAGE TEMPER ATURE FOR THE AREA REFER TO FIGURE 1 1 FOR TRAVEL Figure 7 1 Wing Flap Control System 7 3 2 ietal n 4 il o 4l ShddplesseE AI IE 9 i sy e CA L T i AL 4 3 VRG 7 HE ARE EFE R o o OR VE gur oto...
Page 201: ... electrical leads at quick dis brass washer between drive pulley and wing structure connects for use on reinstallation Tape open ends of drive h Disconnect wiring at limit switches 23 and 26 pulley after removal to protect bearings i Carefully work assembly from wing through ac h To remove left wing drive pulley use this same cess opening procedure omitting step d j Reverse preceding steps for rei...
Page 202: ...ransmission Assembly 8 Electrical Wiring 9 Motor Assembly 11 Bolt 12 Cable Lock 13 Drive Pulley 14 Push Pull Rod 15 Attach Bracket 16 Bolt 17 Direct Cable 18 Retract Cable 19 Bolt 20 Bolt 21 Set Screw 22 Switch Adjustment Block 23 Up Limit Switch UP position 24 Switch Actuating Collar 25 Support 26 Down Limit Switch 27 Nut NOTE Use Locktite No 601 or equivalent Figure 7 2 Flap Motor and Transmissi...
Page 203: ... 871 STA LOK Catalog 21 I mS 12 0 No 800 or equivalent to threads of flap lever 16 e 14 Install knob 15 and allow Lootito to C 154 cure from five to 20 minutes before service 30 29 2224 25 3 l r 13 L Detail D NOTE Torque clamp nut 8 to O2 B Sit j 40 50 inch pounds and 18 Turbuckle lock with second nut 19 Spring i U 19 Sprlng 27 7 Clamp Bar 20 Arm Assembly 8 Clamp Nut 21 Position Indicator I 9 Bolt...
Page 204: ...provide adequate flap clearance at wing root flap well skin and aileron Some lat eral movement of flap is inherant due to the width of rollers This movement should be considered when positioning spacers and direction of bolts Detail A 6 Detail B Detail C NOTE 1 Cover Plate 2 Flap Support Beginning with Serial 18268475 cover plates 1 3 Roller Assembly are attached to flaps with recessed head screws...
Page 205: ...eys as necessary to work cables nected before installing cables If drive free of aircraft pulleys 13 are not installed attach control cables before installing drive pulleys in the wings as illustrated in figure 7 5 NOTE e The 3 32 inch retract cable connects to the for To ease routing of cables a length of wire ward side of the right drive pulley and to the aft side may be attached to the end of c...
Page 206: ...f as turnbuckles are connected NOTE n With flaps full UP adjust turnbuckles to obtain 30 10 pounds tension on cables Adjust retract cable Apply Loctite grade CV sealant to threads of first setscrew 6 and torque to 40 inch pounds NOTE If actuating tube 5 is too long to allow attachment to drive pulley after completion of step g proceed to Ensure cables are positioned in pulley grooves step h and ca...
Page 207: ... position indicator at 0 flaps g With control lever 14 in full up position adjust NOTE switches 23 and 25 in slotted holes until cam 13 is centered between switch rollers Be sure control Flap travel on UP cycle may deviate a maxi lever 14 is in full up position during this adjustment mum of 4 from indicated position h Mount an inclinometer on trailing edge of one flap and set to 0 Turn master swit...
Page 208: ... in the tailcone A push pull tube con 8 2 DESCRIPTION The elevators are operated by nects this bellcrank to the elevator arm assembly in power transmitted through fore and aft movement of stalled between the elevators An elevator trim tab the pilot or copilot control wheels The system is is installed in the trailing edge of the right elevator comprised of control columns an elevator torque and is ...
Page 209: ...ara PRESCRIBED TRAVEL graph 8 14 Cables tightened unevenly Rig in accordance with para graph 8 14 Interference at instrument Rig in accordance with para panel graph 8 14 8 4 CONTROL COLUMN See figure 6 2 e Using care remove elevator Section 6 outlines removal installation and repair of f To remove left elevator use same procedure control column omitting step b 8 5 ELEVATORS See figure 8 2 8 7 REPA...
Page 210: ...10 00 T CAUTION r l 1 2 3 NOTE MAINTAIN SPECIFIED CONTROL CABLE TENSION DelD Shaded pulleys used in Detail D this system only CABLE TENSION 30 LBS 10 LBS AT AVERAGE TEMPER ATURE FOR THE AREA REFER TO FIGURE 1 1 FOR TRAVEL Figure 8 1 Elevator Control System 8 3 AL IO ealDSae uly sdi m only C BL TESO 3 ATAERGETMP TR O TEAE t EE OFGR V igre8 El to Coto i 8 ...
Page 211: ... Push Pull Tube 12 Bolt 13 Bolt 14 Bolt Detail A 15 Hinge Bracket Detail B 14 8 12 NOTE 9 Refer to Section 9 for trim tab control system 11 Detail C Detail D Figure 8 2 Elevator Installation 1 UP Elevator Cable 13 s s 3 S 5 9 Push Pull Tube 6I 3 r o o 10 Pivot Bolt 4 2 12 t 11 Bushing 4 12 12 Bearing 6 13 DOWN Elevator Cable Figure 8 3 Elevator Bellcrank Installation 8 4 ...
Page 212: ...imately 1 of elevator travel TO ELEVATOR DOWN CABLE Figure 8 4 Elevator Bellcrank Travel Stop Adjustment Press fit 3 46 inch 30 inch 1 Support Detail A 2 Neutral Rigging Tool 3 Instrument Panel 4 Pilot s Control Column Fabricate from 0 125 steel plate 0 209 dia drill rod for short pin and 0 250 dia drill rod for long pin according to dimensions shown Figure 8 5 Control Column Neutral Position Rigg...
Page 213: ...rse the preceding steps for reinstallation face travel is available from the Cessna and reinstall all items removed for access Supply Division See figure 6 4 8 12 CABLES AND PULLEYS See figure b Lock control column in neutral position per 8 1 figure 8 5 c Adjust bellcrank stop blocks 7 at brackets 8 8 13 REMOVAL AND INSTALLATION to degree of travel specified in figure 1 1 Position a support stand ...
Page 214: ... adjacent to the trim wheel indicates tab cated on the trailing edge of the right elevator is position A nose up setting results in a tab down controlled by a trim wheel mounted in the pedestal position An electric trim assist system may also be Power to operate the tab is transmitted from the installed This system is described in paragraph 9 20 9 3 TROUBLE SHOOTING NOTE Due to remedy procedures i...
Page 215: ...guard 20 and disengage chain should not be necessary after installation from actuator sprocket 21 of tab e Remove screws attaching clamps 22 to bracket 19 and remove actuator 6 through access opening b Drill out rivets securing trim tab hinge to ele f Reverse the preceding steps for reinstallation vator and remove trim tab Rig system in accordance with paragraph 9 18 safety turnbuckle and reinstal...
Page 216: ...0 Turnbuckle 7 A s 12 11 Bulkhead Station 21 00 r SHE 2 Cable Guard 4 2 y iBulkhead Station 110 00 1 8 Travel Stop 4 011 CONTROL CABLE TENSION NOTE CABLE TENSION 10 TO 15 LBS AT AVERAGE TEMPER Detail E Shaded pulleys are used ATURE FOR THE AREA for this system only REFER TO FIGURE 1 1 FOR TRAVEL Figure 9 1 Elevator Trim Tab Control System Sheet I of 2 9 3 ...
Page 217: ...al Structure 21 Sprocket 26 Horn sembly 7 Trim Tab 17 Trim Wheel 22 Clmp 27 Roller Chain 13 Retainer 18 Pedestal Cover 23 Stabilizer Rear Spar 28 Sprocket 14 Bearing 19 Support Bracket 24 Brace 15 Trim Indicator 20 ChainGuard 25 Push Pull Tube Figure 9 1 Elevator Trim Tab Control System Sheet 2 of 2 9 4 9 4 ...
Page 218: ...ng in Soddard solvent or equivalent Do not g Check bearing 16 for smoothness of operation clean sealed bearing 16 h DO NOT attempt to repair damaged or worn c Inspect all component parts for obvious indica parts of the actuator assembly Discard all defec tions of damage such as stripped threads cracks tive items and install new parts during reassembly deep nicks and dents d Check bearings 6 and 14...
Page 219: ...l acuator assembly in 9 11 TRIM TAB FREE PLAY INSPECTION Position a support stand under the tail a Place elevator and trimtab in neutral position tie down ring toprevent tailcone from and secure elevator from movement dropping while working inside b Determine m imum amount of allowable free play using procedures shown in figure 9 2A b Remove travel stop blocks 8 from control c Using moderate hand ...
Page 220: ...TAL FREE PLAY 1 Measure chord length at extreme inboard end of trim tab as shown in detail A 2 Mulitiply chord length by 0 025 to obtain maximum allowable free play 3 Measure free play at same point on trim tab that chord length was measured 4 Total free play must not exceed maximum allow able See detail B Figure 9 2A Trim Tab Free Play Inspection SHOP NOTES 9 7 ...
Page 221: ... of trim 9 18 RIGGING See figure 9 1 wheel is where further movement is pre vented by the chain or cable ends contact ICA UTION H ing sprockets or pulleys Position a support stand under the tail tie down ring to prevent tailcone from dropping while working inside f With elevator and trim tab both in neutral streamlined mount an inclinometer on tab and set a Remove rear baggage compartment wall and...
Page 222: ...y and a chain connecting the c Remove chain guard 10 from tab actuator drive assembly to an additional sprocket mounted on d Remove mounting bolts from drive assembly and the standard elevator trim actuator The electric actuator and remove units from the aircraft drive assembly includes a motor sprockets and a e Reverse preceding steps for reinstallation chain driven solenoid type adjustable clutc...
Page 223: ...eaker F ure El ric Trim Installation Shet of 9 10 D10ail C a Dt ai 1 17 BEGINNI 197 416 I Sabilc zeric rmDetail A 18 Coiruit Breaketr 6 TbctTrim Tab s 1 7 Clamp 8 Drive Chain 9 Turnbuckle 10 Chain Guard 11 Support 12 Cover 14 Connector 12 15 Switch Disengage B 16 SSwitch Pitch Trim 13 17 Control Wheel 18 Circuit Breaker Figure 9 4 Electric Trim Installation Sheet 1 of 2 9 10 ...
Page 224: ...ainst inside nut wiring far enough to expose the clutch assembly o Connect electrical wiring removed in step 3 f Ensure the electric trim circuit breaker on the and reinstall drive assembly in aircraft pedestal cover is pushed in and place master switch p Rerig trim system in accordance with paragraph in ON position 9 24 and reinstall all items removed for access g Place disengage switch 15 in ON ...
Page 225: ...leading to the motor assembly approximately 5 minutes if several actua d Connect one lead of a dc voltmeter capable of tions of the motor becomes necessary dur measuring the aircraft voltage to either the RED or ing adjustment BLACK wire leading to the motor and the other volt meter lead to a good aircraft ground i Readjust voltage regulator as required to obtain e Operate the electric trim switch...
Page 226: ...rouble Shooting 1L14 10 8 Repair L12 10 6 Rigging 1L18 10 12 10 1 RUDDER CONTROL SYSTEM See prised of the rudder pedals installation cables and figure 10 1 pulleys all of which link the pedals to the rudder and nose wheel steering 10 2 DESCRIPTION Rudder control is maintained through use of conventional rudder pedals which also control nose wheel steering The system is com 10 3 TROUBLE SHOOTING NO...
Page 227: ...INSTALLATION a Remove carpeting shields and soundproofing The two inboard bearing blocks contain clear from the rudder pedal and tunnel areas as necessary ance holes for the rudder bars at one end and for access b Disconnect brake master cylinders 15 and ing blocks for reference on reinstallation parking brake cables at pilot s rudder pedals c Remove rudder pedals 2 and brake links 5 h Reverse the...
Page 228: ...ion 209 00 SEE A 12 Bulkhead Station 110 00 SEE FIGURE 10 5 NOTES Only shaded pulleys are used in this system 2 Trim cotter pin 6 at rudder n L bellcrank 9 to clear elevator torque tube in UP position DO NOT cut pin too short 1 t 2 DetailC 1 2 al iCAUTION MAINTAIN SPECIFIED CONTROL CABLE TENSION CABLE TENSION 30 LBS 10 LBS AT AVERAGE TEMPER Detail D ATURE FOR THE AREA REFER TO FIGURE 1 1 FOR TRAVE...
Page 229: ... HOLE AFT 1 Anti Rattle Spring 2 Pedal 3 Shaft 4 Spacer 5 Brake Link 6 Right Forward Cable 7 Left Forward Cable 15 8 Rudder Bar Arm For wiffletree push pull rod attachment 13 9 Aft Rudder Bar 10 Bearing Block 11 Rudder Bar Arm For wiffletree push pull rod attachment THRU 18268101 12 Forward Rudder Bar 13 Bracket 18268102 14 Brake Torque Tube 15 Master Cylinder 16 Bearing 17 Bellcrank 4 18 Single C...
Page 230: ...MODEL 182 T182 SERIES SERVICE MANUAL 8 10 D 12 D Detail C vmE D D is B LMODEL T182 Figure 10 2 Rudder Pedals Installation Sheet 2 of 2 10 5 ...
Page 231: ... rudder supported remove all hinge bolts and using care lift rudder free of vertical fin 10 10 REMOVAL AND INSTALLATION f Reverse the preceding steps for reinstallation a Remove seats upholstery and access plates as Rig system in accordance with paragraph 10 11 necessary safety turnbuckles and reinstall all items removed b Relieve cable tension at turnbuckles 10 and dis for access connect cables c...
Page 232: ...outed through structure then 5 Clamp rudder pedals in neutral position and cen attach cable being installed and pull the cable ter wiffletree 14 by adjusting push pull rods 12 into position Wiffletree is centered when the bolts in each end are the same distance from the bulkhead just forward of e Reverse the preceding steps for reinstallation the wiffletree Tighten jam nuts f After cable is routed...
Page 233: ...steering bungee adjustable rod end 21 from rudder bar arm 17 are interconnected Adjustments to any one 4 Remove fairing from either side of vertical fin remove safety wire and relieve cable tension at than rigging refer to Section 5 turnbuckles index 10 figure 10 1 5 Clamp rudder pedals in neutral position ad just turnbuckles index 10 figure 10 1 to specified tension with the rudder offset one deg...
Page 234: ...00103 A 20 A 13 NOTE I Dimension is applicable to aircraft utilizing stops 27 7 ONLY 25 V A 3 v A1 4 A 26 Detail B ROTATED 900 14 Wiffletree Bellcrank 16 ROTATED 90 15 Spacer 16 Steering Bungee 19 17 Chain Guard 18 Chain Guard Stop I 19 Steering Bungee Sprocket 20 Washer A 18 h 21 Cotter Pin 22 Pedestal Structure Detail C 1 17 23 Upper Bearing v 1 6 24 Lower Bearing 19 25 Idler Sprocket W AA 26 Ad...
Page 235: ... Universal Joint F 7 Pedestal Structure 8 Aft Trim Shaft Sprocket 9 Indicator 23 10 Upper Bearing 11 Lower Bearing 12 Rudder Trim Wheel s 24 22 Setscrew 24 Fairlead THRU 1981 MODELS T182 BEGINNING WITH 1982 MODELS T182 J T182 ONLY Detail A Figure 10 6 T 182 Rudder Trim Control System Sheet I of 2 10 10 I0 10 tcre ...
Page 236: ...rm 15 18 Clamp 19 Boot 20 Steering Bungee 21 Steering Bungee Rod End 23 Flex Shaft 25 Roll Pin 16 26 Retainer 27 Barrel Nut 20 Lubricate threads with MIL G 23827A before assembly l i l iI I 1 90inches i i 21 Detail B 2 60 VIEW C C _ __ 40 VIEW D D T182 ONLY D Figure 10 6 T 182 Rudder Trim Control System Sheet 2 of 2 10 11 ...
Page 237: ...m control wheel 4 until indicator 2 BEGINNING WITH 1982 MODELS is centered in pedestal slot neutral 8 After completing step 5 of paragraph 10 11 5 Without moving sprocket 19 engage chain on part b tie down or weight tail to raise nosewheel sprockets 9 and 19 free of ground 9 Extend strut and ensure nose gear is centered NOTE against external centering stop Refer to Section 5 10 With rudder pedals ...
Page 238: ...Up Procedures 2A12 11 10 Description 2A24 11 22 Removal 2A12 11 10 ENGINE FUEL SYTEM 2A24 11 22 Cleaning 2A14 11 12 Description 2A24 11 22 Accessories Removal 2A14 11 12 Carburetor 2A24 11 22 Inspection 2A14 11 12 Removal Installation 2A24 11 22 Build Up 2A14 11 12 Idle Speed and Mixture Installation 2A14 11 12 Adjustments 2A24 11 22 Flexible Fluid Hoses 2A15 11 13 INDUCTION AIR SYSTEM 2B1 11 23 L...
Page 239: ... the nose cap front provides access to the oil filler neck and one at c Release the quick release fasteners attaching the left aft side provides access to the oil dipstick the cowling to the fuselage and at the parting surfaces and remote strainer drain control Controllable cowl of the upper and lower segments flaps are attached to the trailing edge of the lower d Disconnect the landing and taxi l...
Page 240: ...th new parts Due to their small size new reinforcement angles e Repeat the preceding step for the opposite cowl are easier to install than to repair the damaged part flap f When cowl flaps are lowered they should be open 11 6 COWL FLAPS 13 3 1 measured with an inclinometer held against the cowl flap 11 7 DESCRPTION Cowl flaps are provided to g Check that ll clamps and jam nuts are tight aid in con...
Page 241: ...arvel Schebler MA4 5 Tachometer Mechnical Drive OilSump Capacity 12 US Quarts With External Filter 13 U S Quarts Oil Pressure PSI Normal 30 60 MinimumIdling 10 Maximum Cold Oil Starting 100 Connection Location Between No 2 and No 4 Cyl Oil Temperature Normal Operating Within Green Arc Maximum Red Line 240 F Probe Location Below Oil Cooler Cylinder Head Temperature Normal Operating Within Green Arc...
Page 242: ...d inadvertant over gines Refer to Continental Aircraft Engine Service speed occur refer to Continental Aircraft Engine Bulletin M80 22 and to any superseding bulletins Service Bulletin M75 16 and to any superseding revisions or supplements thereto for further recom bulletins revisions or supplements thereto for mendations At the time of overhaul engine acces further recommendations sories should b...
Page 243: ...p 5 Cowl Flaps 6 Clevis 7 Shock Mount 8 Bracket 9 Positlon Bracket 10 Clevis 11 Control Lever 12 Bushing 5 NOTE 2 Refer to Section 2 2 for Cowl Flap hinge 6 10 inspection frequency 2 8 1 y f7 B 9 p I 8 18268161 ON I 7 0 Detail C Detail B THRU 18268160 Figure 11 1 Cowl Flaps Installation 11 6 Revision 1 ...
Page 244: ...er plugged thoroughly Refer to paragraph 11 59 Vaporized fuel Most likely Refer to Pilot s Operating Handbook to occur in hot weather with a hot engine Engine flooded Refer to Pilot s Operating Handbook Water in fuel system Open fuel strainer drain and check for water If water is present drain fuel cell sumps lines strainer and carburetor Defective aircraft fuel system Refer to Section 12 Fuel con...
Page 245: ...leaks through primer repair or replace primer Leaking float valve or float Perform an idle mixture check level set too high Attempt to remove any rich indication with the idle mixture adjustment If the rich indica tion cannot be removed the float valve is leaking or the float level is set too high Re place defective parts reset float level Defective carburetor If engine will start when primed but ...
Page 246: ...epair is required Restricted carburetor air Check visually Clean in filter accordance with Section 2 Cracked engine mount Inspect and repair or replace mount as required Defective mounting bushings Inspect and install new bushings as required Propeller control in high Use low pitch high RPM pitch low rpm position position for all ground operations Fuel contamination Check all screens in fuel syste...
Page 247: ... firewall d If the average results of the RPM obtained are lower than stated above the following recommended NOTE checks may be performed to determine a possible deficiency Tag each item when disconnected to aid in 1 Check governor control for proper rigging identifying wires hoses lines and control It should be determined that the governor control linkages when engine is reinstalled Like arm trav...
Page 248: ...m the magnetos or spark 2 Disconnect oil breather and vacuum system plugs to prevent accidental firing oil separator vent lines where secured to the engine h Remove the spinner and propeller in accordance with Section 13 Cover exposed end of crankshaft flange and propeller flange to prevent entry of foreign Residual fuel and oil draining from discon material nected lines and hoses constitutes a fi...
Page 249: ...s not tagged for repair or replacement with new compo present on a particular engine installation nents a Hoist the engine to a point near the engine mount NOTE b Install engine shock mount pads and bonding straps as illustrated in figure 11 2 Items easily confused with similar items c Carefully lower engine slowly into place on the should be tagged to provide a means of engine mount Route control...
Page 250: ...bent excessively and during reinstalla inoperative tion to assure hose is returned to its original position e Refer to Advisory Circular 43 13 1 Chapter 10 3 Connect starter electrical cable at starter for additional installation procedures for flexible 4 Connect tachometer drive shaft at adapter fluid hose assemblies Be sure drive cable engages drive in adapter Hand tighten then torque 1 4 turn 1...
Page 251: ...e made as long as due to aging and deterioration Inspect the rubber strength and cooling requirements are met Replace pads for separation between the pad and metal backing sealing strips if they do not seal properly swelling cracking or a pronounced set of the pad Install new parts for all parts that show evidence of 11 31 ENGINE MOUNT See figure 11 2 wear or damage 11 32 DESCRIPTION The engine mo...
Page 252: ... Relief valve defective Remove and check for dirty or de fective parts Clean and install replace valve if defective LOW OIL PRESSURE Low oil supply Check with dipstick Fill sump with proper grade and quantity of oil Refer to Section 2 Low viscosity oil Drain sump and refill with proper grade and quantity of oil Oil pressure relief valve spring Remove and inspect spring weak or broken Replace weak ...
Page 253: ...ssages clogged Inspect cooler core Clean air passages Oil cooler oil passages clogged Drain oil cooler and inspect for sediment Remove cooler and flush thoroughly Thermostatic bypass valve Feel front of cooler core with hand damaged or held open by If core is cold oil is bypassing solid matter cooler Remove and clean valve and seat If still inoperative re place Low oil supply Check with dipstick F...
Page 254: ...ed by impacting abra 11 42 REMOVAL AND INSTALLATION See sion or pressure Evidence of internal figure 11 3 damage found in the oil filter element justifies further examination to determine NOTE the cause Filter element replacement kits are avail f Wash lid 7 hollow stud 1 and filter can 4 able from the Cessna Supply Division in solvent and dry with compressed air a Remove engine cowling in accordan...
Page 255: ...gaskets listed in the Parts Catalogs 12 11 10 9 f 13 14 SERIAL 18265176 THRU 18267041 F18200026 THRU Fl8200129 1 Hollow Stud 2 Metal Gasket 3 Safety Wire Tabs 4 4 Can 5 Filter Element 6 Lower Gasket 3 7 Lid 8 Upper Gasket 9 Adapter 10 Adapter Nut 11 O Ring 12 Bypass Valve 13 Plug 14 Thread Insert Figure 11 3 Full Flow Oil Filter 11 18 ...
Page 256: ...e adapter are open and free of torque to 20 25 lb ft 240 300 lb in using a torque foreign material Also check that bypass valve is wrench seated properly k Install all parts removed for access and service the engine with the proper grade and quantity of en gine oil One additional quart of oil is required each 11 46 INSTALLATION time the filter element is changed a Assemble adapter nut 10 and new O...
Page 257: ...bly in accordance with para NOTE graph 11 49 NOTE Teledyne Continental Motors recommends that the spin on filter be inspected Refer A special wrench adapter for adapter nut 2 to Continental Aircraft Engine Service Bulle Part No SE 709 is available from the tin M74 2 dated 16 January 1974 Cessna Supply Division or one may be fabricated as shown in figure 11 4 Remove d Before installing oil filter 6...
Page 258: ...arts Catalogs 2 1 O Ring 2 Adapter Nut 3 Adapter 4 Threaded Insert 5 Stud 6 Filter 7 Safety Wire 8 Filter Gasket 9 Plug SERIAL 18267042 ON F18200130 THRU F18200169 7 NOTE All 182 series aircraft Serial 18268294 and ON and all turbocharged 182 Series aircraft Serial 18267716 and ON are equipped with full flow oil filters Figure 11 5 Full Flow Oil Filter 11 21 ...
Page 259: ...ent should be accom plished after the engine has been warmed up Since idle RPM may be affected by idle mixture adjustment it may be necessary to readjust idle RPM after set 11 54 OIL COOLER ting the idle mixture correctly a Set the throttle stop screw idle RPM to obtain 11 55 DESCRIPTION A non congealing oil cooler 600 25 RPM with throttle control pulled full out may be installed on the aircraft T...
Page 260: ...ted to each cylinder by separate intake pipes The intake pipes are attached to the 11 66 INDUCTION AIR FILTER manifold with hoses and clamps and to the cylinder with a four bolt flange sealed with a gasket A butter 11 67 DESCRIPTION An induction air filter fly valve located in the airbox may be operated mounted at the induction air inlet on the front of the manually from the cabin to permit the se...
Page 261: ...isten for loud clicks as impulse couplings operate Remove magnetos and determine cause Replace defective magneto Defective magneto Refer to paragraph 11 78 Broken drive gear Remove magneto and check mag neto and engine gears Replace defective parts Make sure no pieces of damaged parts remain in engine or engine disassembly will be required ENGINE WILL NOT Spark plugs defective im Clean regap and t...
Page 262: ...n the engine or internal NOTE timing may be disturbed The sideof the magneto with the manu 11 75 REMOVAL facturer s insignia has a red timing mark a Remove engine cowling in accordance with para and the side opposite to the insignia has graph 11 3 a black timing mark viewed through the b Tag for identification and remove high tension vent plug holes The distributor gear wires from the magneto bein...
Page 263: ...d engine the engine has been placed in the correct firing posi j Connect spark plug leads to their correct mag tion install and time the magneto to the engine in the neto outlets following manner NOTE NOTE The No 1 magneto outlet is the one closest Install the magneto drive coupling retainer to the ventilation plug on the side of the and rubber bushings into the magneto drive magneto having the ma...
Page 264: ...t on the surface between the points and posits Breaker points may be cleaned with a hard the correct amount of spring pressure on the cam finish paper If breaker point assembly is defective The area on the points should be twenty five percent install a new assembly Make no attempt to stone or of the area making contact The spring pressure at dress the breaker points Clean new breaker points the ca...
Page 265: ...f plugs e Turn the switch to the L position and note the Some controls have intricate parts that will rpm drop then return the switch to the BOTH fall out and possibly be lost if the control is position pulled from the housing while it is discon f The rpm drop should not exceed 150 RPM on nected either magneto or show greater than 50 RPM differ ential between magnetos A smooth RPM drop off 11 83 R...
Page 266: ... CARBURETOR HEAT CONTROL f Release friction lock and check full travel of a Loosen clamp securing the control to the bracket arm on carburetor If further adjustment is re on the airbox quired make all adjustment at the carburetor end b Push control full in then pull it out approximate of control DO NOT change jam nut 3 setting ly 1 8 inch from panel for cushion g Tighten rod end locknuts at carbur...
Page 267: ...continuity Install new switch or wires Defective starter switch or switch Check continuity Install new circuit switch or wires Defective starter motor Check electrical power to motor Repair or replace starter motor STARTER MOTOR RUNS BUT Defective overrunning clutch Check visually Install new DOES NOT TURN CRANK or drive starter adapter SHAFT Starter motor shaft broken Check visually Install new s...
Page 268: ...reinstallation excessive arcing If the commutator is only slightly Install a new O ring seal on motor then install motor dirty glazed or discolored it may be cleaned with a Be sure motor drive engages with the adapter drive strip of No 00 or No 000 sandpaper If the commu when installing tator is rough or worn it should be turned in a lathe and the mica undercut Inspect the armature shaft 11 94 EXH...
Page 269: ...ing the ex be made on the exhaust system as follows haust system from the engine Effected 1 Attach the pressure side of an industrial Serials include 18265176 thru 18268320 and vacuum cleaner to the tailpipe opening using a rub F18200026 thru F18200169 ber plug to effect a seal as required d Remove nuts bolts and clamps attaching stack NOTE assemblies to the muffler e Loosen nuts attaching exhaust...
Page 270: ...mum clearance between exhaust muffler and induction air duct assembly 1 Clamp 2 Exhaust Stack Assembly 3 Riser 10 4 Cabin Heat Outlet Detail A 5 Cabin Heat Inlet 6 Shroud 7 Muffler 8 Tailpipe 9 EGT Probe 10 Clamp Figure 11 8 Exhaust System 11 32 ...
Page 271: ...ternal power source may be connected to assist by the main oil filter screen Partial or in cold weather starting Refer to Section 16 for use complete loss of engine lubrication may of the external power receptacle result from either condition If these con ditions are anticipated after oil dilution The following may also be used to assist engine start the engine should be run for several min ing in...
Page 272: ... Description 2C8 11A 14 Trouble hooting 2B24 11A 6 Trouble Shooting 2C8 11A 14 Static Run Up Procedures 2C3 11A 9 Magneto 2C8 11A 14 Removal 2C 11A 9 Description 2C8 11A 14 Cleaning 2C4 11A 10 Removal Installation 2C8 11A 14 Accessories Removal 2C4 11A 10 Internal Timing 2C10 11A 16 Inspection 2C5 11A 11 Timing to Engine 2C10 11A 16 Build Up 2C5 11A 11 Maintenance 2C11 11A 17 Installation 2C5 11A ...
Page 273: ...INSPECTION Wipe the 11A 11 DESCRIPTION An air cooled wet sump inner surfaces of the cowling segments with a clean six cylinder horizontally opposed direct drive cloth saturated with cleaning solvent Stoddard or carbureted Turbocharged Avco Lycoming 0 540 equivalent If the inside surface of the cowling is L3C5D engine driving a constant speed propeller coated heavily with oil or dirt allow solvent ...
Page 274: ...il A Detail B 3 Clamp 2 10 12 e aDetaiC 8 Detail B 1 Pedestal 2 Cowl Flap Control 3 Clamp 4 Retainer 5 Cowl Flaps 6 Clevis 7 Shock Mount 8 Bracket 9 Position Bracket 10 Clevis 11 Control Lever 12 Bushing Figure 11A 1 Cowl Flap Installation 11A 3 ...
Page 275: ...approved spark plugs and required gap Torque 330 30 LB IN Carburetor Marvel Schebler HA 6 Tachometer Mechanical Drive Oil Sump Capacity 8 U S Quarts With External Filter 9 U S Quarts Oil Pressure PSI Normal 60 90 Minimum Idling 25 Maximum Cold Oil Starting 100 Oil Temperature Normal Operating 160 F 245 F Maximum Red Line 245 F Probe Location Accessory Housing Cylinder Head Temperature Normal Opera...
Page 276: ...ake Compressed Air Exhaust Gas Carburetor Heat Air Engine Cooling Air for Carburetor Heat Mechanical Linkage Throttle Throttle Waste Gate Control Linkage Final 1 2 control Initial 1 2 control Waste Gate travel is waste gate travel is throttle Waste Figure 11A 2 Turbocharger Airflow Schematic 11A 5 ...
Page 277: ...ed thoroughly Refer to Section 12 for fuel strainer cleaning Fuel contamination Drain all fuel and flush out fuel system Clean all screens fuel lines strainer and carburetor Defective carburetor Repair or replace carburetor Vaporized fuel Most likely Refer to Pilot s Operating Handbook to occur in hot weather with a hot engine Defective aircraft fuel system Refer to Section 12 Defective ignition s...
Page 278: ... or float Perform an idle mixture check level set too high Attempt to remove any rich indication with the idle mixture adjustment If the rich indication cannot be removed the float valve is leaking or the float level is set too high Replace defective parts reset float level Defective carburetor If engine will start when primed but stops when priming is dis continued with mixture control in full RI...
Page 279: ...oat level set too low Check and reset float level Spark plugs fouled or improperly Remove clean and regap plugs gapped Replace if defective Defective ignition system Refer to paragraph 11A 57 Defective carburetor If engine will start when primed but stops when priming is dis continued with mixture control in full RICH position the carbu retor is defective Repair or replace carburetor Cracked engin...
Page 280: ...aily changes in atmospheric pressure tem cedure Refer to Section 2 for storage preparation perature and humidity will have a slight The following engine removal procedure is based affect on static run up upon the engine being removed from the aircraft with the engine mount attached to the firewall c Average the results of the RPM readings The average should be within 50 RPM of 2350 RPM NOTE d If t...
Page 281: ...ngine weight will cause the aircraft to be tail heavy and pull controls aft clear of engine Use care to avoid bending controls too sharply Note EXACT r Attach a hoist to the lifting lug at the top center position size and number of attaching washers and of the engine crankcase Lift engine just enough to spacers for reference on reinstallation relieve the weight from the engine mount pads k Disconn...
Page 282: ... cable do not permit should be new parts starter terminal bolt to rotate Rotation of 11A 22 INSTALLATION Before installing the starter to be engine on the aircraft install any items which were removed from the engine or aircraft after the engine was removed 3 Starter electrical cable at starter drive cable engages drive in adapter Torque housing Remove all protective covers plugs caps attach nut t...
Page 283: ...us as possible direction Various lines hoses wires and controls c Hoses should have a minimum of one half inch are routed through some baffles Make sure that clearance from other lines ducts hoses or surround these parts are reinstalled correctly after installa ing objects or be butterfly clamped to them tion of baffles d Rubber hoses will take a permanent set during extended use in service Straig...
Page 284: ...er workers carburetor Note EXACT position size and number who handle engine oil are advised to of attaching washers and spacers for reference on minimize skin contact with used oil and reinstallation promptly remove used oil from the skin In a e Disconnect and cap or plug fuel line at carbure laboratory study mice developed skin cancer tor after skin was exposed to used engine oil f Remove safety ...
Page 285: ...em through an intake port and a is no twist or torque on hose If hose is wrapped filter on the aft left side of the cowling It is ducted with MIL Y 1140 cord in place of wire support the to the airbox and onward to the turbocharger com same installation procedures applies except MIL Y pressor section located under and to the left of 1140 has no miumum bend radius requirement engine After compressi...
Page 286: ... is b Remove the eight screws securing the high installed then remove the magneto tension outlet cover to the magneto The P d Reverse the preceding steps for reinstallation leads may be disconnected for additional clearance and time magneto to engine in accordance with para if necessary graph 11A 62 1 Air Filter Box 2 Air Filter Assembly NOTE 3 Air Box Inlet Clamp 4 Air Box If the aircraft is equi...
Page 287: ...arallel will be thrown off Do not drive cam on rotor to the breaker contacts shaft with a mallet or other instrument d Connect the timing light Bendix Part No 11 9110 or equivalent black lead to any unpainted sur m Recheck timing to make sure both sets of breaker face of the magneto Connect the red lead to the left contacts begin to open within the width of the L E breaker contact terminal and the...
Page 288: ...ghts should go off Continue turning the en mal direction of magneto rotation until the red painted gine in its normal direction of rotation until the other tooth of the large distributor gear is centered in the timing light goes off This should be not more than timing hole hole at each side of magneto 3 engine degrees later than the first light If not d Also observe at this time that the built in ...
Page 289: ...s are A spark plug that is kept clean and properly gapped not moistened with oil re oil using 2 or 3 drops of will give better and longer service than one that is lubricant Bendix Part No 10 86527 or equivalent allowed to collect lead deposits and is improperly Allow approximately 30 minutes for felt to absorb the gapped lubricant Blot off excess lubricant with a clean NOTE lint free cloth Too muc...
Page 290: ...t 19 Bearing 34 Washer 5 Bolt 20 Throttle Control Rod End 35 Support Assembly 6 Washers 21 Nut 36 Bolts 7 Bearing 22 Cotter Pin 37 Mount 8 Lever Slotted Throttle 23 Castellated Nut 38 Gasket 9 Bolt 24 Cam nonfunctional 10 Washer 25 Nut 11 Retainer 26 Washer 12 Washer 27 Washer 13 Bearing 28 Clamp 14 Bracket 29 Bolt 15 Washer 30 Waste Gate Control Cable Figure 11A 5 Throttle to Carburetor and Waste...
Page 291: ... Bolts 13 Control Arm 4 Control Retainer 14 Waste Gate Control Cable 5 Return Spring Bracket 15 Waste Gate Exhaust Pipe 6 Return Spring Eye Bolt 16 Waste Gate Clamp 7 Return Spring 17 Waste Gate Valve Exhaust Bypass 8 Maximum Stop Screw Min Bypass 18 Minimum Stop Screw Max Bypass 9 Waste Gate Valve Arm 19 Cable Brackets 10 Waste Gate Valve Arm Extension Lever Figure 11A 6 Waste Gate Assembly 11A 2...
Page 292: ...em con installed sists of a single pipe for each cylinder two short 3 Tighten castellated nut 23 and install cotter pin stacks a crossover tube a Y connector the turbine 22 after throttle rod bolt 22 after throttle rod bolt section of the turbocharger a waste gate and a 4 Tighten stationary lever bolts 29 before support single exhaust outlet The single pipes collect ex mount bolts haust gases from...
Page 293: ...Hand 4 Clamp Half Right Hand 5 Exhaust Stack Assy Right Hand 6 Exhaust Stack Clamp 7 Crossover Pipe 8 Left Exhaust Riser 9 Exhaust Stack Assy Left Hand 10 Turbocharger Mount 11 Exhaust Stack Clamp Left Hand 12 Crossover Pipe 13 Heat Guard 14 Waste Gate Inlet 15 Tail Pipe Figure 11A 7 Exhaust System Installation 1 A 22 ...
Page 294: ...rs the carburetor where fuel is added be made on the exhaust system as follows and flow is limited by the throttle valve setting Dur 1 Attach the pressure side of an industrial vac ing the transient interval from low to high RPM the uum cleaner to the tailpipe opening using a rubber absolute pressure relief valve functions to limit maxi plug to effect a seal as required mum pressure available to t...
Page 295: ...I _ B A S 5 Absolute Pressure Relief Valve lIHe lr11 8 Compressor Inlet Duct 7 Compressor Inlet Elbow 8 Compressor Clamp 13 _ 1 9 Check Valve 10 Turbocharger 11 Check Valve 12 Turbine Outlet Clamp 13 Taill Pipe 14 Waste Gate Connection 15 Gasket 16 Exhaust Manifold 17 Turbocharger Mount Brackets 18 Carburetor Inlet Gasket 19 Turbocharger Mount Bolts Figure 11A 8 Turbocharger Installation 11A 24 ...
Page 296: ...e lubrication may result from either condition If these conditions are 11A 79 ECONOMY MIXTURE INDICATOR EGT anticipated after oil dilution the engine should Refer to Section 15 be run for several minutes at normal operating temperatures and then stopped and inspected 11A 80 EXTREME WEATHER MAINTENANCE for evidence of sludge and carbon deposits in the oil sump and oil filter screen Future 11A 81 CO...
Page 297: ...fsystem the inboard bay of each ing When the fuel system is system checks and repairs on the airplane fuel system in operation depending upon the aircraft configura tion gravity an electric or engine driven fuel pump draws the fuel from the tanks through the tank strain er a selector valve fuel strainer electric or engine driven fuel pump to the carburetor In the 1977 During all fueling procedures...
Page 298: ... plugged Clean or replace fuel line FUEL STARVATION AFTER Partial fuelflow from the pre Use the preceding remedies STARTING ceding causes Pluged fuel vent Refer to paragraph 12 24 Water in fuel Drain fuel cell sumps lines and strainer NO FUEL QUANTITY Fuel cell empty Service with proper grade and INDICATION amount of fuel Open or defective circuit breaker Reset Replace if defective Loose connectio...
Page 299: ...EDON A SLOPING CONDITION SURFACE PLACE THE FUEL SYSTEM SHOWN WITH SELECTOR VALVE IN EITHER SYSTEM SHOWN WI h LEFT OR RIGHT POSITION FUEL SELECTOR VALVE IN BOTH POSITION FUEL STRAINER y t cii L TO ENGINE I FUEL STRAINER ENGI E DRAIN CONTROL PRIMER CODE THROTTLE CARBURETOR CONTROL O CONTROL 0 I i FUEL SUPPLY L I 1 VENT MIXTURE ENT _ CONTROL ___ MECHANICAL LINKAGE TO ETNGINE ELECTRICAL ENGNE CONNECTI...
Page 300: ...LVE CON OLCONDITION SELECTOR VALVE SYSTEM SHOWN WITH DRAIN PLUG gFUEL SELECTOR VALVE i i IN BOTH POSITION FUEL STRAINER FUEL STRAINER 0E CONTR N0 Wli iir Pialj TO ENGINE CONTROL F i CPT WENGINE PRIMER THROTTLE O CONTROL SS E M N CARBURETOR MIXTURE _ 1 1 CODE CONTROL FUEL SUPPLY TO ENGINE I I VENT TO ENSURE MAXIMUM FUEL CAPACITY WHEN REFUELING AND MINIMIZE CROSS FEEDING MECHANICAL WHEN PARKED ON A ...
Page 301: ... CONDITION SELECTOR VALVE SYSTEM SHOWN WITH IN BOTH POSITION FUEL STRAINER DRAIN CONTROL ENGINE PRIMER AUXILIARY FUEL PUMP AUXILIARY FUEL PUMP FUEL PRESSURE GAGE THROTTLE CONTROL MIXTURE CODE CONTROL TO ENGINE MECHANICAL LINKAGE T182 ONLY CONNECTION THRU 1982 MODELS Figure 12 1 Fuel System Schematic Sheet 3 of 4 12 5 ...
Page 302: ...I ENGINE SWIC P ESU EPRIMER OPT GAGEO__ STD ENGINE AUXILIARY FUEL PUMP AUXILIARY SWITCH FUEL PUMP ELECTRIC FUEL PUMP PRIMER rC FUEL SWITCH _ PRESSURE IOPTS SOLENOIDM U FE LI KGAGE VALVE i i T RIGHT HALF OF DUAL INSTRUMENT TO ENGINE THROTTLE S CODE CONTROL C SU_ RCCARBURETOR PC FUEL SUPPLY MIXTURE Q _ I I VENT CONTROL 0 MECHANICAL LINKAGE TO ENSURE MAXIMUM FUEL LINKAGE CAPACITY WHEN REFUELING TO EN...
Page 303: ...8266391 ON F F18200095 TKRM F18200169 1 Hose 6 Finger Strainer 12 Placard 2 Fuel Strainer 7 Fuel Filler Cap 13 Fuel Selector Valve 3 Primer Line 8 Fuel Quantity Transmitter 14 Gear and Shaft Assembly 4 Primer 9 Crossover Vent Line 15 Strainer Drain Control 5 Hose 10 Fuel Vent Valve 16 Drain Line 11 Vent Line Figure 12 2 Fuel System Sheet 1 of 2 Revision 2 12 7 ...
Page 304: ...m I t uRo m mo at T182 ONLY INCLEAR VEW OF THE PILOT 1 Fuel FlUer Cap 7 Fuel Selector Valve 2 Fuel Quantity Tranmitter 8 Drai Line 3 Crossover Vent Line 9 Fuel Stminer 4 Hose 10 Auziliary Electric Fuel Pump 5 Placard 11 Vent Line 6 Gear and Shaft Assembly 12 Fuel Vent Valve Ftgure 12 2 Fuel System Sheet 2 of 2 12 8 Revision 2 ...
Page 305: ...tly oiled and installed with side against heed 4 of valve 3 4 136176 TMU 1863660 E L I y STAM UBD CELL _ 4 1aB8i7C SBBu a 1 C r 16 mF1 zoom TU P 1ooe 14 1 Valve r9ea t 2 GQakt 10 BHow 3 Adapter 11 Tub 3A Nutring 12 Vent Valve3 13 4 Clamp 13 Ground Strap 5 tting 14 Pul Quantity Detai n 6 Winfg 6in Transmitter 7 Cover Plate 15 Hanger TCp 7k FllerS Cp 16 S3ins FEL QUANTITT TRAMI ER 8 Vent Line 17 Sre...
Page 306: ...htly 3 oil and idtaled witha b to ide iut he d C 6 2 1 7A f L 104 14 l6 las1smu6 TH U n seamo 16 n poooM n oooF THU 11m 1 vw mCp 1 HnaawClyp 13 a d S V UM 1 Usiner 3A Nultoug 10 HRm 18 Vest AdJater 4 Cmp 11 Tube 19 H r Trp tun D a rfntff 1l Vt Valve 6 Wing in 13 Ground SapULQUATIT AM 7 covr P 1f Ct F Q Svu7 sl to DBTALLAT1ON AND GROUMDI Figure 12 3 Fuel Cel Installation Sheet 2 of 2 12 10 Revisou ...
Page 307: ... clamp traces of fuel screws A light application of 10 engine oil to metal tube aids installation into nipple fittings b Remove wing root fairings and disconnect fuel f When installing filler adapter cover plate and lines at wing root fuel quantity transmitter to the wing and fuel cell c Remove clamps from forward and aft fuel cell tighten attaching screw evenly The sealing or com bosses at wing r...
Page 308: ...es If the O rings 3 13 have deteri interchangeable and will fit the same adapter assem orated they must be replaced bly 12 15 CLEANING 12 14 INSPECTION a Using a cotton swab and Stoddard solvent or equivalent gently lift edges of rubber umbrella 5 NOTE and clean stainless steel seat and umbrella removing all contaminates Using a second swab wipe seat If fuel collects in the handle well it could in...
Page 309: ...uid to prevent f Check that square hole in bottom of lock plate tearing the stem 6 is aligned with square surface on threaded end of g To replace the umbrella lubricate the umbrella stem 14 stem with MIL H 5606 hydraulic fluid and use a NOTE small blunt tool to insert the retaining knob on the umbrella stem into the check valve body to prevent It is possible to install the lock plate 6 damaging th...
Page 310: ...hain and remove RH filler equivalent gently lift edges of rubber umbrella cap from fuel tank adapter and clean seat and umbrella removing all contam b Plug fuel tank opening to keep dirt and inants Using a second swab wipe seat and um foreign matter from ontaminating the tank brella thoroughly removing all cotton fibers Repeat until swabs show no discoloration d If the umbrella continues to leak o...
Page 311: ...dard solvent or FILLER CAPS equivalent gently lift edges of rubber umbrella 5 and clean stainless steel seat and umbrella removing The following procedure may be used to detect fuel all contaminates Using a second swab wipe seat and filler cap leakage umbrella thoroughly removing all cotton fibers a Service the aircraft with approved fuel filling Repeat until swabs show no discoloration each bay b...
Page 312: ...then operations Special flights for the sole bends down and inboard A vent valve is install purpose of checking and adjusting fuel ed on the inboard end of the vent line inside the fuel tank feed rates are not recommended cell and a crossover line connects the cells together On aircraft equipped with long range cells a nylon a Inspect the venting system to insure the lines vent tube is attached to...
Page 313: ...NOTE down to allow the roll pin to clear a lock ring slot before rotating shaft through the four oper Repair of damaged or worn parts of the ating positions selector valve assembly is NOT authorized and therefore is limited to replacement of 12 27 REMOVAL AND INSTALLATION See fig component parts only component parts only ure 12 7 a Drain all fuel from wing tanks fuel strainer a Clean disassembled ...
Page 314: ...rings 11 into body 7 c With spring compressors 14 in place as shown in Section A A figure 12 7 compress springs 11 and install washers 10 new O rings 9 and seals 12 33 REMOVAL AND INSTALLATION See fig 8 into inlet ports ure 12 8 d Holding springs compressed carefully insert a Remove cowling as necessary to gain access to rotor 5 into valve body 7 Release spring com strainer pressors and check for ...
Page 315: ...ssor 29 Spring 30 Collar 19_ 18 18288176 THRU 18267715 _7 T r F18200026 T F18200189 A C 18287716 ON i r Ef 030 Typ 22 200 ll t 03 0 R __a 21 _ 10 L 20 Ref Fl8200026 THRU F18200169 23Detal I I oee 1011 6 23 3 9 7 14 f 21 4 Cross Section A A L J 5 Grind flat I 24 S f 9 and break sharp edges 91011y 8 9 Wrap with tape NOTES Inlet Ports 0 12 Fabricate two spring compressors 14 i z 1 2 from 1 16 inch di...
Page 316: ... equiva lent After threads have thoroughly dried apply Grade CV Loctite Catalog 85 or 83 Loctite 242 or 16 equivalent Loctite products may be obtained from Lootite Corp 705 Mountain Rd I4 9 Newington CT 06111 19 21 r 16 22 2 20 182688086 THBU 182684 3 182 218 L0 Figure 18 7 Fuel Selector Valve and Controls Sheet 2 of 3 12 20 Revision 1 ...
Page 317: ...ry partsbefore ap plying bonding agent At 75 F bond cures to 80 ultimate tensile strength within 24 hours Accel erated cure times are as follows a Five minutes at 250 F b Ten minutes at 200 F Before installing screw 26 on drive shaft 18 clean threads of screw 26 with MEK or equiva lent After threads have thoroughly dried apply Grade CV Loctite Catalog 85 or 83 Loctite 242 or equivalent Loctite pro...
Page 318: ...t it from being with drawn if the attaching clamp 17 should come loose 2 Washer 1 Spring 3 Plunger 5 Drain Control 6 Plate 7 O Ring 8 Gasket 9 Filter 12 10 Collar 11 Standpipe 12 O Ring 13 Bowl 14 Ring 15 Nut 16 Drain Line 17 Clamp 2 15 SAFETY WIRE HOLE NOTE Torque nut 15 to 25 30 in lb and safety wre Figure 12 8 Fuel Strainer 12 22 ...
Page 319: ...EMOVAL AND INSTALLATION portion of the inboard wing structure between a With selector valve in OFF position drain the front and rear wing spars extending ap fuel from strainer and lines with quick drain control proximately five feet into each wing This b Disconnect and cap or plug all fuel lines at type construction reduces overall weight as primer Observe precautions in paragraph 12 3 well as inc...
Page 320: ...EALANT Two kinds of sealants are used one to seal the fuel bay and the Purge fuel bays with an inert gas prior to repairing fuel leaks to preclude the possi other to seal the access doors and fuel quantity trans repairing fuel leaks to preclude the possi bility of explosions pliable and will not adhere to metal as firmly as the bay sealant does This permits the access doors and The following proce...
Page 321: ... accel fay sealant need not be cured before the fillet seal is erator and sealant until it becomes a uniform mixture applied but the squeezed out sealant to which the Do not allow air bubbles to mix in If this occurs fillet sealant s applied must be free of dirt and con work air bubbles out tamintion Fillets laid on intersecting joints shall be joined together to produce a continuous fillet Filler...
Page 322: ...ES SERVICE MANUAL NOTE Refer to paragraph 12 46 TYPICAL INSPECTION PLATE 1 Fuel Side 2 Nutplate 3 Filet Seal 4 Faying 5 Rivet and Fastener Seal TYPICAL FUEL BAY END SECTION SPAR Figure 12 11 Typical Fuel Bay Sealing 12 26 ...
Page 323: ...and e Test fuel bay for leakage as outlined in paragrap 12 49 Work life of sealants included in kit SK210 56 12 49 is two hours Work life of sealant included in 12 48 NORMAL CURE TIME Service Kit SK210 56 kit SK210 101 is 1 2 one half hour These 12 48 NORMAL CURE TIME ServiceKit SK210 56 times are based on standard conditions of contained A SP654706B2 access door sealant 77 F 25 C and 50 percent r...
Page 324: ... grease wax dirt etc eter capable of measuring twenty inches of water Pour cleaning solvent onto the cloth and wipe d To the other bay fitting connect a well regulated the surface Then use a clean dry cloth to wipe supply of air 1 2 PSI MAXIMUM or 13 8 INCHES of the solvent from the surface prior to its evap water Nitrogen may be used where the bay might oration Be sure the surface to be sealed is...
Page 325: ...ccureha 2sodmae a located in eachpfuel drain path below hat s connected onc trically to separate galvanometric gages one for r skin 6 Apply pressure slowly untl 1 2 PSI is obtained each tereby ndicl 82level n each bay Apply soap solution as requition and procedur fteor oper change from 3 each to 6 each Figure 12 12 Integrai Fuel Bay Components 1 of 4 h Allow 15 to 30 minutes formpressure to stabil...
Page 326: ... valve 1 16 1 Drain Valve 2 Valve Assembly 4 Gasket 5 Washer 6 Nut 8 Grommet 9 Clamp 11 Screw 12 Finger Strainer 13 Clamp 14 Fitting 16 Gasket 17 FuelSampler Cup NOTE Beginningwith 1979 models items thru 11 13 14 13 12 Detail E When tightening screw clamp 13 13 do not exceed 8 10 in lbs 15 Figure 12 12 Integral Fuel Bay Components 2 of 4 12 30 Revsion 1 ...
Page 327: ...removing and replacing fuel quantity transmitter 5 dis card gasket 4 and replace it with new S2670 1 gasket 8 Torque screws 7 to 20 in lbs once only using a cross pattern sequence 18265176 THRU 18268456 F18200026 THRU 18200169 1 Nutring 2 Gasket Root Rib 3 Root Rib 4 Gasket Transmitter 5 Fuel Quantity Transmitter 6 Washer 7 Screw 8 Gasket 18268457 AND ON Detail C Figure 12 12 Integral Fuel Bay Com...
Page 328: ...0 MIN GRADE AVIATION GASOLINE CAP 46 0 U S GAL CAP 34 5 U S GAL TO BOTTOM OF FILLER NECK Fuel Quantity Placard AVGAS ONLY Fuel Grade Placard 1 Fuel Cap See figure 12 5 2 Fuel Filler Neck Figure 12 12 Integral Fuel Bay Components 4 of 4 12 32 Revision 1 ...
Page 329: ...peller is single move the blades to a lower pitch to maintain the acting in which engine oil pressure boosted and selected engine speed Figure 13 1 illustrates the regulated by the governor is used to obtain the cor different propellers used on the aircraft Refer to rect blade pitch for the engine load Engine lubrica applicable vendor publications for further information ting oil is supplied to th...
Page 330: ...r governor Preform static RPM check TOO LOW adjustments Refer to Section 11 11A for procedures ENGINE SPEED WILL NOT Sludge in governor Refer to paragraph 13 10 STABILIZE Air trapped in propeller Trapped air should be purged actuating cylinder by exercising the propeller several times prior to take off after propeller has been rein stalled or has been idle for an extended period Excessive friction...
Page 331: ...and lug b Remove safety wire back off bolts attaching attaching screws propeller to engine crankshaft about 1 4 inch pull propeller forward 13 6 INSTALLATION 182 F182 propeller 2 can be pulled forward approx imately 1 4 inch eack time until all bolts Be sure magneto is grounded before turningaged from engine crankshaft propeller flange As the propeller is seperated from the engine crankshaft oil w...
Page 332: ...r 1 to ensure a snug fit between spinner 1 and support 2 DO NOT USE more than a total of 14 spacers in this in 7 stallation 17 19 1 j 20 12 1 Spinner 2 Spinner Support 3 Spacer 4 Cylinder 5 Screw 182 F182 ONLY 6 Ppeller 7 Stud 8 Dowel Pin 9 0 Ring 10 Washer 11 Engine Crankshaft TfIU 18268029 12 Spinner Bulkhead THTIU 18268029 1 3 Lug 13 Lug BEGINNING WTH 18268030 1 ing Nut 15 Screw 16 Balance Weig...
Page 333: ...propeller mounting bolts to 660 780 lb in BEGINNING WITH 18267931 3 5 6 1 Spinner 2 Propeller 3 Aft Spinner Bulkhead 4 Screw T182 ONLY 5 Washer 6 Nut 7 Screw 8 Propeller Hub 9 O Ring 10 Mylar Washer Figure 13 1 Propeller Installation Sheet 2 of 3 13 5 ...
Page 334: ... 18267931 Torque propeller mounting bolts to 660 780 lb in 5 6 1 Spinner 3 Aft Spinner Bulkhead 4 Screw OPTIONAL 3 BLADED 5 Washer T182 ONLY 6 Nut 7 Screw 8 Propeller Hub 9 Forward Support 10 Mylar Washer Figure 13 1 Propeller Installation Sheet 3 of 3 13 6 ...
Page 335: ... magneto is grounded before turning propeller When replacing optional three bladed propeller assembly 2 apply Y8560 Polyurethane Film a Remove cowling and engine baffles as required 3M Company a minimum of one wrap on for access to governor propeller hub 8 then as required to obtain b Disconnect governor control from governor a snug fit of forward support 9 to propeller hub 8 NOTE Note EXACT posit...
Page 336: ...crew locknut safety wire stop against high rpm stop screw Be sure to maintain screw and make propeller control linkage adjustment sufficient thread engagement of the control and rod as necessary to maintain full travel end If necessary shift control in the clamps to e Install baffles and cowling achieve this f Test operate propeller and governor e Attach rod end to the governor arm extension Be su...
Page 337: ...ETWEEN OVERHAUL TBO Pro peller governor overhaul shall coincide with engine overhaul Refer to sections 11 and 11A for engine time between overhaul TBO periods The gover nor overhaul manual is available from the Cessna Supply Division 13 9 13 10 blank ...
Page 338: ...linder General Removal Installation 2F20 14 1 Information 2F16 14 12 Propeller De Ice System Cylinder Regulator 2F16 14 12 B F Goodrich 2 Bladed 2F21 14 17 Servicing Oxygen Cyl Description 2F21 14 17 inder Regulator 2F16 14 12 Trouble Shooting 2F23 14 19 Removal of Oxygen Cyl Timer Test 2F23 14 19 inder Regulator 2F17 14 13 Slip Ring Alignment 2F23 14 19 Installation of Oxygen Installation Alignme...
Page 339: ...e firewall of defective parts is imperative because fumes consti The heated air flows from the shut off valve into a tute an extreme danger Seal any gaps in heater ducts across the firewall with Pro Seal 700 Coast duct across the aft side of the firewall where it is Pro Seal Co Los Angeles California compound distributed into the cabin The shut off valve oper or equivalent compound ated by a push ...
Page 340: ...allation and repair of defrosting system com ponents Cut hose to length and install in the origi nal routing Trim hose winding shorter than the hose control Check the airscoop filter elements in the to allow clamps to be fitted A defective defroster wing leading edges for obstructions The elements outlet must be repaired or replaced may be removed and cleaned or replaced Since air passing through ...
Page 341: ... ON F18200076 THRU 18200169 1 Cabin Heat Control 8 Valve Plate Assembly 16 Cowl Deck 2 Nut 9 Valve Seat 17 Nozzle 3 Washer 10 Shim 18 Cotter Pin 4 Control Arm 11 Valve Body 19 Valve 5 Roll Pin 12 Clamp 20 Shaft 6 Clamp Bolt 13 Hose 21 Defroster Control 7 Spring 14 Screw 22 Duct 15 Deflector Figure 14 1 Heating and Defrosting Systems Sheet 1 of 2 Revision 1 14 3 ...
Page 342: ... Spring T182 1827716 ON 4 l Valve Sea 6 Clamp 8 Hose 9 _ Valve Door 14 _ 4 Re a 0 0 0 a 0 4 v Sca I 10 a ii 0 10 75 3 SprHing T182 Sstes e ON 14 8 H ose 10 Clamp 11 Bolt Figure 14 1 Heating and Defrostin Systems Sheet 2 c 2 14 4 Revialon 1 ...
Page 343: ...24 5 Tube Assembly 6 Seal Detail A 7 Nut 8 Washer NOTES 9 Washer Detail D 10 Seal Trap headliner 24 between 11 Bullet Catch housing 30 and escutcheon 12 Outlet Assembly 28 Typical entire perim 13 Knob eter of escutcheon 14 Washer 15 Screw Beginning with Serial 18268335 16 Insert install screw 15 through insert 17 Fuselage Skin 16 to provide attachment 18 Fresh Air Door 19 Clamp Bolt 10 20 Seal 32 ...
Page 344: ... 26 1 r Door Assembiy 0 Hosn 18 Wh 2 Link 11 Cotr 1 Bult ach 9 22 3 Lever 12 Washer 20 t emb y 4 Clap Bl 1 Pn 21 Tbe A se mbly 6 Nut 1 2 Kn 94 Cotte Pi n n 2 Inse c 7 Pin 16 N2 ah ahr A1 Washer 2 or 4 olt 13 Pn 21 ube Assembly 1 DoorAssembly 10 Housing 18 Washer 8 Washer 17 Washer 25 Screw 9 Cotter Pin 26 Insert BEGINNING WITH 18268294 Figure 14 2 Ventilating System Sheet 2 of 3 14 6 ...
Page 345: ...rol 30 in clamps 31 and 45 such 4 that when knob 40 is in OFF 24 position valve assembly 49 46 seals tightly in tube 47 shut tine off outside fresh air 47 Rigging of valve assembly 49 is not required when knob 40 8 48 is in ON position 49 50 Detail D 51 27 Adapter 35 Washer 44 Shaft 28 Bracket 36 Washer 45 Clamp 29 Bracket 37 Spring 46 Bracket 30 Control 38 Washer 47 Tube 31 Clamp 39 Bracket 48 Sh...
Page 346: ... THRU 18267715 72 Buhead Springtation 124 00 F18200026 THRU F18200169 8 Knob 33 Body 13 Support 9 Outlet Valve Assembly 38 Oxygen MaskCylinder Figure 14 3 O5 ygen Systems Sheet 1 of 3 14 8 6 Bulkhead ion 140 7 Regulator 18 Tee 19 Filler Line 20 Lock Ring 21 Cover 22 Window Moulding 23 Nut PressureGage Line 26 Retainer 2 Low Pressure Line 27 Retainer Assembly 3 ON OFF Control Casing 28 O RiR y sa 4...
Page 347: ...y 18267716 THRU 18268293 2 F _ 1 X 1 W 1 Pressure Gage Line J e s 2 Low Pressure Line 3 ON OFF Control Casing i i 4 Bracket oa H 5 Cover 6 Speaker Grille 7 Arm 18267716 ON 8 Knob 9 Outlet Valve Assembly 10 Oxygen Gage 37 Bracket Figure 14 3 Oxygen Systems Sheet 2 of 3 Revision 1 14 9 ...
Page 348: ...n 124 00 17 Regulator 18 Tee 19 Filler Line t25 9 20 Lock Ring 21 Cover 22 Window Moulding 23 Nut 24 Bracket 23 24 26 25 Nut 26 Retainer d 22 31 27 Retainer Assembly 21 Detail r 30 28 0 Ring 29 Washer 28 Detail G 30 Seat 27 31 Poppet 38 32 Spring 33 Body 34 Access Plate 35 Spacer i DetailH 36 Adapter Assembly 7 38 Oxygen Mask 1 18267716 a ON Figure 14 3 Oxygen Systems Sheet 3 of 3 14 10 Revision 1...
Page 349: ...N IS Defective pressure gage Replace gage TOO SHORT Leak in system Locate and tighten loose fittings Replace defective part PRESSURE INDICATION Defective cylinder regulator Replace cylinder regulator NORMAL BUT NO FLOW OF OXYGEN WITH CYLINDER Crimped or damaged lines Replace damaged lines REGULATOR ON Damaged control cable Replace control cable 14 20 MAINTENANCE PRECAUTIONS b Cap all openings imme...
Page 350: ...e to be used until they fail hydrostatic With oxygen cylinder charged do not pull test control to ON position with outlet ports low pressure open to atmosphere Dam NOTE age to regulator metering poppet may occur Commission Code of Federal Regulations Whenever a component of the oxygen system Title 49 Chapter 1 Para 73 34 has been removed reinstalled replaced or the system has been disassembled for...
Page 351: ...a manifold or a portable oxygen cascade 90 f Slowly open valve on cascade cylinder or mani g Reinstall aft baggage partition fold with lowest pressure as noted on pressure gage allow pressure to equalize then close cascade cyl 14 26 INSPECTION OF OXYGEN CYLINDER inder valve REGULATOR g Repeat this procedure using a progressively a A careful visual inspection of the oxygen cyl higher pressure casca...
Page 352: ...ns caused by contact with figure 14 3 blunt objects in such a manner that the a Remove access plate 34 from fuselage skin thickness of the metal is not impaired b Remove filler line 19 from filler valve 11 The major diameter of the dent must be cap filler line equal to or greater than 32 times the c Remove screws attaching filler valve 11 to depth of the dent Sharper dents or adapter assembly 36 d...
Page 353: ... assemblies are mounted pressure gage into the oxygen outlet valve overhead and outboard of each passenger station c Test retainer assembly 27 adapter junction for leaks with fluid leak detector No bubbles are per 4 38 REMOVAL OF PASSENGER OUTLET VALVE mitted ASSEMBLY See figure 14 3 d After completion of leak tests fully charge oxygen system as outlined in paragraph 14 23 NOTE 14 43 OXYGEN SYSTEM...
Page 354: ...observe indicated pressure rise as the system e Recharge oxygen system as outlined in para is charged and decrease as oxygen is bled off graph 14 23 14 49 OXYGEN MASKS 14 54 HEATED WINDSHIELD PANEL See figure 14 5 14 50 DESCRIPTION One pilot s mask and three passengers masks are provided with the aircraft 14 55 DESCRIPTION The panel is constructed of The pilot s mask has a built in microphone and ...
Page 355: ...the surfaces of the 14 57 PROPELLER DE ICE SYSTEM B F Good propeller blades where ice would normally adhere rich 2 Bladed Propeller Installation See figure This heat plus centrifugal force and the blast from 14 6 the airstream removes accumulated ice When the de ice switch is turned on the timer provides power 14 58 DESCRIPTION The system is of an electro through the brush block and slip ring to a...
Page 356: ...eS oe o 12 4 Stop Assembly S 82 8 8jL5 Bracket Figure 14 5 Win e6 Lower Windshield Retainer 14 18 WT T 7 Pluiger 8 Handle 7 _ 9 Tube 8 9 l z 10 Bracket 8 T r11 Connector 12 Bumper 10o 13 Cover Detail A 14 Circuit Breaker Detail A 15 Switch 18268294 ON Figure 14 5 Windshield Anti Ice Installation 14 18 Revision 1 14 18 Revision I ...
Page 357: ...s condition will c Turn on de ice system result in rapid deterioration of the slip d Check timer operation per the chart Use a ring and brush contact surfaces leading voltmeter to eventual failure of the de ice system e Check volts to ground in each case If engine is not running and auxiliary power is not used voltage a Securely attach dial indicator gage to engine will be battery voltage and cycl...
Page 358: ...t G 3 Clamp 9 4 Modular Brush Assembly 10 5 Slip Ring Starter Gear Assembly 6 Bulkhead 11 7 Lead Clip 8 Tie Strap I i 12 9 Restrainer Strap 10 Propeller Blade I 11 De Ice Boot 12 Spinner B F h 2 d Pro r D e S m t 14 20Revisi on I o _ FIgure 14 6 B F Goodrich 2 Bladed Propeller De Ice System Sheet 1 of 4 14 20 RevisIon 1 ...
Page 359: ... Il i I 13 Timer 14 Circuit Breaker 15 Propeller De Ice Gage 16 Propeller De Ice Switch 14 Detail C 15 16 r i l l _ __________g l ____ v__ _ _ _ Detail B 18268294 ON Figure 14 6 B F Goodrich 2 Bladed Propeller De Ice System Sheet 2 of 4 Revision 1 14 21 ...
Page 360: ...S SERVICE MANUAL I M i 2 4 View E _ E E 3 View D D 1 Support Bracket 2 Mounting Bracket 3 Clamp 4 Modular Brush Assembly BEGINNING WITH 18268294 Figure 14 6 B F Goodrich 2 Bladed Propeller De Ice System Sheet 3 of 4 14 22 ...
Page 361: ...rap approximately in this location so a double thickness is over View F F lead strap of the de icer 9 Restrainer Strap 10 Propeller Blade 11 De Ice Boot 17 Lead Strap 18268294 ON Figure 14 6 B F Goodrich 2 Bladed Propeller De Ice System Sheet 4 of 4 Revision 1 14 23 ...
Page 362: ... 062 curing time before operating the de icers 0 030 inch 2 The brushes must be lined up with the slip e Mix EC 1300L cement Minnesota Mining Mfg ring so that the entire face of each brush is in con Co thoroughly Surfaces shall be 65 F prior to tact with the slip ring throughout the full 360 of slip applying cement During periods of high humidity ring rotation care shall be taken to prevent moistu...
Page 363: ...sh o Install restrainer strap as shown in detail in block and slip ring to outboard elements for approxi figure 14 6 sheet 4 Start strap approximately in mately 30 seconds reducing ice and adhesion in these location shown in detail so a double thickness is areas Then the timer switches power to inboard over lead strap of the de icer The lead strap must heating elements for approximately 30 seconds...
Page 364: ...arter Support 10 Slip 11 Bracket Assembly 13 Brush Block Assembly 14 26 R 3 Lead Strap 4 Propeller Blade 5 De IceBoot 6 Lead Clip 7 Bulkhead 8 Tie Strap 9 Starter Support 10 Slip Ring 11 Bracket Assembly 12 Spacer 13 Brush Block Assembly T182 18268294 ON Figure 14 7 McCauley 3 Bladed Propeller De Ice System Sheet 1 of 3 14 26 Revision 1 ...
Page 365: ...____ ___ 15 v F 0 K i Detail A l i Detai Detail B 16 17 De Ice Switch I _ I I Detail C 14 Timer 15 Circuit Breaker 16 De ice Gage 17 De Ice Switch T182 18268294 ON Figure 14 7 McCauley 3 Bladed Propeller De Ice System Sheet 2 of 3 Revision 1 14 27 ...
Page 366: ...strainer strap approximately in ieV D D this location so a double thickness is DView over lead strap of the de icer 2 Restrainer Strap 3 Lead Strap 4 Propeller Blade 5 De Ice Boot T182 18268294 ON Figure 14 7 McCauley 3 Bladed Propeller De Ice System Sheet 3 of 3 14 28 Revision I ...
Page 367: ...ECT OR NOT CYCLING Defective timer Replace timer RAPID BRUSH WEAR Brush block or slip Align properly FREQUENT BREAKAGE ring out of alignment SCREECHING OR CHATTERING 14 67 TIMER TEST When correctness of the cycling sequence is estab a Remove connector plug of wire harness from lished turn propeller de ice switch off at the begin timer and jump power input socket of wire harness ning of one of the ...
Page 368: ...IES SERVICE MANUAL SLIP RING ASSEMBLY 0 062 t 0 030 inch 1 28 PELLERS ROTATION It BRUSH BLOCK ASSEMBLY Figure 14 8 Angular Brush Alignment SLIP ING BRUSH INCORRECT CORRECT INCORRECT Figure 14 9 Brush Face Alignment 14 30 ...
Page 369: ...while indicated in the readings by pushing in retightening the hardware Slotted holes are pro or pulling out on the propeller while vided rotating it Care must be taken to exert a uniform push or pull on the 14 70 REPLACEMENT OF DE ICE BOOTS Refer propeller to hold this error to a mini to paragraph 14 63 mum d If slip ring run out is within the limits specified 14 71 ICE DETECTOR LIGHT T182 See fi...
Page 370: ...MODEL 182 T182 SERIES SERVICE MANUAL A Termnl 6 Fuselage Skin 7 Lens Light _ A _ _ _ 1 Lamp 14 32 Revision Lamp 7 Lens Figure 14 10 ice Detector Light nstalltion 14 32 Revisot 1 14 32 Revision5 1 ...
Page 371: ...ding steps rain snow or ice crystals In some cases if dis establish a good ground before proceeding to step 3 chargers are not installed or not functioning as a 3 Connect the EARTH terminal of the megohm result of age or repeated exposure to static electricity meter to the base of the discharger and check the static build up can result in the loss of usable radio resistance at the tip of the wick ...
Page 372: ...o wm 214 15 26 SrtdIib Vl Tu TomBta 2415 26 TMsU l HoIng b14 15 18 TooblelBo 215 15 27 1ul EH14 1 1 215 15 27 In ballaio 14 11 16 D 215 15 27 bgmeuIndiMtor 217 15 1C Outde Air Tempertu1 Tahometr 17 1 1C oe 2515 27 15 1 ISTRUENTS AND INSTRUMENT SYSTEMS handled by Itrument spectalists Federal Aviation Rulation require mnlfsaclo truments be sent 15 2 GENERAL This section describes typical to an appro...
Page 373: ...MODEL 182 T182 SERIES SERVICE MANUAL D oew i_ 6 11 10 9 87 6 REDOVG OR INSTALLGE SHOCK PANEL I 3 i J Figure 15 1 Instrument Panel Sheet of 2 rtB15 2 15 2 ...
Page 374: ... 3 Removable Panel 4 Radio and Switch Panel 5 Fuel and Engine Instruments 6 Knee Pad 7 Heating and Ventilating Controls 8 Wing Flap Control 9 Engine Controls 10 Circuit Breaker Panel 11 Switch Panel 12 Nut 13 Washer 14 Shock Mount 15 Ground Strap 16 Threaded Button 17 Decorative Cover 18 Stud Figure 15 1 Instrument Panel Sheet 2 of 2 15 3 ...
Page 375: ...over pres tal and directional gyros is secured to the removable sure connections on instrument to prevent thread panel with rubber shock mounted assemblies Most damage and entrance of foreign matter Wire ter of the instruments are screw mounted on the panel minals should be insulated or tied up to prevent ac cidental grounding or short circuiting 15 5 REMOVAL AND INSTALLATION a FLIGHT INSTRUMENT P...
Page 376: ...re 1 Slowly apply positive pressure until altimeter system assuming altimeter has been tested and in indicates a 500 foot decrease in altitude and main spected in accordance with current Federal Aviation tain this altimeter indication while checking for leaks Regulations Coat line connections and static source flange with a Ensure static system is free from entrapped LEAK TEC or a solution of mild...
Page 377: ... BEGINNING WITH 18268490 1 Airspe 1 re eed Indicator 10 True Airspeed Ring 2 Altimeter 11 Instrument Panel Vertical Speed ndcator 1 Spacer 4 Static Line To Right Sump 13 Sump Plastic 5 Static Line To Left Sump 14 Static Port 6 Pttot Line To Pitot Tube 15 Fuselage Skin 7 Mounting Screw 16 HeaterElement Heated Pitot Only 8 Decorative Cover 17 Mast Body 9 Retainer 18 Connector I 19 Sump Metal Figure ...
Page 378: ...2 SERIES SERVICE MANUAL 2 NOTE See figure 15 2 for sump installation 1 Line To Instruments 4 Line Alternate Air 2 Line To Left Sump 5 Bracket 3 Line To Right Sump 6 Valve Figure 15 3 Alternate Static Air System 15 7 ...
Page 379: ...e connections for tight when necessary disconnect static line at first instru ness If hose or hose connections are used check ment to which it is connected then blow line to clear for general condition and clamps for security Re with low pressure air place hose which have cracked hardened or show other signs of deterioration 2 5 WITHOUT ALTERNATE STATIC SOURCE INSTALLED 2 WITH ALTERNATE STATIC SOU...
Page 380: ... may be applied sparing of tubing will be simpler if a guide wire is drawn in ly between tubing and fittings 15 17 TROUBLE SHOOTING PITOT STATIC SYSTEM TROUBLE PROBABLE CAUSE REMEDY LOW OR SLUGGISH AIRSPEED Normal altimeter and vertical Straighten tube repair or replace INDICATION speed pitot tube deformed damaged line leak or obstruction in pitot line INCORRECT OR SLUGGISH All three instruments l...
Page 381: ...lowing a small amount of air to enter static system To do this tilt end of suction hose away from opening then immediately tilt it back against opening Wait until vertical speed indicator approaches zero then repeat Con tinue to admit this small amount of air intermittently until all suction is released then remove test equipment TO APPLY PRESSURE Do not apply positive pressure with airspeed indic...
Page 382: ... valve Close for normal operation open HAND VIBRATES Excessive vibration caused by Tighten mounting screws loose mounting screws Excessive tubing vibration Tighten clamps and connections replace tubing with flexible hose 15 20 TROUBLE SHOOTING ALTIMETER NOTE Refer to paragraph 15 15 before blowing out pitot or static lines TROUBLE PROBABLE CAUSE REMEDY INSTRUMENT FAILS TO Static line plugged Blow ...
Page 383: ...TUBE DOES NOT HEAT OR Switch turned OFF Turn switch ON CLEAR ICE Popped circuit breaker Reset breaker Break in wiring Repair wiring Heating element burned out Replace element 15 23 VACUUM SYSTEM ing system is utilized The reading of the suction gage indicates net difference in suction before and 15 24 DESCRIPTION A dry vacuum system is after air passes through a gyro This differential installed on...
Page 384: ... F18200026 THRU F18200169 1 Suction Gage 8 Bolt 2 Directional Gyro 9 Suction Relief Valve 3 Gyro Horizon 10 Firewall 4 Bracket 11 Tube Locator 5 Cabin Skin 12 Overboard Line 6 Filter 13 Hose 7 Washer 14 Vacuum Pump Figure 15 6 Vacuum System Installation Sheet 1 of 3 15 13 ...
Page 385: ...0 12 11 BEGINNING WITH 18268404 8 Suction Relief Valve 1 Gyro Horizon 9 Firewall 2 Directional Gyro 10 Hose 3 Suction Gage 11 Vacuum Pump 4 Bracket 12 Overboard Tube 5 Filter 13 Vacuum Switch 7 6 Washer 14 Overboard Hose 7 Bolt 15 Cover 18267716 THRU 18268434 Figure 15 6 Vacuum System Installation Sheet 2 of 3 15 14 ...
Page 386: ...8 Suction Relief Valve 2 Directional Gyro 9 Firewall 3 Suction Gage 10 Hose 4 Bracket 11 Vacuum Pump 5 Filter 12 Overboard Line 6 Washer 13 Vacuum Switch 7 Bolt 14 Cover BEGINNING WITH 18268435 Figure 15 6 Vacuum System Installation Sheet 3 of 3 15 14A 15 14B blank ...
Page 387: ...r cleaning replace it 15 26 TROUBLE SHOOTING GYROS TROUBLE PROBABLE CAUSE REMEDY HORIZON BAR FAILS TO RE Central air filter dirty Replace filter SPOND Suction relief valve im Adjust or replace relief valve properly adjusted Faulty suction gage Replace suction gage Vacuum pump failure Replace pump Vacuum line kinked or Repair or replace damaged lines leaking tighten connections HORIZON BAR DOES NOT...
Page 388: ...must be changed avoid damage to gyro system When a com when installing a new pump Failure to do ponent is removed cap off and identify all so will void pump warranty DO NOT CON open lines hoses and fittings to prevent dirt NECT A PUMP BACKWARDS Since the from entering system and to ensure proper manifold check valves provide no pressure reinstallation Upon component replacement relief the pump wil...
Page 389: ...em components installed in aircraft The excessive pressures will damage gyros If an obstructed line is to be blown out c Position vacuum pump in a jaw protected vise disconnect at both ends and blow from with drive coupling downward instrument panel out instrument panel out low vacuum warning light is installed on the instru Pump housing should never be placed directly ment panel The light is cont...
Page 390: ...not properly Adjust relief valve adjusted Defective pump Check pump Replace pump Central air filter dirty Replace central air filter 15 30D REMOVAL See figure 15 6A 15 30E INSTALLATION See figure 15 6A a Make sure circuit breaker switch 1 and battery a If motor was removed from assembly position switch are off motor 26 and install washers 22 and nuts 21 b Remove clamps securing hoses 15 and 16 to ...
Page 391: ...RVICE MANUAL eee o q oooO O F NOT o do c t W o o o o a 1 Circuit Breaker Switch l i 2 Instrument Panel 182 1 2 Detail A A ____ Fi e 15 Stany Vacm Stm t of Figure 15 6A Standby Vacuum System Sheet 1 o15f r o w o o u o o 15 18A ...
Page 392: ...Washer 8 Firewall 9 Washer 24 22 10 Relief Valve 23 11 Hose to Directional Gyro 12 Hose to Gyro Horizon et B 13 Washer Detail 14 Nut 15 Hose to Manifold 16 Motor 17 Power Input Wire 18 Ground Wire 19 Fittings 20 Vacuum Pump 21 Nut 22 Washer 23 Bolt 24 Washer 25 Vent Hose Flgure 15 6A Standby Vacuum System Sheet 2 of 2 15 18B ...
Page 393: ...d pressure and ing coat lower two thirds with AC Type ST fuel pressure gage are in one instrument case How 640 speedometer cable grease or Lubriplate ever each instrument operates independently The No 110 Insert cable in housing as far as manifold pressure gage is a barometric instrument possible then slowly rotate to make sure it which indicates absolute pressure in the intake man is seated in th...
Page 394: ...s Repair or replace damaged line 15 39 TROUBLE SHOOTING FUEL PRESSURE GAGE TROUBLE PROBABLE CAUSE REMEDY DOES NOT REGISTER Pressure line clogged Check line for obstructions Blow out line Pressure line broken Check line for damage or leaks Repair or replace damaged line Fractured bellows or Replace instrument damaged mechanism Clogged snubber orifice Replace instrument Pointer loose on shaft Replac...
Page 395: ... sending unit not tion Unit SK182 43 isavailable and may be to exceed 4 inch pounds The Rochester and Stewart ordered through the Cessna Supply Division Warner gages are connected the same but the Rochester 15 42 TROUBLE SHOOTING TROUBLE PROBABLE CAUSE REMEDY GAGE INOPERATIVE No current to circuit Repair electrical circuit Defective gage bulb or Repair or replace defective circut items GAGE FLUCTU...
Page 396: ...to a tempeatr in lectricle lfSci of the elemeat dirdtcated bulb in th engine The temermeblb apiU ry tube by the gt calibratd for tmpertare Tbe sym ad gag ar filld with f lid nd mald zpmimn aMd requir powr from the aircraft lectrical sy olatetioofflitd in tbe bulbwithhtawrs u andprn d oprat y w inthe asnr switch mon Al peraes the ge Checkng capillrytube for damrg and thogh both inatrumet and sening...
Page 397: ...fective master switch Replace switch SCALE WITH CURRENT OFF Defective gage Replace gage 15 51 FUEL QUANTITY INDICATING SYSTEM 15 53 REMOVAL AND INSTALLATION OF TRANS MITTER Refer to section 12 15 52 DESCRIPTION The magnetic type fuel quan a Drain fuel from cell Observe the precautions tity indicators are used in conjunction with a float in Section 12 operated variable resistance transmitter in eac...
Page 398: ...R OPERATION Low voltage Correct ERRATIC READINGS Defective Defective master switch Replace switch 15 55 Referto page15 24A 15 56 HOrU TER See Fiure 15 7 15 57 DESCRPTIO The hrmetar is mae1ec ticaly operated asnnment aced by a pessre switch in the ol presure gage lne Electcal pwer is spplied throgh a ne amp fuse from the electrical clock circt and therefore will operate independm of the masr swtch ...
Page 399: ...e 3 Insert 4 Tube 5 Nut 6 Light 13 7 Compass Card 8 Compass 9 Mount 10 Lockwasher 11 Washer 12 Adapter 15 17 13 Hourmeter 14 Pressure Switch WS A 15 Positive Wire a 14 6 Ground Wire 1 B 17 Wire from Clock 16De oi CCircuit 12 18 O A T Gage 15 419 Rubber Washer 20 Knob 21 Air Vent 22 Washer Detail C 23 Plastic Washer 24 Nut Figure 15 7 Compass O A T Gage and Hourmeter Installation 15 24 ...
Page 400: ...situation Before installing transmitter attach electrical wires and place master switch in ON position Allow float arm to rest against lower float arm stop and read indicator The pointer should be on E empty position Adjust the float arm against lower stop so pointer indicator is on E Raise flat until arm is against upper stop and adjustupper stop to permit indicator pointer to be on F full Instal...
Page 401: ...n your aircraft from the left column and the temperature from the column headings Read the ohms value under the appropriate temperature column PartNumber Type 200 F 220 F 450 F 475 F S1372 1 CHT 310 0 34 8 S1372 2 CHT 310 0 34 8 S1372 3 CHT 113 0 S1372 4 CHT 113 0 82334 3 CHT 745 0 38 0 S2334 4 CHT 745 0 38 0 15 24B Revision 3 ...
Page 402: ...ARDOUS SITUATION B While the transmitter float arm is being actuated apply airplane battery electrical power as required to ensure that the fuel quantity indicator follows the movement of the transmitter float arm If this does not occur troubleshoot repair and or replace components as required until the results are achieved as stated NOTE Stewart Warner fuel quantity indicating systems can be adju...
Page 403: ...l quantity indicating systems can be adjusted Refer to instructions for adjusting Stewart Warner fuel indicating systems in this section Rochester fuel quantity indicating system components are not adjustable only component replacement or standard electrical wiring system maintenance practices are permitted 8 Install any items and or equipment removed to accomplish this procedure remove maintenanc...
Page 404: ...ace the EGT indicator hand over the 4 5 scale increment of the indicator scale Turning 15 64 DESCRIPTION The magnetic compass is the screw clockwise increases the reading and coun liquid filled with expansion provisions to compen terclockwise decreases the reading The adjusting sate for temperature changes It is equipped with screw has an adjustment range of approximately 600 F compensating magnet...
Page 405: ...mination Replace instrument TURN TO CENTER in the indicator dampening Friction in gimbal assembly Replace instrument DOES NOT INDICATE A Low voltage Correct voltage STANDARD RATE TURN TOO SLOW Inverter frequency changed Replace instrument NOISY MOTOR Faulty bearings Replace instrument ROTOR DOES NOT START Faulty electrical connection Correct voltage or replace faulty wire Inverter malfunctioning R...
Page 406: ... ZERO balance Hand incorrectly sits on rod Replace instrument Sensitivity spring adjustment Replace instrument pulls hand off zero IN COLD TEMPERATURES Oil in indicator becomes Replace instrument HAND FAILS TO RESPOND too thick OR IS SLUGGISH Insufficient bearing end play Replace instrument Low voltage Correct voltage NOISY GYRO High voltage Correct voltage Loose or defective rotor Replace instrum...
Page 407: ... Water to Battery 2122 16 14 Description 2K1 16 41 Testing the Battery 2I22 16 14 Removal Installation 2K1 16 41 Charging the Battery 2I23 16 15 Anti Collision Strobe Light 2K1 16 41 Battery Box 2I23 16 15 Description 2K1 16 41 Description 2I23 16 15 Operational Requirements 2K1 16 41 Removal Installation 2I23 16 1 Removal Installation 2K1 16 41 Maintenance of Battery Overhead Console 2K8 16 48 Bo...
Page 408: ...h panel battery is utilized An engine driven alternator is the normal source of power during flight and maintains a 16 11 AMMETER battery charge controlled by a voltage regulator An external power receptacle is offered as optional equip 16 12 DESCRIPTION The ammeter is connected ment to supplement the battery system for starting between the battery and the aircraft bus The meter and ground operati...
Page 409: ...reaker 12 Flashing Beacon Switch 27 Radio No 3 Circuit Breaker 13 Navigation Light Switch 28 Radio No 4 Circuit Breaker 14 Pitot Heat Switch 29 Radio No 5 Circuit Breaker 15 Avionics Master Switch 30 Flashing Beacon Circuit Breaker 16 Ignition Switch 31 Flap Circuit Breaker 17 Master Switch 32 Cabin Light Circuit Breaker 18 Bus Bar 33 Instrument Circuit Breaker 19 Strobe Light Circuit Breaker 34 P...
Page 410: ...DEL 182 T182 SERIES SERVICE MANUAL 8 9 10 11 12 13 14 15 16 17 s TT T 37 18 36 35 34 33 32 31 30 22 21 20 19 18 18 BEGINNING WITH 1981 MODELS 16 1 Switch and Circuit Breaker Installation Sheet 2 of 4 16 4 ...
Page 411: ...6 41 19 35 32 33 40 20 21 39 22 18 37 38 Aux Fuel Pump Switch 39 Fuel Pump Circuit Breaker 40 Fuel Quantity Circuit Breaker THRU 1982 MODELS 41 Taxi Light Circuit Breaker 42 Electric Trim Circuit Breaker T182 ONLY 16 1 Switch and Circuit Breaker Installation Sheet 3 of 4 16 5 ...
Page 412: ...I I S _ 1 I O TEI sULJ lao s s a s e isfJL 9ng a s U U IL 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 19 Landing Light Circuit Breaker 20 Taxi Light Circuit Breaker 21 Strobe Light Circuit Breaker 32 32 22 Flashing Beacon Circuit Breaker 23 Navigation Light Circuit Breaker 24 Cabin Light Circuit Breaker 25 Instrument Circuit Breaker 26 Fuel Quantity Circuit Breaker 27 Stall Warning Circuit Bre...
Page 413: ...ty battery replace the battery Faulty contactor or wiring 3 Measure voltage at master between contactor or master switch terminal smallest on switch contactor with master switch closed Normal indication is zero volts If voltage reads zero proceed to step 4 If a voltage reading is obtained check wiring between contactor and master switch Also check master switch Open coil on contactor 4 Check conti...
Page 414: ... Closing Circuit 5 Diode Board 15 Nylon Cover 24 Fuse Clock 6 Bracket Relay Mounting 16 Master Switch Wire 25 Bracket Fuse Mounting 7 Split Bus Power Relay 17 Wire to Battery Contactor 26 Resistor 8 Battery Closing Circuit 27 Diode 9 Battery Box Lid 18 External Power Cable 28 Solder Terminal 10 Battery Box 19 Battery Drain Tube 29 Spacer 20 Clamp 30 Screw THRU 18266075 AND F18200085 Figure 16 2 Ba...
Page 415: ... y 5 Positive Battery Cable 10 Nut 15 Diode Assembly 20 Bracket Fuse Mounting 16 Lasher 21 Resistor 13 Battery Contactor 17 Insulating Washer 22 Diode 18266076 THRU 18266523 AND 18 Fuse Battery Contactor 23 Solder Terminal F18200086 THRU F18200144 Closing Circuit 24 Screw Figure 16 2 Battery and Electrical Equipment Installation Sheet 2 of 6 16 9 ...
Page 416: ...ble to Starter 18 Starter Contactor 19 Firewall 20 Cable to Battery Contactor 21 Wire to Ammeter 22 Bolt 23 Wire to Starter Switch 24 Nipple 25 Ground Wire 26 Washer 27 Cover 28 Wire to Clock Fuse 29 Diode Assembly 30 Battery Contactor 31 Wire to Ground Service Diode 32 Cable to Ground Service Contactor 33 Wire to Master Switch Detail B 18266524 THRU 18267730 AND BEGINNING WITH F18200145 Figure 16...
Page 417: ... L n LF18200065 TR 18266978 THRD 182687 20 21 29 22 a THRU 1826 2 7 STARTER CONTACTOR Detail B 24 THRU 18266977 AND F18200129 THRU 18266977 AND F18200129 27 16 18266978 THRU 18268058 0 17 c S dL 21 13 s KI23 r 1 25 34 2 22 26 STARTER CONTACTOR 14 Figure 1Battery and Electrical Equipment Installation Sheet 4 of 6 16 11 16 11 ...
Page 418: ...ER CONTACTORS 12 1 Bolt 2 Cover 9 3 Battery 4 Cover Positive Te rminal 10 5 Drain Tube 6 Positive Cable 7 Ground Strap 8 Clamp 9 Bolt Detail B 10 TailconeSkin 11 Nut 12 Cover Battery Contactor BEGINNING WITH 18267731 Figure 16 2 Battery and Electrical Equipment Installation Sheet 5 of 6 16 12 ...
Page 419: ...ontactor 18 Wire to Master Switch 19 Wire to Starter Contactor 20 Wire to Ground Service 21 Diode Wire _Detail 22 Clock Fuse RSw Detail C 23 Fuse Battery Contactor C l DClosing Circuit 24 Nut 25 Lockwasher 26 Washer 27 Insulating Washer 28 Bracket 29 Spacer 30 Solder Terminal 31 Diode 32 Resistor BEGINNING WITH 18267731 Figure 16 2 Battery and Electrical Equipment Installation Sheet 6 of 6 16 13 ...
Page 420: ...e compensated for the temperature of the electrolyte 3 Cut sta strap and remove cover from positive Some hydrometers have a built in thermometer and battery terminal conversion chart The following chart shows the bat 4 Disconnect positive cable from battery tery condition for various hydrometer readings with 5 Disconnect drain tube from battery an electrolyte temperature of 80 Fahrenheit 6 Remove ...
Page 421: ...F actuated by turning the master switch on When the master switch is off the battery is disconnected from 16 22 BATTERY BOX THRU 18266523 AND the electrical system A silicon diode is used to F18200144 eliminate spiking of transistorized radio equipment The large terminal of the diode connects to the battery 16 23 DESCRIPTION The battery is completely terminal of the battery contactor The small ter...
Page 422: ...T 16 30 DESCRIPTION This circuit consists of a Failure to observe polarity when connecting 5 amp fuse a resistor and a diode mounted on a an external power source directly to the bat bracket on the side of the battery box This serves tery or directly to the battery side of the bat to shunt a small charge around the battery contactor tery contactor will damage the diodes in the so that ground power...
Page 423: ... tBatrCottr 1Doe12 Bar 19 Do 6 12 GuSreta o Detail A 10 THRU 1980 MODELS 1 Nylon Cover 8 Nipple 15 Screw 2 Sta strap 9 Nut 16 Receptacle 3 Nut 10 Washer 17 Rivet 4 Washer 11 Ground Strap 18 Doubler 5 Cable to Battery Contactor 12 Diode Board 19 Door 6 Ground Service Contactor 13 Bracket 20 Engine Cowl 7 Power Cable 14 Firewall 21 Wire to Diode Board Figure 16 3 Ground Service Receptacle Installati...
Page 424: ...rap 3 Bracket K 12 4 Receptacle 5 Doubler Detail B 6 Door 7 Engine Cowl 8 Diode Board 9 Contactor Wire 10 Ground Strap 11 Cable to Battery Contactor 12 Jumper Wire 13 Ground Service Contactor 14 Wire to Diode Board BEGINNING WITH 1981 MODELS Figure 16 3 Ground Service Receptacle Installation Sheet 2 of 2 16 18 ...
Page 425: ...ck for voltage at small terminal of ground service re ceptacle If voltage is not pre sent check ground service plug wiring If voltage is present proceed to step 3 Open or mis wired diode on 3 Check polarity and continuity ground service diode board of diode on diode board at rear of assembly ground service receptacle If diode is open or improperly wired replace diode board assembly Faulty external...
Page 426: ...breaker located on the instrument panel stalled The system is controlled by the left hand portion of the split rocker master switch labeled ALT The diode plates are connected to accomplish full wave rectification of the ac The resulting dc out 16 37 ALTERNATOR put is applied to the aircraft bus and sensed by the voltage regulator alternator control unit The regu 16 38 DESCRIPTION Thru 1977 Models ...
Page 427: ...with the voltage ex temperature chart in the Cessna Alternator Charging System Service Parts Manual If charge rate tapers off very quickly and volt age is normal check battery for malfunction If ammeter shows a low charge rate or any discharge rate and voltage is low proceed to step 2 2 Stop engine remove cowl and remove cover from voltage regulator Turn master switch ON OFF several times and ob s...
Page 428: ...ance If reading indicates no or poor continuity repair or replace alternator ground wiring ALTERNATOR OVERCHARGES Regulator faulty or improperly Check bus voltage with engine BATTERY BATTERY USES adjusted running Normal indication EXCESSIVE WATER agrees with voltage vs temper ature chart on page 16 13 Ob serve ship s ammeter ammeter should indicate near zero after a few minutes of engine operation...
Page 429: ... reading in the other direction If an infinite reading is not ob tained in at least one direction repair or replace alternator ALTERNATOR REGULATOR Short in Over Voltage Disconnect Over Voltage Sensor CIRCUIT BREAKER OPENS sensor plug and recheck If circuit WHEN BATTERY AND breaker stays in replace Over ALTERNATOR SWITCHES Voltage Sensor ARE TURNED ON Short in alternator voltage Disconnect regulat...
Page 430: ...ow continuity in one direction but should show an infinite reading in the other direction If an infinite reading is not obtained in at least one direction repair or replace alternator OVER VOLTAGE LIGHT DOES Shorted regulator Replace regulator NOT GO OUT WHEN ALTER NATOR AND BATTERY SWITCHES ARE TURNED ON Defective over voltage Replace sensor sensor AFTER ENGINE START Regulator faulty or high With...
Page 431: ...does not rise when alternator switch is turned on proceed to step 2 2 Stop engine turn off all switches Connect voltmeter between F terminal of alternator and ground Do NOT start engine Turn on battery switch and alternator switch Battery voltage should be present at F terminal less 1 volt drop thru regulator if not refer to step 3 3 Starting at F terminal of alternator trace circuit to voltage re...
Page 432: ...tery Switch ON Alter alternator case Reverse nator Switch OFF all leads and check again Resis other electrical switches tance reading may show con OFF tinuity in one direction but should show an infinite reading in the other direction If an infinite reading is not obtained in at least one direction repair or replace alternator ALTERNATOR REGULA Short in alternator control Disconnect Over Voltage T...
Page 433: ...nuity in one direction but should show an infinite reading in the other direction If an infinite reading is not obtained in one direction repair or replace alternator LOW VOLTAGE LIGHT Shorted alternator control Replace alternator control unit DOES NOT GO OUT WHEN unit ALTERNATOR AND BAT TERY SWITCHES ARE Defective low voltage Replace alternator control unit TURNED ON sensor AFTER ENGINE START Alt...
Page 434: ...ernator output voltage 2 Stop engine turn off all insufficient cont switches Connect voltmeter between F terminal of alternator and ground Do NOT start engine Turn on battery switch and alternator switch Battery voltage should be present at F terminal less 1 volt drop thru regulator if not refer to Step 3 3 Starting at F terminal of alternator trace circuit to alternator control unit at Pin 1 Blue...
Page 435: ...t On New aircraft or whenever a new belt is installed belt tension should be checked within 10 to 25 hours 16 47 ALTERNATOR CONTROL UNIT of operation h On 95 amp alternator or on initial installation of 16 48 DESCRIPTION The alternator control unit new belt adjust belt tension to 75 Lb thereafter belt is a solid state voltage regulator with an over voltage tension should be 58 to 72 Lb sensor and ...
Page 436: ...bracket refer to Cessna Single Engine 4 Rubber Bushing Customer Care Service Information 5 Bolt Letter SE79 58 Dated May 12 1980 6 Upper Adjusting Bolt 7 Drive Belt 8 Bushing 9 Bonded Mount 10 Nut 11 Support Asembly THRU 18266408 18266413 18266415 THRU 18266418 12 Figure 16 4 Alternator Installation Sheet 1 of 3 16 30 ...
Page 437: ...IES SERVICE MANUAL TORQUE TO 165 10 IN LBS TORQUE TO 450 500 IN LBS TORQUE TO 200 270 IN LBS BEGINNING WITH 18266409 THRU 18266412 18266414 18266419 AND 18266542 ON Figure 16 4 Alternator Installation Sheet 2 of 3 16 31 ...
Page 438: ...MODEL 182 T182 SERIES SERVICE MANUAL 6 2 14 13 Cover 16 Sta strap MODEL T182 95 AMP ALTERNATOR Figure 16 4 Alternator Installation Sheet 3 of 3 16 32 ...
Page 439: ...l energy must be practiced until the flight can be tive action should be followed terminated The over voltage red warning light fila a Inspect COM coax connections at the radios and ment can be tested by turning off the Alternator por antennas for security and proper installation tion of the Master Switch and leaving the Battery por Replace as required tion turned on This test does not induce an o...
Page 440: ...ES SERVICE MANUAL Detail A 1 Voltage Regulator 5 Housing Plug 2 Firewall 6 Screw 3 Ground Wire 7 Over Voltage Sensor 4 Housing Cap 8 Nut 1978 MODELS Figure 16 5 Voltage Regulator Alternator Control Unit Sheet 2 of 4 16 34 ...
Page 441: ...UAL 4 Screw 11 Alternator Control Unit 5 Terminal Block 12 Ground Wire 6 Firewall BEGINNING WITH 1979 MODELS 13 Bolt 7 Cover Terminal Block 14 Housing Plug Figure 16 5 Voltage Regulator Alternator Control Unit Sheet 3 of 4 16 35 16 35 ...
Page 442: ...MODEL 182 T182 SERIES SERVICE MANUAL THRU 18258408 BEGINNING WITH 18268409 MODEL T182 ONLY Figure 16 5 Voltage Regulator Alternator Control Unit Sheet 4 of 4 16 36 ...
Page 443: ...tch LANDING OR TAXI LIGHT Lamp burned out 1 Test lamp with ohmmeter or OUT new lamp Replace lamp Open circuit in wiring 2 Test wiring for continuity Repair or replace wiring 1 Inspect circuit breaker If FLASHING BEACON DOES Short circuit in wiring circuit breaker is open proceed NOT LIGHT to step 2 If circuit breaker is OK proceed to step 3 Defective wiring 2 Test circuit until short is lo cated R...
Page 444: ...epair or replace wiring The anti collision system is a high voltage device Do not remove or touch tube assembly while in operation Wait at least 5 minutes after turning off power before starting work BOTH ANTI COLLISION Open circuit breaker 1 Check if open reset If STROBE LIGHTS WILL circuit breaker continues to NOT LIGHT open proceed to step 2 2 Disconnect red wire be tween aircraft power supply ...
Page 445: ...er and strobe power sup ply connecting negative lead to wing structure Check for 12 volts thru 1977 models and 24 volts beginning with 1978 models If OK proceed to step 2 If not check aircraft power supply battery external power 2 Replace flash tube with known good flash tube If system still does not work replace strobe power supply 1 Inspect circuit breaker If DOME LIGHT TROUBLE Short circuit in ...
Page 446: ... light switch turned off 1 Nav light switch has to be LIGHT WILL NOT LIGHT ON before map light will light Short circuit in wiring 2 Check lamp fuse on terminal board located on back of station ary panel with ohmmeter If fuse is open proceed to step 3 If fuse is OK proceed to step 4 Defective wiring 3 Test circuit until short is lo cated Repair or replace wiring 4 Test for open circuit Repair or re...
Page 447: ...each wing tip A maximum of two washers may be used rib between support 2 and plate 3 for ad justment 16 67 OPERATIONAL REQUIREMENTS THRU 1977 MODELS f Connect wires to lamps and install cowl g Check lights for operation The capacitors in the strobe light power 16 58 ADJUSTMENT OF LANDING AND TAXI supplies must be reformed if not used for LIGHT See figure 16 6 Adjustment of the a period of six 6 mo...
Page 448: ...may be used to secure lamp 5 be tween bracket 6 and plate 3 A maximum of two washers Detail A may be used between support 2 and plate 3 for adjustment 1 Nose Cap 2 Landing Light Support 3 Plate 4 Gasket 5 Lamp 6 Bracket 7 Screw 8 Tinnerman Screw Figure 16 6 Landing and Taxi Light Installation 16 42 ...
Page 449: ...na Single engine Service Letter SE76 13 dated June 14 1976 1 Electrical Leads 17 Lamp 2 Cap 7 Housing Plug 12 Flash Tube Assembly 18 Seal 3 Washer 8 Housing Cap 13 Lens 19 Grounding Washer 4 Insulated Washer 9 Wing Tip 14 Screw 20 Power Supply 5 Spring 10 Lamp Socket 15 Lens Retainer 21 Bolt 6 Insulator 11 Spacer 16 Gasket 22 Wing Tip Rib Figure 16 7 Navigation and Anti Collision Strobe Light Inst...
Page 450: ... T182 SERIES SERVICE MANUAL 7 14 Detail A BEGINNING WITH 18266076 15 AND F18200086 22 Detail C 14 20 BEGINNING WITH 18265300 Figure 16 7 Navigation and Anti Collision Strobe Light Installation Sheet 2 of 2 16 44 ...
Page 451: ... the lamp r y NOTE Detail A Fingerprints on lamp may short en the life of the lamp 1 Lens 10 Flasher 2 Gasket 11 Ground Wire 3 Lamp 12 Fin Assembly 4 Screw 13 Housing Plug 5 Baffle 14 Housing Cap 6 Clamp 15 Ground Wire 7 Socket 16 Resistor 8 Nutplate 17 Ground Wire 9 Tip Assembly 18 Wire to Flasher Figure 16 8 Flashing Beacon Light Installation Sheet 1 of 3 16 45 ...
Page 452: ...MODEL 182 T182 SERIES SERVICE MANUAL 2 r 8 9 14 10 Figure 16 8 Flashing Beacon Light Installation Sheet 2 of 3 16 46 ...
Page 453: ...NOTE When installing lamp be sure socket assembly is installed in mounting plate so lamp may be installed with filament per pendicular to the longitudinal axis of the aircraft Figure 16 8 Flashing Beacon Light Installation Sheet 3 of 3 16 47 ...
Page 454: ...ontroled by the in assembly with a tinted lens The intensity of the strument light dimming rheostat located on the post lights is controlled by the instrument light swithc panel dimming rheostat located on the switch panel 16 74 REMOVAL AND INSTALLATION See figure 16 9 and 16 10 NOTE 16 75 ELECTROLUMINESCENT PANEL LIGHTING When installing postlight assemblies assemblies shall be coated with RTV 10...
Page 455: ...ND INSTALLATION See outer portion controls engine instrument and radio figure 16 9 for removal and installation lighting The right hand is a single rheostat and con trols instrument lighting this includes glare shield 16 86 MAP LIGHT lights instrument flood lights compass light and post lighting if installed 16 87 DESCRIPTION A light assembly is installed in the instrument panel galre shield above...
Page 456: ...Bracket 12 8 Speaker 9 Grill Speaker 10 Socket 11 Lamp 12 Cover Assembly 13 Socket Post Light 2 14 Lamp Assembly 15 Slide Cover 16 Slide Knob 17 Switch 13 18 Lens 19 ShieldK 20 Cover Plate 21 Lockwasher 15 22 Nut 23 Ground Wire 2 16 Figure 16 9 Overhead Console Dome Light and Courtesy Light Installation Sheet 1 of 2 16 49 ...
Page 457: ...EL 182 T182 SERIES SERVICE MANUAL 7 17 10 7 0 21 2 7_ 7 2 i1s 1 BEGINNIGT WITH 182006774 THRU 182006773 3 11 22 2 Figure 16 9 Overhead Console Dome Light and Courtest Light Installation Sheet 2 of 2 16 50 ...
Page 458: ...ERVICE MANUAL A 6 IA CF I P qg 33 3 _ 4 S h i l DelellB m_ De il C Detail A Detail C 1 Cover 2 Light Housing 3 Nutplate 4 Shield 5 Screw 6 Switch Map Light Figure 16 10 Instrument Panel Glareshield Lighting Installation 16 51 ...
Page 459: ... Washer 12 Set Screw 3 Washer 8 Heat Sink 13 Control Instrument Lighting 4 Nut 9 Mounting Bracket 14 Control Engine Inst and Radio lighting 5 Glove Box 10 Housing Socket 15 Control Lower Panel Lighting Figuer 16 11 Transistorized Light Dimming and Electroluminescent Light Inverter Installation 16 52 ...
Page 460: ... 1981 MODELS 1 Control Tube Assembly 9 Mike Switch 2 Cover 10 Plug 3 Adapter 11 Insulator 4 Connector 12 Plug 5 Plate 13 Lamp Assembly 6 Map Light Rheostat 14 Map Light Socket 7 Control Wheel 15 Knob Map Light 8 Pad 16 Connector Circuit Board Figure 16 12 Control Wheel Map Light Installation Sheet 1 of 2 16 53 ...
Page 461: ...VICE MANUAL 1 Control Tube Assembly 2 Adapter 3 Map Light Rheostat 4 Control Wheel 5 Pad 6 Map Light Socket 7 Lamp 8 Knob Map Light BEGINNING WITH 1982 MODELS Figure le 12 Control Wheel Map Light Installation Sheet 2 of 2 16 54 ...
Page 462: ...lighter becomes jammed in the socket or held in wing and is actuated by airflow over the surface of position too long The circuit breaker may be reset the wing The switch will close as a stall condition by inserting a small probe into the 078 diameter is approached actuating the warning horn which is hole in the back of the circuit breaker and pushing mounted on the glove box The stall warning uni...
Page 463: ...MODEL 182 T182 SERIES SERVICE MANUAL 2 1 Shield 2 Socket 3 Cover T182 BEGINNING WITH 1982 MODELS 4 Lamp Figure 16 13 Pedestal Lighting Sheet 1 of 2 16 56 ...
Page 464: ...MODEL 182 T182 SERIES SERVICE MANUAL 3 MODEL 182 AND ON T182 THRU 1981 MODELS Figure 16 13 Pedestal Lighting Sheet 2 of 2 16 57 ...
Page 465: ...etailD BEGINNING WITH 18268056 1 Glove Box 8 Wing Leading Edge 13 2 Rivet 9 Stall Warning Actuator 3 Nut 10 Heater Assembly 4 Washer 11 Pitot Tube 5 Bracket 12 Screw 6 Stall Warning Horn 13 Bulkhead 7 Tinnerman Nut 14 Insulation Washer Figure 16 14 Pitot Heat and Stall Warning Installation 16 58 ...
Page 466: ...MODEL 182 T182 SERIES SERVICE MANUAL 7 8 5 1 1 Knob 2 Element 3 Socket 4 Pawel 5 Shell 6 Circuit Breaker 7 Probe 8 Nut 9 Lockwasher 10 Power Wire Figure 16 15 Cigar Lighter Installation SHOP NOTES 16 59 ...
Page 467: ...feet When battery inspection and replacement imately one second The control tower should schedules are adhered to the transmitter will broad be notified that a test is about to be performed cast an emergency signal at rated power 75 MW minimum for a continuous period of time as listed NOTE in the following table Without its antenna connected the ELT will TRANSMITTER LIFE produce sufficient signal ...
Page 468: ...OTE Metal Strap 4 must be positioned so that latch is on top of transmitter as installed in the aircraft and not across transmitter cover 1 Cover 9 Co axial Cable 2 Transmitter 10 Arm Switch 3 Fabric Fastener Pile 11 Connector 4 Metal Strap 12 Rubber Washer 5 Fabric Fastener Hook 13 Rubber Boot 6 Bracket 14 Antenna 7 Tailcone Skin 15 Doubler 8 Sta strap 16 Placard Figure 16 16 Emergency Locator Tr...
Page 469: ...card from the towards the nose of the aircraft end of transmitter and replace with new battery pack placard supplied with the new battery pack 16 107 REMOVAL AND INSTALLATION OF ANTEN NA See figure 16 16 a Disconnect co axial cable from base of antenna b Remove the nut and lockwasher attaching the Be sure to enter the new battery pack expira antenna base to the fuselage and the antenna will be tio...
Page 470: ...a Simpson Model 1223 ammeter to thejack c Set the toggle switch to ON and observe the ammeter current drain Ifthe current drain is in the 85 100 ma range the trans mitter or the coaxial cable is faulty Faulty coaxial 4 Check coaxial antenna cable for high antenna cable resistance joints Ifthis is found to be the case the cable should be replaced This test should be carried out with the coaxial cab...
Page 471: ...ack This date is supplied on a sticker attached to the outside of the ELT case and to each battery Power is supplied to the transmitter by a battery pack The C589511 0114 alkaline battery packs have the 16 114 REMOVAL AND INSTALLATION OF TRANS service life of the battery pack stamped on the battery MITTER See figure 16 18 pack on the end of the transmitter below the switch a Remove baggage curtain...
Page 472: ...in Skin 7 Arm Switch 2 Bracket 8 Co axial Cable 3 Transmitter 9 Rubber washer 6 r 4 Cover 10 Rubber Boot 5 Screw 11 Antenna C 6 Battery Pack 12 Doubler DeRO TaDI18 Figure 16 18 Emergency Locator Transmitter Installation Sheet 1 of 3 16 65 16 65 ...
Page 473: ...MODEL 182 T182 SERIES SERVICE MANUAL 11 THRU 1980 MODELS 1981 MODELS 18266591 THRU 18268308 Detail C ROTATED 180 Figure 16 18 Emergency Locator Transmitter Installation Sheet 2 of 3 16 66 ...
Page 474: ... B S oxDti Detail AWITH 182 BEGINNING WITH 18268309 ELT IS LOCATED BEHIND THIS SURFACE 6 PLACARD LOCATED ON RIGHT 5 HAND 8IDE OF TAILCONE ADJACENT TO ELT ON CANADIAN AIRCRAFT Detail C ROTATED 180 Figure 16 18 Emergency Locator Transmitter Installation Sheet 3 of 3 16 67 ...
Page 475: ...alent to antenna whip only do not apply adhesive to fuse lage skin or damage to paint may result 16 116 REMOVAL AND INSTALLATION OF BAT TERY PACK See figure 16 19 NOTE Transmitters equipped with the C589511 0105 or C589511 0106 battery packs can only be replaced with a C589511 0114 after modification by SK185 20 has been com pleted C58511 0105 BATTERY PACK C589511 0106 BATTERY PACK iCAUTION CANADI...
Page 476: ...with paragraph 16 114 TROUBLE PROBABLE CAUSE REMEDY POWER LOW Low battery voltage 1 Set toggle switch to off 2 Disconnect the battery pack from the transmitter and connect aSimpson Model 260 voltmeter and measure voltage If the battery pack voltage is 7 5volts or less the battery pack is below specification Faulty transmitter 3 Ifthe battery pack voltage meets the specifictions in step 2 the batte...
Page 477: ... 0 Cessna 00A Nawomitlc Type AF 395A 2 5 2 5 2 5 2 5 2 5 2 5 2 5 With Unsavd HS IG 832C 2 8 2 8 2 8 2 8 2 8 Cesa 300 Nav Com Type RT 385A 1 0 1 0 1 1 0 1 0 1 0 2 3S 2 3 2 3 2 3 2 3S 2 3 Cessna 400 Nav Com Type RT 485A 1 6 1 6 1 6 1 6 1 6 1 6 4 0 4 4 0 4 0 4 0 4 0 4 0 Cessna 400 ADF Type RT 485A 1 6 1 6 6 1 6 1 6 1 6 4 0 40 4 0 4 0 4 0 4 0 Cessna 400 ADF Type R 446A 6 1 1 3 1 6 1 1 6 1 1 6 1 6 Cess...
Page 478: ...5 0 25 0 25 0 25 Wing Courtesy Lights and Cabin Lights 5 1 2 1 2 1 2 1 2 1 2 1 2 Landing Lights 15 6 Flap Motor 15 0 10 0 10 0 8 5 8 5 8 5 8 5 Landing Lights Dual ea 3 6 ea 3 6 ea 3 6 ea 3 6 ea 3 6 ea Electric Elevator Trim 0 7 0 7 0 7 0 7 0 7 0 7 Map Light Control Wheel 0 1 0 1 0 1 0 1 0 1 0 1 Air Conditioning 19 7 19 7 Only one or the other may be used at one time t Negligible Receive Transmit 1...
Page 479: ...6 1 6 1 6 4 0 4 0 4 0 Cessna 400 ADF Type R 446A 1 6 1 6 1 6 Cessna Glideslope Type R 443B 0 5 0 5 0 5 Cessna 400 Transponder Type RT 459A 2 0 2 0 2 0 Cessna 400 Marker Beacon Type R 4 0 1 0 1 0 1 Cessna 400 DME RT 477A 15 1 5 1 5 Cessna 400 RNAV RN 479A 1 0 1 0 1 0 Sunair SSB Transceiver Type ASB 125 2 5 2 5 2 5 7 5 7 55 Flashing Beacon 6 0 7 0 7 0 Post Lights 0 8 0 8 Blind Encoder 01 0 1 0 1 Ces...
Page 480: ...heads 3A7 18 5 Damage Necessitating Repair After Hard Replacement of Part 3A5 18 3 Landing 3A7 18 5 Wing Ribs 3A5 18 3 Firewall Damage 3A7 18 5 Negligible Damage 3A5 18 3 Engine Mount 3A7 18 5 Repairable Damage 3A5 18 3 Description 3A7 18 5 Damage Necesitating General Considerations 3A7 18 5 Replacement of Parts 3A5 18 3 Engine Mount Support Wing Spars 3A5 18 3 Cradle Damage 3A7 18 5 Negligible Da...
Page 481: ...rmed auxiliary spar assembly and formed sheet figure 18 1 The fuselage assembly from the tail metal nose intermediate and trailing edge ribs cane to the firewall must NOT be supported from Stressed skin riveted to the rib and spar structures the underside since the skin bulkheads are not de completes the rigid structure Access openings signed for this purpose Adapt support stands to hand holes wit...
Page 482: ...in position without the filler material could not be made between adjacent ribs refer to the following paragraph 18 19 DAMAGE NECESSITATING REPLACEMENT OF PARTS If a stringer is so badly damaged that 18 35 DAMAGE NECESSITATING REPLACEMENT more than one section must be spliced replacement OF PARTS Where extreme damage has occurred is recommended complete leading edge skin panels should be replaced ...
Page 483: ... 48 ELEVATORS AND RUDDER 18 57 FUSELAGE 18 49 NEGLIGIBLE DAMAGE Refer to paragraph 18 58 DESCRIPTION The fuselage is of semi 18 13 The exception to negligible damage on the monocoque construction consisting of formed bulk elevator surfaces is the front spar where a crack heads longitudinal stringer reinforcing channels appearing in the web at the hinge fittings or in the and skin panels structure ...
Page 484: ... crack that progresses past a stop drilled hole shall be repaired Refer to paragraphs 18 40 41 and 42 as applicable for repair information 5 A control surface that has any of the following conditions shall have a repair made as soon as practicable A A crack that is longer than 2 inches B A crack that does not originate from the trailing edge or a trailing edge rivet C Cracks in more than six trail...
Page 485: ...ain inservice without additional repair 18 49A CRACKS IN CORRUGATED ELEVATOR SKINS Continued from page 18 4 1 It is permissible to stop drill crack s that originate at the trailing edge of the control surface provided the crack is not more than 2 inches in length 2 Stop drill crack using a 30 128 inch drill 3 A crack may only be stop drilled once NOTE A crack that passes through a trailing edge ri...
Page 486: ...members irregularly 18 70 DAMAGE INVOLVING ENGINE MOUNTING formed to provide clearance for control cables fuel LUGS AND ENGINE MOUNT TO FUSELAGE ATTACH lines etc the patch type repairs will be for the ING FITTINGS Engine mounting lugs and engine most part impractical Minor damage consisting mount to fuselage attaching fittings should not be re of small nicks or scratches may be repaired by paired ...
Page 487: ... constructed components on the quired Hi shear rivets are special patented rivets aircraft may be repaired as stipulated in instructions having a hi shear strength equivalent to that of stan furnished in Service Kit SK182 12 Observe the resin dardAN bolts They are used in special cases in manufacturer s recommendations concerning mixing locations where hi shear loads are present such as and applic...
Page 488: ...8D5 050 NAS1398B6 NAS1398D6 NAS1398B5 NAS1738E5 CR3213 5 040 NAS1738B6 NAS1738E6 NAS1768D5 CR3213 6 CR3243 5 032 CR3243 6 MS20470AD6 080 NAS1398B6 071 NAS1398D6 063 NAS1738B6 NAS1738D6 NAS1768D6 CR3213 6 050 CR3243 6 MS20426AD3 063 NAS1399B4 NAS1399D4 Countersunk 040 NAS1769D4 CR3212 4 See Note 1 025 NAS1769B4 NAS1739E4 CR3242 4 MS20426AD4 080 NAS1399B4 NAS1399D4 Countersunk 063 NAS1739B4 NAS1739D...
Page 489: ...D5 Dimpled 090 NAS1739B6 NAS1739D6 CR3212 6 MS20426AD6 Countersunk 071 NAS1769D6 063 CR3242 6 032 AN509 10 Screw with MS20365 Nut MS20426AD6 090 NAS1739B6 NAS1739D6 Dimpled 032 AN509 10 Screw with MS20365 Nut NOTE 1 Rework required Countersink oversize to accommodate oversize rivet NOTE 2 Do not use blind rivets in high vibration areas or to pull heavy sheets or extrusions together High vibration ...
Page 490: ...AS464 AN364 MS20304 MS21042 o NAS1103 NAS1305 NAS6203 NAS14XX NAS1080C NAS529 NAS524A NAS1080E NAS1446 NAS1080C NAS1080A6 NAS1080G NAS7034 NAS1080K o NAS464 AN364 MS20364 MS21042 NAS1103 NAS1303 o NAS6203 NAS529 NAS524A See Note 3 NAS1446 NAS1080C NAS1080A6 NOTE 1 See appropriate tables for nominal diameters available NOTE 2 Available in oversize for repair of elongated holes Ream holes to provide...
Page 491: ...IR OF GLASS FIBER CONSTRUCTED concerning mixing and application ofthe resing COMPONENTS Glass fiber constructed components Epoxy resins are preferable for making repairs on the aircraft may be repaired as stipulated in in since epoxy compounds are usually more stable and structions furnished in Service Kit SK182 12 Ob predictable than polyester and in addition give serve the resin manufacturer s r...
Page 492: ... periodically 3 Tape two bolts to straightedge according to dimension C 4 Locate inboard wing station to be checked and make a pencil mark approximately one half inch aft of the lateral row of rivets in the wing leading edge spar flange 5 Holding straightedge parallel to wing station staying as clear as possible from cans place longer bolt on pencil mark and set protractor head against lower edge ...
Page 493: ...im tabs installed all foreign matter removed from inside of control surface elevator trim tab push pull rod installed and all tips installed 4 Place balancing mandrels on a table or other suitable flat surface 5 Adjust trailing edge support to fit control surface being balanced while cen ter of balancing beam is directly over hinge line Remove balancing beam and balance the beam itself by moving t...
Page 494: ...ng bar stock solder to weight after removal from control surface The ailerons should have balance weight increased by or dering additional weight and attaching bracket listed in applicable Parts Catalog and installing next to existing inboard weight the minimum length necessary for correct balance However install weights and attaching brackets in lengths which contain at least two attaching rivets...
Page 495: ...nce in this range is underbalance BALANCING MANDREL Detail F RUDDER 90 Detail G LESPIET LEVEL TRAILINO EDGE 18 SU0PROTRACTOR PPORT J SLIDING CENTER LINE I i CHORD LINE BALANCING MANDREL D H LEVELED SURFACE HINGE POINT ELEVATOR Figure 18 3 Control Surface Balancing Sheet 3 of 6 18 10 ...
Page 496: ...AL PLANE aance aileron i nverted with trailing edge at point op Balance aileron inverted with trailing edge at point op posite cut out for middle hinge 85 below hinge line horizontal plane DETAL A A Figure 18 3 Control Surface Balancing Sheet 4 of 6 18 11 ...
Page 497: ...NDERBALANCE is defined as the condition that exists when surface is trailing edge heavy and is defined by a symbol If the balance beam sliding weight must be on the leading edge side of the hinge line to balance the control surface the control surface is considered to be underbalanced OVERBALANCE is defined as the condition that exists when surface is leading edge heavy and is defined by a symbol ...
Page 498: ... APPROVED FLIGHT CONFIGURATION CONTROL SURFACE BALANCE LIMITS Inch Pounds AILERON 0 0 to 9 64 RUDDER 0 0 to 6 7 RIGHT ELEVATOR 0 0 to 20 47 LEFT ELEVATOR 0 0 to 20 47 Figure 18 3 Control Surface Balancing Sheet 6 of 6 18 12A 18 12B blank ...
Page 499: ...R EXISTING 5 00 DIA SKIN 2 00 DIA HOLE SECTION THRU PATCH PATCH REPAIR FOR 2 INCH DIAMETER HOLE 2 50 DIA MS20470AD4 RIVETS EXISTING 8 REQD S IN PATCH i1 75 DIA 1 00 DIA HOLE C On firewall sheet repair SECTION THRU PATCH use MIL S 5059 corrosion resistant 18 8 steel On firewall sheet repair use MS20450C rivets PATCH REPAIR FOR 1 INCH DIAMETER HOLE ORIGINAL PARTS 1 REPAIR PARTS OVERLAPPING REPAIR PA...
Page 500: ...T SPACING 1 2 RADIUS I R i lil I _ EDGE MARGIN 2 X RIVET DIA DOUBLER 2024 T3 ALCLAD On firewaKll sheet repair use MIL S 5059 corrosion RIlVET R TS L N DOAAVERLAPPING REC SKIN GAGE RIVET DIA On firewall sheet repair TANGUAR PATCH 020 1 use MS20450C rivets T _ 025 1 8 ORIGINAL PARTS 032 I1 8 1 2 m i 1 2 i I 040 1 8 1 REPAIR PARTS 051 5 32 REPAIR PARTS IN CROSS SECTION Figure 18 4 Skin Repair Sheet 2...
Page 501: ...GIN A 2 X RIVET DIA CLEAN OUT _ IS 0 l DAMAGED AREA 1 2 RADIUS RIVET SPACING AoS e eX 6 X RIVET DIA A _ EDGE MARGIN tC C 2 X RIVET DIA DOUBLER 2024 T3 ALCLAD 0 O O v 1 2 RADIUS On firewall sheet repair use MIL S 5059 corrosion 1 2 RADIUS RIVET T LE resistant 18 8 steel On firewall sheet repair FLUSH RECTANGULAR PATCH SKIN GAGE RIVET DIA use MS20450C rivets CIRCULAR FLUSH PATCH IS 020 1 8 I ORIGINA...
Page 502: ...LER EXISTING SKIN PATCH 2D MIN SKIN GAGE RIVET DIA 051 5 32 On firewall sheet repair use MIL S 5059 corrosion resistant 18 8 steel On firewall sheet repair use MS20450 rivet NOTE REPAIR PARTS CROSS SECTION Figure 18 4 Skin Repair Sheet 4 of 6 18 16 ...
Page 503: ...5 MIN RADIUS TYPICAL _ S I r EDGE DISTANCE 2D MIN RIVET TRBLE M SKIN GAGE RIVET DIA 020 1 8 A 025 1 8 032 1 8 040 1 8 051 5 32 L LJ k PATCH OVERLAPPING PATCH AT STRINGER BULKHEAD L INTERSECTION I On firewall sheet repair use MIL S 5059 corrosion I resistant 18 8 steel On firewall sheet repair use MS20450C rivets ORIGINAL PARTS I REPAIR PARTS REPAIR PARTS IN CROSS SECTION Figure 18 4 Skin Repair Sh...
Page 504: ...D r 1 _ l Za MS20470AD4 R IVTS4 On firewall sheet repair use MIL S 5059 corrosion resistant 18 8 steel On firewall sheet repair A use MS20450C rivets ORIGINAL PARTS 1 REPAIR PARTS _ REPAIR PARTS IN CROSS SECTION Figure 18 4 Skin Repair Sheet 6 of 6 18 18 On firewa11 sheet repair 1 ...
Page 505: ...T4 ALCLAD 1 4 EDGE MARGIN RIVET SPACING TO MATCH 6 RIVETS EACH SIDE STRINGER OF DAMAGED AREA CLEAN OUT DAMAGED AREA LLER 2024 T4 ALCLAD A A MS20470AD4 RIVETS SKIN REPAIR PARTS IN CROSS SECTION Figure 18 5 Stringer and Channel Repair Sheet 1 of 4 18 19 ...
Page 506: ... 2024 T4 ALCLAD A A STRIP 2024 T3 ALCLAD 1 4 EDGE MARGIN CLEAN OUT OF DAMAGED AREA ANGLE 2024 T4 ALCLAD SPACING PICK UP EXISTING SKIN RIVETS ORIGINAL PARTS REPAIR PARTS IN CROSS SECTION Figure 18 5 Stringer and Channel Repair Sheet 2 of 4 18 20 ...
Page 507: ... 182 T182 SERIES SERVICE MANUAL 3 4 RIVET DOUBLER 2024 T4 ALCLAD MS20470AD4 RIVETS ORIGINAL PARTS SKIN REPAIR PARTS REPAIR PARTS IN CROSS SECTION A Figure 18 5 Stringer and Channel Repair Sheet 3 of 4 18 21 ...
Page 508: ...AREA 1 4 RADIUS T y CL e e 2 ROWS RIVETS OUTBOARD Y t v tC OF LIGHTENING HOLE DOUBLER 2024 T4 ALCLAD C CHANNEL 3 4 RIVET T s SPACING 1 4 MARGIN Oe MS20470AD4 RIVETS DOUBLER 2024 T4 ALCLAD i A II ORIGINAL PARTS REPAIR PARTS REPAIR IN CROSS SECTION Figure 18 5 Stringer and Channel Repair Sheet 4 of 4 18 22 ...
Page 509: ...AL 0 air STOPDRILL CRACK IF CRACK DOES NOT EXTEND TO EDGE OF PART DOUBLER 2024 T3 ALCI AD em l 1 4 EDGE MARGIN A A M IS20470AD4 RIVETS l ORIGINAL PARTS REPAIR PARTS REPAIR PARTS IN CROSS SECTION Figure 18 6 Rib Repair Sheet 1 of 2 18 23 ...
Page 510: ... T3 ALCLAD 3 4 RIVET Q S SPACING CLEAN OUT DAMAGED AREA 1 4 EDGE MARGIN s al ANGLE 2024 T4 ALCLAD r A _ 1 ONE ROW RIVETS AROUND DAMAGED 4s C M5204A D MS20470AD4 RIVETS I ORIGINAL PARTS REPAIR PARTS A A REPAIR PARTS IN CROSS SECTION Figure 18 6 Rib Repair Sheet 2 of 2 18 24 ...
Page 511: ...4 ALCLAD FILLER 2C24 T4 ALCLAD y Si2024 T4 ALCLAD CLEAN OUT DAMAGED AREA 2024 T4 ALCLAD ANGLEA S t SPAR 2o2 3 8 EDGE MARGIN MS20470AD4 RIVETS I ORIGINAL PARTS REPAIR PARTS REPAIR PARTS N CROSS SECTION A A Figure 18 7 Wing Spar Repair Sheet 1 of 4 18 25 ...
Page 512: ...ies to either front or rear spar if the spar is a single channel 1 4 EDGE MARGIN TYP CLEAN OUT DAMAGED AREA DOUBLER WING SPAR 3 4 RIVET SPACING TYPICAL ALL PARTS 1 4 EDGE MARGIN TYP REPAIR PARTS WING SKIN REPAIR PARTS IN CROSS SECTION Figure 18 7 Wing Spar Repair Sheet 2 of 4 18 26 ...
Page 513: ...MODEL 182 T182 SERIES SERVICE MANUAL FILLER 2024 T4 ALCLAD 3 4 RIVET SPACING 1 4 EDGE MARGIN A A MS20470AD4 RIVETS REPAIR PARTS IN CROSS SECTION Figure 18 7 Wing Spar Repair Sheet 3 of 4 18 27 ...
Page 514: ...NUAL FILLER 2024 0 ALCLAD FILLER 2024 0 ALCLAD HEAT TREAT TO 2024 T4 HEAT TREAT TO 2024 T4 FILLER 2024 T4 ALCLAD DAMAGED AREA 1REPAI R PARTS _N REPAIR PARTS IN CRO88 SECTION Figure 18 7 Wing Spar Repair Sheet 4 of 4 18 28 40 A 02 3 L ...
Page 515: ...G EARGIN K l 20 RIVETS EACH SIDE OF K FILLER DAMAGED AREA SPAR WING SKIN X A c C MS20470AD4 ORIGINAL PARTS C e REPAIR PARTS A _ 20 REPAIR PARTS EA CROSS SECTION Figure 18 8 Auxiliary Spar Repair 18 29 0 FILLER 2024 T4 ALCLAD A RIVETS r IREPAIR PARTS A REPAIR PARTS IN CROSS SECTION Figure 18 8 Auxiliary Spar Repair 18 29 ...
Page 516: ...e maintained after repair has been completed use epoxy filler as necessary and sand smooth before painting 5 Vertical size is limited by ability to install doubler clear of front spar 6 Lateral size is limited to seven inches across trimmed out area 7 Number of repairs is limited to one in each bay 1 MAXIMUM RIVET SPACING TYPICAL DOUBLER NEED NOT BE CUT OUT IF ALL 5 16 MINIMUM EDGE RIVETS ARE ACCE...
Page 517: ...J REPAIR DOUBLER TO BUTT B t 1a AGAINST CORRUGATED SKIN rS o e 1 AT TOP AND BOTTOM OF FLAP 1 4 MINIMUM EDGE MARGIN DOUBLER 2024 T3 ALCLAD 020 O 7 s O s O X 0 D FLUSH PATCH SIMILAR S O 7 0TO THIS MAY BE USED IF NEEDED OR_ 2 IGINAL1 8 DIA RIVETS _ ORIGINAL PARTS REPAIR PARTS Figure 18 10 Flap Leading Edge Repair 18 31 ...
Page 518: ...ion leading edge rib from table below RIBS Blind rivets may be substituted for solid rivets in proportionally increased numbers in accordance with the table SPARS Blind rivets may be installed in wing spars only in those locations where blind rivets were used during original manufacture ie fuel bay area of front spars on aircraft with integral fuel bays NUMBER OF FLUSH RIVETS IN DIMPLED SKIN RE QU...
Page 519: ...MODEL 182 T182 SERIES SERVICE MANUAL PATCH USE EXISTING RIVET PATTERN AND RIVET SIZE CUT OUT DAMAGED AREA AILERON REPAIR PATCH IN CROSS SECTION A A Figure 18 12 Corrugated Skin Repair 18 33 ...
Page 520: ...the front spar as practicable 7 Locate new access holes aft of the front spar between the first and second stringers aft of the spar When installing the doubler rotate it so the two straight edges are closest to the stringers 8 Alternate bays with new access holes staggered forward and aft of the front spar are pre ferable 9 A maximum of five new access holes in each wing is permissible if more ar...
Page 521: ...RIVETS EACH SIDE I OF DAMAGED AREA I I FIREWALL ANGLE FILLER 2024 T4 ALCLAD MS20470AD4 RIVETS FIREWALL NOTE _FUSELAGE SKIN See figure 18 4 for firewall A skin repair procedures ORIGINAL PARTS 4 iREPAIR PARTS REPAIR PARTS IN CROSS SECTION Figure 18 14 Firewall Angle Repair 18 35 18 36 blank ...
Page 522: ...E CONFIGURATION AREA OF APPLICATION PAINT ACRYLIC LACQUER Domestic thru NOTE 1 Serial 18265780 LACQUER French NOTE 1 CES1099 IS ZINC RICH PRIMER Both NOTE 6 CCM44A K000486 CES1054 812 VHT ENAMEL Both NOTE 7 PRIMER P60G2 With R7K44 Both NOTE 2 484 684 with 120 789 Reducer Both NOTE 2 THINNER T 8402A Domestic NOTE 4 T 6094A Both NOTE 3 TOLUENE Both NOTE 8 SOLVENT Methyl Ethyl Ketone MEK Both NOTE 5 ...
Page 523: ...ng is acceptable to remove NOTE scratches and repair the surface but care must be exercised to maintain the surface texture or grain Acrylic topcoats can be successfully spotted in 2 Ensure a clean surface by wiping with Naphtha to remove surface contamination 19 4 EXTERIOR PARTS Epoxy or Polyurethane topcoat parts Do not use strong solvents such as Xylol 1 Lightly scuff sand to remove scratches a...
Page 524: ...is standard on serials 18265785 18265807 18265810 thru 18265814 18265816 and 18265818 IMRON MODIFIED URETHANE MATERIAL NO TYPE AREA OF APPLICATION PAINT IMRON ENAMEL Used as corrosion proof topcoat IMRON 192S Activator Catalyst for Imron Enamel PRIMER WASH PRIMER P60G2 Used to prime aircraft for Imron Enamel REDUCER IMRON Y8485S Reducer Used to thin Imron Enamel THINNER Catalyst Reducer R7K44 Used...
Page 525: ...oxic therefore breath ing fumes or allowing contact with skin can cause When an airplane has paint or zinc chromate over serious irritation Material stock should be rotated spray on the exterior stripper may be used to re to allow use of older materials first because its use move the overspray The stripper may be applied ful life is limited All supplies should be stored in by brush and will requir...
Page 526: ...on is standard on serials 18265785 18265807 Imron is standard on serials 18265785 18265807 18265810 thru 18265814 18265816 and 18265818 18265810 thru 18265814 18265816 and 18265818 c Corrosion proofed and standard aircraft will b On standard aircraft mix the required amount of receive Sherwin Williams Primer P60G2 DuPont Imron with Imron 192S Activator in a 3 to 1 ratio by Imron Enamel for over al...
Page 527: ...rer area only b Do not apply White Streak Filler over paint All d If the base coat is not over 72 hours old the paint shall be removed in the repair area and the alu stripe area does not require sanding If sanding is minum surface sanded lightly to increase adhesion necessary because of age or to remove surface de Apply the White Streak to a level slightly above the fects use 400 or 600 sand paper...
Page 528: ...ing BeaconLight 3F14 20 72 LIGHTING Electroluminescent Panel 3F15 20 73 Dome Courtesy Lights 3D16 20 26 Instrument and Oxygen 3F16 20 74 Navigation Lights 3D17 20 27 Instrument and Oxygen 3F17 20 75 Flashing Beacon Light 3D19 20 29 Instrument and Oxygen 3F18 20 76 Electroluminescent Panel 3D20 20 30 Instrument and Oygen 3F19 20 77 Electroluminescent Panel 3D21 20 31 Control Wheel Map Light 3F2020 ...
Page 529: ...0 128 ENGINE CONTROL HEATING VENTILATION AND Starter System 3H8 20 104 DEICING FUEL Cigar Lighter 31920 128A Fuel Pump 3H9 20 105 Heated Pitot Heated Electric Primer T182 3H10 20 106 StallWarning 3111 20129 ENGINE INSTRUMENTS Air Conditioner 3112 20 130 Carburetor Air Temperature 3H11 20 107 AirConditioner 3113 20 131 Hourmeter 3H12 20 108 Prop Anti Ice System 311420132 Hourmeter 3H13 20 109 Winds...
Page 530: ... Tachometer QB Oil Dilution EH Torque Indicator QC Engine Primer EJ Instrument Cluster QD Main Fuel Pumps F Flight Instrument QE Fuel Valves FA Bank and Turn R Radio Navigation and Communication FB Pitot Static Tube Heater and Stall Warning RA Instrument Landing Heater RB Command FC Stall Warning RC Radio Direction Finding FD Speed Control System RD VHF FE Indicator Lights RE Homing G Landing Gear...
Page 531: ...AL NUMBERS SR No AIRCRAFT SERIAL NO SR No AIRCRAFT SERIAL NO SR No AIRCRAFT SERIAL NO SR4081 18254680 SR7639 18262936 SR8861 18265966 SR4642 18256685 SR7469 18263476 SR9087 18266522 SR4905 18257626 SR7677 18263095 SR9113 18267301 SR5852 18259306 SR7692 18263476 SR9187 18266591 SR6030 18260056 SR7912 18264296 SR9193 18266612 SR6222 18259909 SR8085 18263666 SR9195 18266599 SR6292 18260315 SR8142 182...
Page 532: ..._ ____________ 5 t Is 1204 1SRE S TOR ___ _D PC Z l ____ 9 I t1 t 14 iS CIo9 b IFUSE D DA3 ________ I ____ O3P DIODE 869410 _ b DAI s _ 57 i 4 _ 2 Z N 70 DIODE v _PA 3 I z 5_ _ 1 p 1 _ _ IIIS I60 I CON TACTOR D___ PoIZ l 207 t49 1 _____ 10 1570043 3 DIODE SOO P AS ____ PAII Z ISO 51 1 11 5 I1 1 9 C0770Z ZB DIODE AYf D PAIO ________ a 1 fl L e 04IZ OO 1 BAT 6NCD ___ P I ___t 4 i5 49 11 7T 5 L7 S RT...
Page 533: ...OCK g 0 PCL _ I f CLOCK I P Ct I L __1 _YJ I i 5 I IT g F 1 c IAJ 11ro I 0 V1 PA1 1PW COW V n T WIRING DIAGRAM O A _ E BATTERY 4 EXTERNAL 1 C C 2 r POWER SYSTEMS D P _ C 73 07 706 10 SL NON I L I PAE 4 1 C lkRk OU wIZASIBtZ ML Battery External Power Systems Sheet 2 of 2 2 0 f6f 4 ...
Page 534: ...I I I I r t AJMATEIAL LO TMtAINALS SERIA L WIRE TABLE CONTRACT O COMMERCIAL AIRCRAFT DIV D CeSPAna__AIREAZ D 500 C PAWNH NAME DATY C aI IAC AFT CO WICHrTA KANSAS EIROUPM TABLE ______ S _TTL WIRING DIAGRAM I PART oDmcTO DRAWN R _a o 11 75_ IATTER L EXTEPNAL VXNDOOW CODES MM 154t0 NO O CO r XXXxC NA C m PI C NO I C 71379 7 70 cO F CoMCMXXXX CC NA SUPERSEDD by OTHER No SCALE NON PAGE 20 7 ...
Page 535: ...AL G6 S itLOaD vviI AlTEfRIt PER CS l 9 OSERvE POL RIT i f11o O 0 0 DIODC 6mEN ilN1r LLINt ON SW s t TERt IT ALS OR OOlt I N L FI vweKlt TSTEf Is ENefCl Z ED 4 D P3 I i 0 1q T II 71 1 _ lll4 1 ll IIN 7 M a o S UN J a l 1 fi _t_ C lo 0 OtOZRitoULAloB O Fw tC I I I H _______ll P r jn a _ _1_ _ 1 1 5 ITV r C I CITO iTl 5l8l J q l 4 S UL g37t VS 0 A JII_ 3 SUSI3JN 8u ___ a Z Z lP i M J I AIMOO 3001 00...
Page 536: ...TAIL WITHi ADF w45TL 4 l 4 CONTIR CT O E C oize O 5O C PAWNEE NAME DATE CO Pa ARCIAFT CO WICHITA KANTSA DESiN WI TITLC SR C CS r S 7 1 0ET A DWTRlI D R OPT0 1_D IF ALD ERAO SYSTCEM 60AMP AP TS C 713 7 9 0770610 wI SCL o Ne I L IISAGZE 4 7 1 r Lcna AHOAF o W 4ZQ 03 M Alternator System 60 AMP Sheet 2 of 2 YSTEM o AMP 20 9 20 9 ...
Page 537: ... T _ DErAIW 1 F SEPII26036 tON PART A aTI L ILG L I I f AL _ S ll WIRE TABLE i CONTNACT NO COtCIAL AlCrnFrT om oo PAWNlIE NAM oAr Lssa iAIICIA FT CO Wo W rA AS carG V ITr WIRING DIAGRAM AT No I oSCm O I A I CrNATO SYSTEM J EQUIPMENT TABLE cH f a L 60 AM P Cv t XXXXc A OPC N0 C 7379 0770610 I XXX ON CMXXXX C IMA UIK iR 4OO LY OTNI R S TD NO CX_ SCALE NONE 182 PAo 4 7 3 20 10 ...
Page 538: ...st26I q29c t oi P2AO 5 SII_ 5_9 ER_ _ S i _S_ oI I L _______ NM o _ 5e I____ b 1 Z0 5 Oe6 k PO R _ l_________ 1 ______ ___ __4 __ __ 9 M3C60 60L ClQCOUIT KBI ___2_ I 1____ i 61t _ _ S044 5 _ S 3 2O OL tLUCU v lKR P 4 10 _5 W9r_ _ _1_ 2 ___ TJ 82 044 S5 7 _ Sf O SL Ct CLUVAT B9L _A cM ATERIAL LC TWERMILS SERIALS _ 5 O OL Cl RC U T eK _______ _WIRE TABLE S O5 3 0 5SL CU 1e L CONTRACT no COMMERCIAL A...
Page 539: ... P1f a b 14 a s Ct GEF 0 _ O l t STROBISTL Tb A I _ oE TA 1 iICt WARN IND R EFF z 3 1 l i R t2I _ _ t rr r 13 l F l vai A C F CO 5 MVIA KN EF MMMI iNO IC I aSSIGN R wIE WIRIG DT As rFF BusF Bas r salt 2 046 S Split Bus Bsr Sheet 2 of 2 20 12 CO ACT F0 CON AMC T ON ms I R essnaIRIAc n CO wexot A I MI ag V I 1 I W IRING DIAGRAM 1IOJ S I oo I OU i Cooc IOT wO APM C 71379 0770G10 Split Bus Bar Sheet 2...
Page 540: ... CONNECT TO GRO TERMIN D Y L 99 WAS L 0 ON SWITCH _ S 1537 1 10 TERMINAL ON L V 5 O CFCE HOT LEAD S 1347 O10 ON SHIELD S R L L 5 R L _R S R LRF S R L LR TCa C RC CON INUITY BAT EXT_ Lf CC CLN BIT ARCvU N I I BA AT RD RD R MG MAG T i MAGF5 D JAIO 11S_51 160 S15 137 I C T Sc I 0e51l T2 S c _ _ WIRE TA LE C_ iS Lk9 1 I ICO T P 0 o v 0 S 13GO IG CIRCUIT BRT AKER _ T _S 1 W3 l START SOLENOID _ WOO_ 716...
Page 541: ... u O D JA8 1 J lry i stPf8260 26C bc 4 A 3TM T THEU EW 18259908 ua e 1826t83 s 5 o NSTRUMENT LIGHTS __ Gwoo 0 WIRING DIAGRAM 7Z IGNITION SYSTEM Cessna _ i Z C I o 7C 6 05 v 6 7 7 rr C_________________________ 077C610 vi IiBz Ignition System Sheet 2 of 2 20 14 ...
Page 542: ... L 7O b 2i9FV 0 NITION T VV1T S R5 S g t t L T T wIL 5 z7 I N I2 WIRE T RA B D__ _ _ _ _ _ _ N 2A G Ro A M szE O t e 7 _ A T sNB Z __ __o_ z c So 67 0 sL7NIT10 7wllt r coos o CO C l O O eV J 7I EQUIPMENT TABLET TAB z B OO Starter System Sheet 1 of 2 r Ov MT0 E r 7 20 15 A s jDI o o S VITIOIU 3WI n I K C O E 6 c J I C I 1 757 O I O E _ _N2C DEOUIPMENT TABL E b I 5 i i jj TI0 I O SSCh RM sTa CN 15r9...
Page 543: ..._______ _ _ ISTRMt F T LPAI ls JrO f J D JA1 s 3 1 7 _ 1v l I I o 6 U 1 PL AlMT 13 J t T I O A7 tO P ki 5n Lb 7 9 Iolv i net C UII SER 8 OLt K WIRE 1 ETABL o THIRU SFRA i RA59909 INSSTRUMtNT O ETAH1 IT I XT U RVS sr C S AX j _ WIRE TABLE C 6EF Starter System Sheet 2 of 2 20 16 201B8 ...
Page 544: ... ID a W IRC L fcrw aM f bTqIPpMOL Wi c CIMPA _ woi SuOP s RArT rE 5 AMD 5O D PcR C C5 1040 _ u5E M00k eT n1 9 C CR D b R c S O CT al5Yv s r bktKuIm 6 rr E 5 t lS Z A5DDO l Li kMTERAML S AlPM 5S57 7 IW V _ 8 _ CODE 92 14 R i ELDENB8300 If REV AP rTE 4 j I I I vE3OOR C09 70903 E MOW H0f wAC1CE w C 4x I i J1n Q __ 0z Etb IEF z I o T 9 i _ _ Oi I 8 1 1 4 i I Bna 1 12 60 I L_ l r I7 I BLC _R Tr MP ____...
Page 545: ...l rTWINc OO 1S o 5 WAS S 341 1 E E5 4 00 W Y L e85 vaEB4 _ S 16i37 Z CNO SHOP I QLAT _M ER I2EOl6 5R 80372 __ IDI LW r i t r 7 0 E B3 WIRING DIAGRAM r v G 1 V L 3I t LL Krr FUE QUANTtT f s 1l 3 47 i I I I I 1 _ QUIPMENT T I D E20t0 E8 _ _ _ CO D IO GA 6 5 640 9 tHC SIo G 3 _ elo lloJ Xm E sWIRING DIAGRAM ts c cI 35sr UB rI T I 7 FUEL QIJANTTY Yna I 3feO C pq RcuTaRE CR ________ rf IN CiCA70R _ al ...
Page 546: ... LSS T S7 I I1 CLAMP 5 3 I 3 WAk S 31 t M1 v ___________ ________ ttOX SOP s P CE _ t_ A C 7 o Il I i DA 3 LL LZ I D I T I i FuV I r At lALe5 T MF Z 0o EBK t fr ii Z u i 1 F I Plc 4 EU INST __ __ LIGHTS2 C I II I I I tG EA IS c__ i _____ ______ I_ SPEUC E _ WIRE TAA BLE 0 EW 16 ___ ____ lo l C aC Llc E LE_ _R_ _ E Z 20 19 9D 18 _ W IRING DIAGRAM _ ___ _ Fc ____ IJ h ______ a _D_ __ _ CAARIi C LC A...
Page 547: ...v ST L S iO l FU5E C o 4502 0 1 W b uO S qO FdS EOLOER c OR_ Oi SIO OP AL40 c CCr 45cACt oCI 5 105o0 22 WS LZZ S lciO z OtE I I NOJ SO4P PRACTtCE S142 __ _ ef WtLV D PS lAS b O _ 4 20 OIL PRESSURE SWITCH HOURMETER Rev C D DOF5 DF4 D DFI F A 4 D OFI F2 3 I DFD AT5 3 I7 _____ I ia Lfci_______CLOCK T D CEQUIPNT TABLE S WIRG D IAGRAM Rr 3cE wracssm m 0_ 2 0__I __ ____ p u DC OD F4 to s 5 cX O1CMXXXXCU...
Page 548: ... TERMINALS SERIALS ________________________________ _______________WIA TABLE___________________ WIRE TABLE S S f 3Ce0 5 CUX IT B gQ _______ CONTRACT NO COMMERCIAL AIRCRAFT DIV 6 C10 050 TURN C OOR NoTTOR s lOOE0PAWNEE 3 3I0b30 oto5 CO tCTOR Q NAME IDATE Lssra AIRCRAFT CO WICHITA KANSAS 2 AC z CIRCUIT BREArE oOI0 DESICN TITLE C C1003 0 B T BA T Og 7 GROUP c 7 e W IRING DIAGRAM PART NO DESCRITION RA...
Page 549: ...Qo r E K r _ _ _ _ _ COCIT4CT No cMMERCIA L AICRAFT Ov SW PAWN _____ 0A IRRAT O WIHIAIKCRAF TN COS Z 460 C T _ 4l v I g T WIRING DIAGRAM rrg 0 L IAL1AIIY IC W OIV EOQUIPMENT TABLE CTC i DAL T O Q CS O O o IS APPLICASLx SUrcEos ROJ I 1 n IZZ COOE DONT OWo NOO VNO C001ES cER pa4o 4 P A NO CES XXXCSNA SPO EC NOlrrfS Y AO _ C 71379 S IISS ORICMX CESItMA SUPERSrDED 3 OTHER AI STO O 20 22 ...
Page 550: ...bJ t LV SOUeCE 9 t FT D Of l ll R C H ACF T GoJD I DEA HT 7IVDCi vLV lt B J I _ 1PD ___ ____ _ i ___ _ REiW to 2 o 20I 2 s jmr X EL 22 22 0 4 60 I7 Ia 2 0 43 IS 2190 1 M _ 22 0S 4iv _____ BLX B l _ 22 J o 1 0_ r__ 22 8 a I I RY 22 8 _____ tY i _ _ 22 a 5 mr tu _ 22 a T __ __ _ 7 1 S70 5 A CA J ______ A COMMAC MATIRIAL LC TINAL IA A FT C W KNSS2 10 T WI2 22 10 43 JS l90 I O __ 2 z al COJ If DESIGN ...
Page 551: ... 6 _ _ ________ GPN 22 i _ r YSELI I 2 6 ___ 22 6 6 2 8 0 4LK LI I 22 0 S2i90 K ELf T1 22 0 4 34t T __ q 22 222 9 i2 Y 9 SOLCEr4 I 04704C4 IaAE 45 _____GI MATEAL Tt TUNALS SE IALSr 6 C7 44001 0101 A AA 6 oo o O E J WIRE TABLE 5 49 Tra SPO4ot 4 RAN ___ N _________ COITACT MM COMMOCKIAL AIRCRAFT DIV 4 RT 59 TAANS4oS4CEAR II NAl AT A F 0O0 PAWNUE 3 S 21Fp9 l C CTB K 0 AICAT CO WITI KANSAS C S C ECTP ...
Page 552: ..._ __ TWUCOst _ C r oI SL M S q O r _ Ev 7 0 T4 P ImsT PAKIEL LL INWSc S 7EF D OCr 3F S cl 8257 2L w f 7 uc 5 1 1S_ 13 1 t2 Dc0 tF C3 BAC Ut p I _I _tF _ ___ I It DCi _ 1 r____t_ TS e aZ D Die T s L aER IC 6 F 76 Z 6 0 ti Z 3 i D DC I I I _ O S _ 1 _ _ _I I to roz c j E Z OC S __t____ ___ tEe 0 6 e G hl C0S 15tEQUI ME IT WIRE TA BLE fo 0 7a La see B L GBB L20 25 4 OT S S _ __ I e et WIRING i A AM z...
Page 553: ...s S5 t _____ ____________ 10 S ART____ __ 6_I DRLAWZ 1 Ua E Y LIGHTS I 5 1641 9 9 HOUSING_ 5CKT _______ 0LAa f ______ S S B _____ ______ 10 s 6640 9 MOUSING PI ___DLAZ _____ s t OO___________ _ S 1640 6 O JING PIN 7 MS5584 Z LAMPQ 7 of MATTRIAL LO I TtRMINALGS E RIALS C 51S1 ZM T _________ WIRE TABLE _SS t I4u I CONTRACT NO SIZ CEN cO 54CP OU 51 _ _ COMMERIAL AIICRIAT OIV 3 3SI lI L MP NAM OATS a ...
Page 554: ...5 B I I EESM 4WA WIUERETALE 14 S 1641 9 IHOU51 tI SCc T L Dl4 815 __ S IZ_ I S 93 1 AIRAT C4 13 5 1640 9 HLj51NG PIN RF__ C __ iv3g 10 2_ l 5 Z 6 __ TRU5__P 18 3534 I 54 G P HOUC ___ X_ KT W lI S e6l ITIfRU SEP 8 3334 II s 1640 6 OU5NG PIN _ D I1 l 24 5 163 l j49u 5e o iG _ _______ 0 LcZZ0OI 401 L r Iki 7 7 1_ L D LI15 5L I305 s O6MS 15 1493 _ I__ tU SE IB 2C C 9 34002 55 TER E0a D t LD e 4 0 5 16...
Page 555: ...rj leiO sr T v DC Lt L8I J A I L 1 93 D LDI OI N I COQ W 00 40 0 C Q 0 1 ________ SIPE0 T O1TKP WU GR0 P WIRING DIAGRAM D TI 13 ONAWN YOt NAVIGATION LIGHTS ThRu SE r 82 co3S34 5 S C001 O 0F T WIGNO __________1____ ___3_______________________ iSCALN4ONL PAGt i q 4 i 2 GNavtgation Lights Sheet 2 of 2 1 20 28 ...
Page 556: ...OlX c t S lic t 5 LPK jd __ B__O_ LV S _ o L 1 ________ __ S_ Z L 1 6_2_ l8 2O LCt Or Ii IU fi _C_ _Z _s 3S _ _ _ ___u a_ _IBZIZ_ _ 9 K 4 O ez C__ Tl tu et 608S2r_ CLrS 1OO IS 9 140lr 2 AII LICA tJ 1 S6 6 s _ i utw lfc_ _________ _5 5 l 3Ef 1__L_ 2 w BCt iSt2 _ O 5 2LG o l U5IJTCI 1 F1 _ P_ 5_ 1_ 3S esn 5 T AuA SEIA 1 Z 18 CST 2 9 c3Ztoolloo T t ASS I___ _ 8 5 13R Z U sOU1WIIGI CGP ILFS II 7 095 1...
Page 557: ... SlftTR4 29f Mf rUEO3L TEHMNMA IlSTASLt E ON C zLAfT OF TXNOEA PO _ _ 5EA SRT7i t h lr sue TO 04E T OISBAT O RCe STO MAUT e S SBY eV AhO iIXp FOQIIS57 E L MN at KEPT PrRO m aunoe M Ptk4EL tn G 2 e O H Ai iiK 0 5n tb iZin i a3 VAs r fw W PG0 P 1t4092 1 DEIA I P i SE lel4t 2 o is e 1 Ss 1 J11t 9hI Y o L e __ _ __ __ __ L_ _s__ i__ iQ 34005ts 4 MCIt ___ __ __ _iOe BaT W i 1 I 4 1 il L tzeo _ ft U__ _...
Page 558: ... TOTRWI SPECID CONTRACT NO DIV 000 A 0 DO NOT SCALE SPAST D ENICCOES SrE IN S OUPINHESE CSTDO IS AOP CLIS ABC sEL C 1 oup tl_ _ RC J C _ 7 IS APPLICABLE _ 0 DRAWN _WAN BOf 5asP7 PA N E vErDORf CODfE S PS S I 00 CEOCKKL P_ L 5 1000 IS APPLICABLE SUPESDES A CO7 D I IIO I CT SCI ILS PAG PAL T NUMBE Z DESC AI TIO Z 20 31 NO RNQD NEXT AS Y ____________ __LIST OF MATERIAL 00 NOT 5CAHL IiNT DIM NIION AR ...
Page 559: ... ER 1piktozSRS Ao TRvU 5ER SZV02 ol OEZ5 5 0 r THft SUE LSR15 Win ll E Lz aNvL 1 5 X 1 9 2C 4a9S _ z LQ 22 j RID 5 Z L RED O kv io Q I KI Nk C tiO 0D7 R A S T 5XR iLZCOZo4 TiU 5ER IBZ CGZ4 G5 CONTRACT NO PAWNEE IVISION I 1300 I PAWNEE NAME S Sia AI CIAFT C O WICHITA KANSAS K i 6A WIRING DIAGRAM ___S_ i r ELECT1RO LUMINESCCENT cHcK fi PANEL _OJ A ___ _ SIZE COOX IOiNT OWG NO Jo I c 71379 00 SCALE M...
Page 560: ...T 341 T M A II 1_6 IB o0 I IS ISLDER 5 1 L 1 ___ B i8s214o a ON VoR ut6 __ LB29 I 50LDEER LDE SERI 1426 T A IND CNED TErUR CE G AB2626f C24S _ 182162556 tLB28 18 _ 6Z0 s ssER SOLDERI S__ RI___26T iu ID HST L SS 1_35 1 TReiM oj _ _ _ _ ___I 15_26g556 vekjDIOC _lSPH ED LEASID VS RJ 6 l _ __ _ AS t is __5___ _ II oYOICr cTD 5 E l_2C2 4Ct i Oa eL2 Z L L 4 Et ________ 8f eS 0_201 SOL OC 5 bE W t1f Eti8...
Page 561: ...E 5 Ew aDrO 1 5 re r D LB9 D 1b 4 s Wt WR 1 DDL AEC Lighting Instren OxygenOXY C e of 50 2 20 34o t oMkJ p l 71 1 CODE 4E T 0PEFIC 1 I Yt I I I O A I L 14 _ kB C S CIX Lihtn nCONTrmCT N COxCgLe hAeT OV 20 0 341tr woo r__ Hf c IAj Ts ____ oen n IB D v Hw E WWIRING DIAGRAM _ Y m wuixi 1 GHT M6 iRUMEN D tu _ 37O l CCOTL N O tL I ICI W Lighting Instrument Oxygen Sheet 1 f 2 20 34 ...
Page 562: ... 2 C 6 NTADIL C AI0 0 7 0TITLBZE OAw 7sv WIRING DIAGRAM SCALE P S 0 l r Ra S4ZC f H O Z Isr 55c DLAI1 J C T k Lighting Instrument Oxygen Sheet 2 of 2 2035 CONTrACT NO N COMMERCIAL AlCIRCRT D1V NAME DATE L ssfla AICIAFT CO WICH TA A NA H WvISE 7 TITL vx TIt rT Q WIRING DIAGRAM Lighting Instrument Oxygen Sheet 2 of 2 20 35 ...
Page 563: ...zi i LIGHT A lS I ___ ___ _ __ WIRE TABLE 5 t513ZO20 I SOC_ ET ___ CONTT NO _ CoIAL AIRCArcr OIV 4 C 507 0101 COMPASS SS 1 0_0 PAWN 3 IZ331C 4 LIG4T ASST _ NAM OAT1 AIRCRAF CO w IT KrANS Z oo C e7 TeCrtitAI BSLOC o o _ T r TnL _ 3S4 00 3 TCH J ROU WIRING DIAGRAM PAT O o DCRTrONk O WH MlE lC 9 24 73_ POST L I G HT S EQUIPMENT TABLE OPT ON1AL cE Sooo I APPLICAULE SUP S nEfl S4 i sz3 jcooK IoIT owo N...
Page 564: ...uI J5LK 1 BL RED I I IlSL I I T BLK D L BL MD ALQ 0 eC F tT L BLIt I so CD r v B2 WeIt a w eU L 0 C BL 1 I sT X e 9 4 BF BP r I B I Rr SRe FoL 1 D L Ct o Ia D BQO IUGH j __ DRAWN MEWIt K 9 2473 _POST7 L ICIGHT S CH CK YOuv 9tS73 O PTt 73 Po J S z 13 SIZE IODE T DWC NO AP o o Q77Obi 2OTH C 71379 77O I CAL OE _ PAGE A ID B O a I Post Lights Sheet 2 of 2 20 37 ...
Page 565: ... I w AoIbo __MAoEI L P WIRING DIAGRAM PARNo ___ _ _S _E _ VENO 1R 5 14bK IN I PlERm t _I A P CE IAP AE SP E 3_ C _ET D I TO SiEXE CMXX2 M CPROHERK AWL AGT C t170 NO _ CL A WIREEUIP TABLE C 38 CAle uJ i W C 8 C OMMRI II I CRA T DIV VCMO9 n COOZRCmm A1 1Y UOO C PAWN f cI xxxl IszA QP0C NA DCnr AIRICIFT CO WICHlIT KANSAS ZPB 415 l MP Diz 1 1 nns WIRING DIAGRAM PART NO OascKWTae I DRAWNl t J MAP uGc4 ...
Page 566: ... E Z B9 S l TRESS 5 Z sro C 5 1640 9 IOUSINP PIN 1U RB Z ZOO 5 I S ICODE DENT WG 1No EO 5 141 6 U5SNG SCKT ll 5 S 93 1 5 3 07 Z _____ER Tu 79iZ 9 S 1640 6 4 OU51N PIN I Z s_ I____ I4493 S1 1 93 L ______ TU RU EH 7 8 S Z O M TERPI ADAPTI 9 16 2 3S 93 l__________________ C7S Z x 0 SwI T WI C MATRIAL LG TE INALS Sr I G CC2ZOOCiO MP ASS5 WIRE TABLE__ 3 C 200 7IOI POWER ASY _____ CONTRACT NO N COMMERCI...
Page 567: ...5I7 D A _ _ _ _ _ _ _ 5 S I __ 14 14 0 il S Itoit 54_ _ ___ _ _ _ _ _ _ _ m C i _ _ t _2 c_ l 5 _ _ _ _ ii __ __ i 7CC 0 XXU LCI 7M P C PO qT Al 4 l l o A4 O _______ 1 I ____ __ _LI I S CAPOOT A al D WIRING DIAGRAMG 2040 i 7 4 o o c cl 7D D L t aj5l _ _ r_ A_ v U140 I0l CIO OV S JQ _ICH _S0 _ p_ IIut aXXu III W o Cu 71379 07 70 6 10 S XX Or CM1 l 5 O7THI __ l_ _____________ SZ CALE OIQ II82 PAoC I...
Page 568: ...l c 70 1CC o t kero t1 BY REV AD DOI KF DA EF B G __ NOv SlOP PRACTICE 2 4 t D BY REV SER IN D H CZ BLA L _____________________ S 13O0 20L S 5ER OUTr lio I C oc S 9ia mtr co 320 5 p ALTA TH U ISER 18 54680 lT4_S SF 5P 792 D 5 F AMMETEIR n X I I L IGHT o BU5 Q 9 5ER siR 9a ON _ _ l a_42 4 ___ ___ Dc C 5 2C 2 5 912 O N 7 LIOZ5Z 1 JCKT 3tR Cut _ _ WIRE TA BLE G LUTK502 12l NST CUuSTEIR FItI 5 I I I 4...
Page 569: ...G TA ILo 13 THRQ 56R 1Z E60055 5ER 8Z6 TUM IZ6A24 11 F II T6 H ZTIRu W 7 01 tO Sl I TH AI _ U SER 005R 12Z39 7 y 157 Z 4OVG PLfUCA QA I ATEAIP I TalAJ A 5 SER ieZ676006 TtR 6a262465 PITo HI SeR IaeE 466 d ON S S__ _57 1_ _OUSI_ CAP _ _ WIRE TABLE 4 ZoSI 46 S rro ITP T AC ORA AICRAFT CO CV Z T RU s6R l elP I6 I ONSi _ _ o TITLE I cI 1 CU c GR OUP WIRING DIAGRAM PAlRT 0 DESC RIPTION 0 _ j out4 HEATE...
Page 570: ...IL 3 _ 16 21 S I 1C 2 ID CC48 16 16 19 S 1463 2 S 1367 1 GREEN _ Dl CC4l 16 16 S 10S S 136l 2 S 1636 2 VIOLET iCC4 s1C 16 7 19 5 13m 2 S 1373 24 VH _ _ 6 13ORANGE 367 4 1287 24 D CC451 16 1S 3 10 S 135 2 S 1 36 2 VD CC28 16 1 1367 5 136 7 2S _____ D CC9 i 1V 16 16 1__ S 163 2 S 1635 2 VOH CCS4 16 ____10 S 1367 2 4 S 1636 2 VDH CC33 16 6 S 136 367 2 4 S 1387 24 VOH CB __ ___16 l S 1367 2 4 S 1367 2...
Page 571: ...Q 0 L_ ZL Z CO iL I 4zIL o t t u L 4_ b Gus rt 2 C2 1 T j _ Q 0 1 NM Ot AICAFT CO wcHr KAN I O XOW A N 1 C 0770610 ONScTSS T NO AnniL N rr DIV T N I s r s a UC cor3 F offem Tr _ C cmwm I aPAI o4 C A5 I C 71379 0770610 rwso RE F Wing Flap Sheet 2 of 2 20 44 ...
Page 572: ...LLtI1 A 5v I BJ 20 Io J x L __ 10 3421 oo0000 SCtET CDi 20 j _ _ I I j 1 IEu omet lblIZ _ 1 I9t L Z O 1u lCu r _______ I ZO 2 hoFlZ lbF r1 _ _ tIIJRU IbEt I Rb t4 O 19VZ 1 O W5OUCJJO ____ D CDI 20 7 19g0 z O O I CIC GA MATERIAL LG TEI ALS SERIALS 6 S 19 0 1 0 Ol0 I Ca _ _ WIRE TABLE 5I_ CONTRACT NO COMMlERCIAL AFIRCRACT DIV ff I 0 PAWN I f I ea wa I 2 o iUU t tNAME DATE LC A AIlCRAFT CO WICHITA KA...
Page 573: ...20 G 3uM xt 2 r f ow oeL a C T I 7 1 ZED ETAir I D C D 0 EFrF TrtL 5 IStR542 A Z2 05 o CONTRACT O COMRCIA AIRCRAFT IV M r OX1 IL PAW rAE LC T a AIIUFT C WICHITA IIANAS V H ve_ PEBS B C TITLf WIRINC IA AM CPrEC TM L tf s 4 OP61 AL c sI z 2ECODE 1 T WC N sC ul mok1021 C LZ 11C 4 0 6 M St I 20 46 0 oC 4 Q L Y ___ ____ ...
Page 574: ... S 1637 2 TA PCA s 2t 4 RS WAS TAN L6 5 WAS I TAN C P Mef iseolr s eo37 eo Q uMTERIA A SIA D Fc2 S PW 5 tC b o67 65 I i Y b16 iL 0 FE5 lB 5Ta 1 Z A Jcc A 8 S 16 40 6O IOuS PIN NO COEL T DIV CODE So 1 NNI 0 PAWN S D XSGO 5L CdUvX CES S 5E 1 r BOTHER sLE __ 7 4 T c r p GROUP 74 L 7 13CRUWIRING DIAGRAM RSI K OO 1I APPLICABLE SUPERSEDESP0ro I_ t_ SIZE _COE DENT DWG NO VENDOR CODIES PE S 400 P eI I APP...
Page 575: ... I 0 aS EF TO STARTER ObATEVP S00 WIRE CONTALEZ 5 0 P s W TO iS tma E m IaIm Mq dl wa I to I ms 3sob I L I 1 I cx occ i o I owl N ___ l I_ _ ____ o P Isf _ __ _ _ 9 OSISS 6MO STmIP __ e _ o i t 21 4 _0 7 5i 3 _ _ 1 5 157 1 m ID Yl ta C lO _ _ T 20 48 3 O _ 5 i1 bTTEmY cOMTCO k UO WIRING DIAGRAM _o N I rnscil l p GROUND SERVICE FEEPTACLE E KQUIPMEINT TAM EL 2 ____ OPT __ _ 9 an I i _ C 1379t0770 4 ...
Page 576: ...HRU SER SR9087 9 Co4002 o0101 8ArTcR ASSY D DAZ 5 154 9 137 4 i _____ ls____ ___l S 3tO SL CKT BKR DAi _8 5i34iW4 _______________ 7 CZ HS 001 INST CLUSTER DA MATEIAL L T C _M ALS RALS 5 1577 1 STARTR COnTACTO ________WIRE TABLE 5 5 1994 I I 5ynrc CONrIACT PO PAWNEE DIVSBION 0770728 DroDE A s C AIIIC IAFT A 580 o BAr CONTACTOR A AT S s AIRCIA CO A 2 04 2007 BAT GOD TrRAP o EN SWIRI NG3 3 7 I rTrL C...
Page 577: ...L P Tt U9ESO WLAA D _ _ I 14q IH ____b C3 5C 45305 0103 oiol OVERHLT m mhT L D _ __ __I_ 1 SeI _r_ _ it IO5 7O CAlW b 4S B KEC D F6 Im I I 6 01 1t ts aO 4 CIKCUIT 2CEA E L oI I u 5 t S IP II I O I CID Uir f f EEg pq I _ 1 i ______ 5q44 t l HtSEtt aWlCA D DP2 _6 S 5l B 9 _b 14 S 7 t u 8 S Ztl5 LJ4HP A6 I o Pi b S i662 6 3 IN T 4 44 1j 4 l ____ iau_4_ A 4 l 7 5 tI 7 It OUbm a Ao MATERIIAL LG TEAINAL...
Page 578: ...TAIL Q Q CA L______ ______THRU SER sqbc33 LTS LI E0 6 IPAI51 S 1552 8 S 136 4 I l7 4 1 SER SR933 OD D PAl 101 I tO56 0 9 137 3 3 I 3 ISER 5R9S b33 ON A D PAI6 164 _ ______1I Z I 3 13I 2 8I ____SEK 533 ON 1IF_ L A D XPJ 8 a ilZ 5 9 i J L1 U 3 _ 4 ___ THRU SER SgR 33 T4RU R St R O00 pD PA7 I O S lcO 9 I if 3 7 3 73b 3 6 OFT q 4 S 5 5 FVSi I ID PA I IO 5 _S2 0 9 51347 3 34735 i THRU 5ER 5sR 33 8 CM 3...
Page 579: ...S 15428 9 1943 1 1143 31 SOL 97a5 t 014 cSZ94z95 1 O 3 8 PB21 a S 1S6 8 9 a 25 1943 s 19431 S E s78S tON _ 1 F70 5O S 1ts 5 _9 _ R9S 4r3 SER 5R IS THRu S 97859 IU r p an _ sB Ys Tz ERa9 3 37 3 DETAIL I 20 ZO 3 I 0 6 l l __ rTRU SER SR 978 mas 2C 4 G 0 _ 23 SS IR l l 2ZO 20 2_ s2099 S 1 14 I2 05703 5 rfm NAL BOARD 2o E PBIZ 20 20 4 _ l36 1 s 2099J_6 TWJeu 11 11 0 11 S 13b0 5 CiRCV ir 8R f ER Pi31 2...
Page 580: ...4 S ON oC A0G MANRA CA MTEANATOIL LSYSTEM E____UIPMENT TABLWIRE TABLEM CONT ACT Noo PEER DI O NO CA _______________________________ ____00 __C _ N MV ATI CtssEa AHOAFT CO MT K A E DErSON 6 5 AIVHI Vh i TITrrL _c___ gROUP __ WIRING DIAGRAM PART O DESCIpTION DORAWN G STAMI j ZJ ALTE PNATOP SYSTEM EOUIPMENT TABLECHECK Iu 6I EO AMP CCI 1o00 IS APPLICABLE PI O P1OJ7 l IZ CODE IOENT DWG NO VENDOR CODES ...
Page 581: ... COEP S a 4 m ri 1 1 _ DIS2 ISSS GMP STP AP a rioo0a S0oot DIODE y______ _ __ _ ___ 7 5 ST77 i QaWO EVAI na _______ YSo Ga mATMAL 4 TIA _ _ 6 D0IO P S OOE _ WIRE TAB LE 7 i ooo MtM K _ 07i Soo 0 5I4P 2 3 S l S FUibe AI___ CAFT Co C T KANSAS Z s Z445 l wAtTx COC M CTOA ON Datu m i2 f e _ Smz I_ 1is8o 1BATTERN COMXCATO _ a n I _ WIRING DIAGRAM Q PAT NO I o o 2ol r m GOU NO SERVICE _CEPTCLLoEt w EQUI...
Page 582: ...________ s i3WO SL CKT BK 0 DA 6 2 9 5 137 4 0 5 I3j t____________________ 7 C 4 S4S OlOt IN5r CLUSTER A MATtERIAL LC TERMINALS 0JIA _ S Z 445 5TA RTER COrACTro R WIRE TABLE s 5 s 1 4 I S__w__rcH COiNTRACT tN tO PAWNEEC D ISION 4 0770728 _ DIOOE ASSY S10 C PAWNI 5 1580 BAT CONACTOR N AME DAT C WCHTA K Z 042Z007 BAT CGNO5TRAP OESIN IR Cl rq 71 T EITU WINSA K ____O_ B5T Gh SOGROUP j _ T WIRING DIAGR...
Page 583: ...9________ S1 1 I _ ____________ I0 P 35 d l 7RECEPTACLE 1C16Qq46 9 9 O55 3010 6No _ L pt i 22 _ R S 1 5_____ a 1570043 D0oe m P t __ _ r______ _____ cI iOO4 D e maw A MATIrLAL I G aLR 3IMI a ZOuwP OtODE WIRE TABLE T 21 Z 15 A 5 EfQTlU COENTRCT NO A olvWo 5 r TFUSE IOLDEK CIO2 AIIF T CO PAE WS s 4T 5 2435 ST1ER CoT oRI G IS 5 90 TL __ 47S BATnm Cuw_ aCouTO ig J WIRING DIAGRAM S 2475 2 SATTEVV OWITO...
Page 584: ...CESSISLE BAAT pmN0 BO 0 l 0 0 TERMINAL JAI J SAT G 0o s0 INST ST BuA BA8 O JA4 ZO S I 31 S 13 7 lfl 0 JAI gO ________ __ 5 1 7 _7 i ____________ tSSS GA MATRNiAL LG TERMINALU 111Al UJ WIRE TABLE cON m AC NO I iWN DIVI ON S000 IrItPAWNIE LICA b bp MAGNETO NAME DATt eSSnaIRCAFT CO WICHITA KANSAS Z C29Z OI 0 10 5 IOaNITON SWITCH eN SR I TT 5 3 O L CIRCUIT cREu P fr u 4 I 7 7 C WIRING DIAGRAM PAR T NO...
Page 585: ... i 3pL i 7 4 13 O JAS Zt _ B S1 1 _l ___ __ _ A t u iA6L _IA _1in I II S __ __ _WIRE TABLE comuncr Do woms oll Nr 2 C Z 50 005 IGNITION SWITCH omNI R l rTI 5 c5 7cro7 I STttEA CON TAC O4 WIRING DIAGRAM P Ar A e Oru iFFLVTI 1 77 SrA RrER SY5TEM EQUIPMENT TABLE 57 c_________ U N 6 AP P____ g O o no p c ioos AFPLICA ____ S m s 4 n 5 coos mSuir o_ NO I0 S0 1Me C 7379 07704137 WM Mo 0 5o 04 P NE IS I e...
Page 586: ...It 3 5 130 5L CIRCUIT BREAKER AM DT tASa AIICIA CO WICHITA KAN 2 C 92 50 o05 IGNITION Svv TCH DSn 76 TITLNG IAGRAM S Z44o o5 o 2ouw U STA RTOTT GROTUP _ 7PR NO DSCRIPTION DRAWN Uk 2 l f STARI cR SYSTEM EQUIPMENT TABLE s REs CS KIOOO IS APPLICABLE SUPERSDES PROJ I r SIZE CODE IDENT DWG NO VENDOR CODES PrK B OO 0 1104c 4 S APPD 7 7 0 4 CUS XXXX CESSMA SPEC NO 7137704 8XXX OR CMXXXX CUN4A SUPERSEDED ...
Page 587: ... O 8tlo rEroTlt AY _ WIRE TABLE 5 5 30 SL cORcur J S r DI 4 C 952OZOOZ vYSr CLISrEt so a P 1 al a 0 Z S 4JI3 4 WuyC Sw5 SPWKR k3 5t Tr i 5 1 2 iENDING ir CL NOTM LIPI WIRING DIAGRAM PvTr O DT lRf SWIf KNIFnELB IN 3__ J7 CYLINDER HEAID TEMPERATURE EQ 6Uo ICPMENT TAB _____ WE TABL e snilAr CLU TeEr I CoE ODITM OwO No SS orsS 1 I O C 71379 ____________________ EC jA NONE L w9 3 IP a I I 20 60 NmE Oif...
Page 588: ...A MATERIAL XLC nAL 1AL S 5X0 ifo 1 xoi smt __________ __WIRE TABLE 5 S 4 I HOUSINC COT D 4 CONTRACT NO S 4 9 OvSING IVWION 3 5 I 40 9 OUSNN __NAME DATr esna AIICAFT co ECHITA K 2 O 9502 O 20 INST CLUSTER DESI N SPE cER 3 31 r TITU i z072 c 0 io ITR FUEL LEVEL GROUPwW I WIRING DIAGRAM PART C DRAWN H SClIFF LBSEIN 3 7 FUEL QUANTITY INDICATOR EQUIPMENT TABLE STRES 17 CLES OOO 19 AIPPLICAL UPERIEDI PO...
Page 589: ...7 k CLAMPMp 1 1 Cme ANCIAFT CO w iCITAt KA l AS 2 S 1 l 11 Ol ro R SP1 3 1 rLT _ 055 Zr ut u Es r C s e jo Ai k hI R WIRING DIAGRAM _ Pain o I oa IC WnTev rr 3 _ CARBURETOR AIR TEMP EQUIWPMENT TABLE _ s7 T_______pR CASIO I AM P JICA1 I 4 I1 U___ C01 0G P iniT O TIII co r na 077041o 4 EC uIP0lnmE C 71379 07704 1 __________ Q NXXINCMft UPPB T OT11 __________________ UCL NT41 PA 211 _ 0 62ONE sL O 3 ...
Page 590: ...75 I AT aEY CONrTACTUR r C E45 ao2 DIlTAL CLOCK OED N4ZL 2Z ___ IC Co51 1 010 DI GIThALCLOCK AD OF Z___ __ S i ____ ____ S 35OL oCIRCUITEREAKER 2 493 5 37 B w 8 s I z C0651G _ DDF 2 _____ i 3W 1 S i7 __ _____ 7 6f31 1__ HC v siNG _ __ IcO l C A MATERIAL LG TIRINALS SERALS ES 109o02t fuSE HOLDCR WIRE TABLE Sj O A v SE CONt ACOT N PAWNMDIVIS10O 4 AS I Ar f A ONTN CiC 5r 0 oo PAWN9I1 3 Ie 56 t s rl r...
Page 591: ...F OETAIL A 1 ol1 REQD WHEJ4 OPT DIGITAL CLOCK 15 MbTALLEO WH TE REF i DC 7 R caOTmAC no PAWN DiVSON 0D 1 N _ tAMEC LOAIT ACSAFT CO WIcirT KAAS nm a sir W IRi CG DIAG RA fPITOT HE KT ow KIN1 7 1 1 IHOUR METER OPT DETAIL1 3J J lf 7 L 1IZ coo 10CNr owG r RU eR R 9M C 1 71379 07 7 0 1 G OTWM _____ ________ A_____ 05 5EV 2__0__ ____ cALn NJoWJE E C 5 Ro Et I IP a q 20 64 ...
Page 592: ... 19Zl CRIMPING TOOL ONLY 0 0 r II I S IE MQ La r ISn _i IR2 8EDl EEZ 4 C1 45 OO ST CLsr CLULI r Cr E Z oSs 4G 5OU Z Z P L oi SPrEiCER _____ _______ T C2 rIRC uIT 17 GROLAKER 4_ __W IRINGDWIRE TABLEG RAM 5 S 13tO SL __CIC____ ____R _ _________ WATRO C NO NEE OIVIUIOW 4 C S4 O INS C LUSTr _ _ __ _L A FT CO am C I 5 stii33 2 xousi f P ua __ 5V U GROUP WIRING DIAGRAM PART D sIDEnr W DRAWN a C 2 15 7 _...
Page 593: ...__ _ 22_ E __ _ _ t I 1OS I i I X S 4 N bO 2t E 7_FUELUATlYs I ICATOS l 7 lbI3o SL CIfRCUIT EREAKER s____ cFoGA MATERIA L LO T__RIA _ ta b I EO U MOUSINGT WIRE TABLE 8 S IX l 9 HOUSING CONTRACT N0 PAWNEi oI1ISNo STIO t 1 oo r I cSC No meoc 7 701 c no PA a0 4 C2 0S4S OI INSr _Lu__t S X 4 6 40 U L R OOUS WIRING DIAGRAM I C G SOSO FUEL LEIEL XMTR GROUP QUNTIT I N DA o oRAT O o u Z 5 FUEL QUANTITY IND...
Page 594: ... 13bO L cl IRCuiT BREAAER NACME DATE sia CIAFT WICHITA IASA Z iS310 A105L35 CONNECTOR ODEIN SP E ER 31 7 TITLE C 0O3 505S TURN COORDINATu ouPr S WIRING DIAGRAM PART 040 o9SCH pT c ECK ZORLEIVRE 1 r PART NO DSCKROPT T DAWP 4N IFFL IN1 77 7 URN COORDINATOR EQUIPMENT TABLE STRESS L _ CES4OOO I AIPLICAILE SUPERSEDES PIOJ PLUIoRI K i 12 77 51ZE CODE IDENT DWG NO VINDOOR COODES Cr S MlOO 0710110 P 9 s 9...
Page 595: ...2S O s t AV o oc8 I _ e13 D IC K 0 O CJ D PA RtEF 0 _ _ D o c 5 C3 OCTAIL 13 1_ _ 2_ _ _ 61 36 1 Y _7_ _ _ _3 _ T2 Z 5 6OLDER S 167f it 0 W9 3S r _ _z_z 5 I S N s T s 9 3 7 i4SfrooI CLOC ssw A T ATL A I iALS AL 5 j 5 3L 2T MO N r 1 NO ln N I T II 9o ISION 4 0770aZ St _00i T0 aW P A S Z 3 1090 a FUSE HOLDER Mff m speNOcEPI 3 l17 TITALGRAM 3 5 4 gl rTt cOTAtCorr I o I zzl 2 z1si I IS s L I ___ S 0 I...
Page 596: ... rZZ ZD I s l S3SZ sI I 33 ON C 1 e I S 13 7 Fe l 5 SER 6956a DL I tW11 ___________T E 13Q 1 K Tr _ _________ _HR SER SR95 5 2475 1 TT COTACTOR RED t TU SE SR3___ C6645I11 010oo2 DIGIT L CLOCK R _ _ S 10 34003 817 TERMINAL BLOCK c lb ti Cl _ e MS25z231 le19 LIGHT Gr Gc MATR L LOTEtRMI INALS S IALS 17 S O COkT fZ TOR_ _ __ WIRE TABLE 5 5 1O90 ZZ FuSE HODETg ________ CONTRACT NO PAWNEE DIVISION w 1 ...
Page 597: ...9 M515584 LAMP t o TLA 3Z _ S L30 5 370 t 3 5 1 40 4 HOU ING PIN D 0LAI Z t _ 30 0 1 _ I p 7 5 Al WOV5 NC SOCKCET a m AAL LA TEI AL S IDALS 5 16 4 1 9 MOUS NSOCKET _WIRE TABLE S 5 40 9 1M0IN PIN CAXOTRP PAWNER VISION 14 3 NOV ING T oo C PAWNEE i 3 S7 I 3_ OUS PIN _I nDATX AIICRAFT CO wsCrrT ANSAS o Lla 6 o K PAWN EQUIPMENT TABLE IC _ ODURT7F SY LIGH1TS OPFT c4C0OOD 1S APPuCAU I suPaRSEE PROJ mISIE...
Page 598: ...I6 PlN ____ DI 1tt 51 l 1 i 7 5 IfO Cr5CIRCUIT BES E R GA MATERNIAL LG TERMINALS I I SAL s5 tloo i SVITCu WIRE TABLE I_ 5 14S7 t HUOU5ING CONTCACT NO PAWNSEDIVISION 4 6 Ii ST l OUIN4b lO_ o t PAWNEE 3 34 o00Zt EM SLOLK NAME DATE sna AIRCRAFT CO WICHITA KANSAS 2 C 2001 0401 LIUWT AYY ceSImN pfNCER r TITE I CI 2t OOtI 0401 iLAU _ D N AStNEFV 1 t7 T WIRING DIAGRAM ART NO DTSCI T IN U _ u ev N AVIG AT...
Page 599: ...___ 7 L 5 I n B E AXO______N I ll ou ______ ______ c l r Co_ ___________ v CCI l 001 0 oOE IMENT YTABLE t IG H L 1 ____ __ oPT 0 72 C 2 UOLIto D0P l _________ i 4 l q4 6il I on C Csu O OTHQ C 713TO7 O P S SmI c 1t01104AL L1 T AL SA C bIs o Ic L cIe CwT sEe ___________ IWIRE TABLE _5_ _____S O__________ ____ _ CONTACT NO oIIoSIN __ hIC 3 i IAU I6 EgR 3 yl V7 ITL c T4Go1 t PL UER AIb EuPE SQC H WIRI...
Page 600: ...III IReP E I 6A Z2 ____ 5 IBIZ I s5 7O i _ _____ 5ER EC tq5sz oON L i47 2z _______ I70 1 OLER RER5 5 2 ON LK Lb42 1z 22 _ 0 85969 6 5 136 1 8 SER SR9113 C ON _____ ______ _____ _____ f l8 _________ otR t so a i CQ __________ I 2470003 AUDIO CONTROL PNL o 63 Z ____ _ 5 i37 1 O TuRU bt C5bOq 5Z Io0 714 I CONNETO _ _3 SEE C 3 85 _____ q ZI lO I 5Nt1C D i 7 ___ _ 5 3 S X _______ L Iit135 EL PANEL o 2 ...
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Page 602: ...________________ ___________________ so oI EYE BROW co 0 S LJ a n L t14 IL _ D Lbq S s tO A AUMPO BL7ld TLB i SE E SKT 1 S I _ FrT TE M LO C ID L6161 Instu 22 6A JUMPER WI ING DlkG2A 7M VUY 3 7 77 IN6TUMENT OXYGEN c ___ LIGHT6 Pow L l I J Instrument Oxygen Lights Sheet 1 of 2 20 75 ...
Page 603: ... LB r O e el e orTloCA7 I _ N 22 A JUMPSCRSM5 OETAIL DErAILA SKR aR7a TMh SR9437 rNU 5M 3SRS783 mean OAlE CC AIUCRAF CIL WOW a Hlar bCP LR J mM WIRING DIXGRAM Dowigm 3 7 77 INSTRUMENT 4 0 YGEN o SSCMLE T L IGHT 6 POMJ am r r rr sr gp p Low D o Appe Z C 71379 Q77o4t Instrument Oxygen Lights Sheet 2 of 2 20 76 ...
Page 604: ...P L AFT TEOM UOCK 0165 r r 1 1 I I D 1 f1X LI _ a u A E REK L O FOT E IOMeTEL __ LI Z4 tIPL EF Z2 R Bz j 0m I I I BtLU XEF Z 2 _ WC L L_ Z jI N I MMDI C r K R 164 ft i iZ 26 Jt J LPR YdaiE i L FWC5 1 t t Z DESON SPP iER H 3 i T uE GROUP P 6 E WI M DI A LRAM C ORAWN1 1_A IN CMECK L I LI GHT P J I o SIZE C o ca IDEN WG NO I APP I I I 4 1 7 1 3 OTHER 4 7 I I NTU CT I SCALE A ONE R4 I PAE 11 C 20 77 ...
Page 605: ...eCC 5 _A__IX l__ _ l____ _1 0 ___S___ ______ __ _dfi_ _ IOPT A3 S _9GI _Z0 ouStI I2Z 1TB70307 AB LE C5SL l Se TfO 5L CPT SIZ 9 1g4COOZ i S T M a OC s g s 1 1 7 S _ S l 3 3 S 1 v EB 157C o o CS___ Y 0RED 77 11 P85 t 1 _LOE 70 LDNO _ C 3a73 3e OC tlT__ t i T C LO T 17 _m mC71379 Sib on O x 1 1 I I i27o8 CAB S5 ___________________WIRE TABLE_____ I 170at CJ o AA trA 8A W I 23 0 Saf7 5al REO A t __A I ...
Page 606: ... 9 __ 4 I I ClS _ l Tb___ II S 1 48 I HOvSwI __6 _zo__ 2 0 2 z o z _ I S I____14 l_____ 10 Co ZZOOc 0017 LA MP AV Y Y o__ LDIO I L 5__145 1 I5 AlA cl C 2z008 0102 FWE lt UPPLY ___ LD Z L7 s 14 I s l T 54 I S r 371 1 UOUlN4 _____ P LDO tZ I _I SI 1 t 9i __ 5b le 0ob C CA IC1 T HOU1IN ____cM GA MATERIAL LI TERMINALS SERALS 6 5 040 UOUo C N___ ____ WIRE TABLE 1 1a4IA w0u im ______ LICO9TRACT NO PAWNK...
Page 607: ... I GA JUMP It O LCI q 4I 0C4it _ _ TO CIG It LIG1TEL 10 i 3 LOC LT5 T 7 L I _I_ Ob J M S 5 Sb 111041 a IwlSO NT T N PA DIO 4 2t aoC Ct oIt1 bpi_ _I___CPA__ 2 21 0 DLC 1 1 C R WITC 1_ IL I4c l L CICUIT E a ATu La L 7 WIRING DIAGRAM PAT NI RC O 3 7 7 LANDING LIGHTS IOU EQUIP WENT IR TABLE T LE______ I IO I UCICuIT O E PI 1 a W I RIN G DIAGRAM 4 n i9Te a A wm lE 13 7 77 LANDING LIGHT5 EQUIPI ENT TABL...
Page 608: ..._ P I 0 Z3il CIKUT EY 1 5 1C 1 p 5 S rI TEK IN L DL I r_ _ WIRE TABLE I D LBS2 __ _SZ S Ko5 t l I S c I _ CO2ONTRA nt NO _ 4 5 I 3 I 01J51N OOLK E PAWNEE 7 moa i q iOu s C SG FR0 L Z2 i I l e _ S o 5oII OI4 N o ou a 4 B 5 J WISERING DIAGRAM VL1S I s s i P05 3fT LI NRHT S OPT vl oC SL CiR LUIT ScKEAK E 0 L54 5 11 31I 2 0______ _____lISLl E Q MUIPMENTANL _ WIRE TABLE CES IOOO ISAU k _ _ RACTNO PAWNE...
Page 609: ...0 CAI ASty Z4 1 5 1VO 1 ________ q IL R____ LAMP _____ V S i3L 5 ____1_LE a I 1 oo SOCK T to__ 2 Z 2 S s ieq lsb___r ___ ___ _ SS Al fIi 1 Z QHE 0 S5TAT _______ A M TL ILO TSAuL _ UALS i 1 70 1 SPLI C _ _ _ WIRE TABLE 5 2S14 t I 0 WOUSINC__ AW___ L 5 0 C TI C Y NO 90 C Pi A tl v r O 34o00Z SS I t1MIrNAL BLOC NN LtAN DATY SSa AICIAFT CO WICNITA KANSAS I L K 5K E MAP LGlHT COIROQ W EE EQUIPMENT TABL...
Page 610: ...__Y WIRE TABLE i350 5 HO SI __V _ _ CO TICAACWT NO PAN r L ODIVIIION 4 S 2 34S 1 VSlNG r I K PAWNS 3 4 Ns l _I 5uLDC I T NSS Al _ CO C CNAME DATE Na IcF KAN S Z S ES N PE c l 1 _ _3_ T ITL ElA 2 S Wl _ I Ss IT H DESIGN 5 91 13 TITLE i t SL s T z A R R OUP Iu zz e WIRING DIAGRAM DRAwN SPEC R 4 1r3 PART NO DEScRIPTIpoN N SAP LIGHT CJDNTROL WHEEL 1Q 5 _ CHECKVe LA c OPT EQUIPMENT TABLE pTIVI _ CES IO...
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Page 612: ...INO PAWNER DIVII1QN 4 40 _ _ _ __________ _____IN4 Be C PAlUki 6 1 4i weue Ih O AIlCEAFT CO WICHITA KAN A t _ _ d T Itdl l tqIICH 11111 sn 1 tp v rIs Tn I e IOL CIRCUIT EGIaKIuKI 4 ac p WIRING DIAGRAM PAR I 1 HE TED PITO T TUBIE EQUIPMENT T ABLE uEATED 5TALL WA ErNIN sFT I _ W S li4 n t coi l rn No o so GS 1I o l WC _10 I L n 5 m D C 71077041C o S IXX _____ _ ______I__A C______ 7 137 9 iS 2 20 No ...
Page 613: ...__ 1 _____A_ __AL 6 C C _ _ WIRE TABLE_____ 4W C S 4I i U LV E 0 C3 h b_________ 6o2 1 6 E r cooo s i U CT Clto 4 I m COIDC______ IDKL_3_ b_ 2_ _ 5 _ 3c DO Z ODC 0_TGu tO9 ______ Io NO COCIAL AmCRAPT mYv _______ c NAME AIR CR CAFT CO w 06001 PNE Z DEcic S I b l 33 IV IT S 1t 41 __ C 4 7oULz N OC T P N s W T U WI RING DIAGRAM bQ L CPLU I I S MoZl IEEE D Cc 1C 16 NTo OM PTu OIN vAEyP S E 7I WING FLA...
Page 614: ...FS L BS I l0l It J PLCL _____ Cti A S SEI9 3 THIU SER SR 33 2n 13q 3 s5qL 5 2A WILOS i RaD A Z2 8958 Z O5LI O lR T4iufu 5Ct sRAqSL z Z4R E LAMP Riltl 8s gS8 2 0 o0 _____o 25 5 la5a 1I SWITrCH MIKIE K rY K _ I 8s6B 1 0 _ St sCo 0 _ 249 S iZ3 2 z CIRCUIT RtEAER _____ i 8 I WI _ _ 8 0 e 0o _ O 5o TIU St 5Rqq 5sZI L3z 2Z70030 CArLE A5Y _ 22 O1 51 7 1 _ Z L I 9 Z 10 wOUSIb 1_ 22 4 _ s5M il _ _ 21 IS Iq...
Page 615: ...YEL REF I RED DCD 3 ORCD CD o BLUW O CDiR EC REF 6 C OCD S _ _ 6 D CD5 I O _ R lCD Di B tREF _ _r_ _ __ I 4 f D C D I 2 ORN Ay4 1 13 t I PE l a CO TACT NO O PAWNiEE DIVISiON i _N O __ TITLE c r r lltt STRSN _______ IAltD CO r i 6 A JUPER Wi R C l _ 2 CDl on Io AI _71379 c O F I CL NOIE O Electric Elevator Trim OPT Sheet 1 of 2 20 87 ...
Page 616: ...i19 13 CDi co 7 C O DIAW DNETAILAFT CO w 4 R NOJ I 714 u coo E WON R S13 CRU t1 s 5 D C3 o QP r I CC__NTACT _ _ _ _ PAWN__LA DlW5 0hZ ow 0A1AZS i ELECTRIC ELE JA OR TR Il SttWt LEZG Z G OPT OT I c 71379 07 70 1 o Ica s N 4E c 1 903 2 1 Electric Elevator Trim OPT Sheet 2 of 2 20 88 ...
Page 617: ..._ I 19 S ZO SIF32 1 1 JU o C iG I f _____15 l Z_ 35 Z ____ I r16 7 119 4 93 2 a16 16 6 13 1 5 2 ______ l H 5Gr16 16 2 1U 5B 5 15 2 _ _ 10 5 16038 I HOUSING c IC I 2O I 63 Z 1 Z__ 9 5 1638 I HCOLSIG __ _ _ 6 i 16 0 Srf Z 5 2 a C30100LZ ACTUATO A 5Y I DCC 21 16 ___ _ 7 V3 1 D9 SWITCH FA____ I MATERIAL LG TE MINALS gUAL 6 5 2035 1 HOUSING CAP 1 WIRE TABLE 5 5 2035 2 HOUS ING r PLUG _COT A O r voN 4 5...
Page 618: ...C1uAor 0____ _ B 46 I COMuXC TOR ___3 3___ ____________ 232 a C19R 1 MECA AG MATLaAL _ TEp4AIL SpAL 6 S I2i z O 1HOUSING WIRE TABLE 5 IL I O HOJSIN COC P A DIVISO _4 _70030 CAS LE AUy CIi__ C AI CCOAF S CAO 4Z0 0a223 r AlAn SAUY aA IC ______ 23i4 COouoECTOR R _ KLEIN I G 1 7205P4 SwIT c aeD PoiMbi WIRING DIAGRAM r NO _ a R KLLN t 2 ELECTRIC TRIM 0or EQUIPMENT TABLE U COD P MA rG O c NOo 4 S vroo c...
Page 619: ..._ IM UP _ 8I O 04 4i I 1 10 M M ll CONTROL WI4EL AW STS o cois coMTrOaL wu ee CNRC ASNONT CONTRACT NO PAWNEE DIVISION 5 I 600 E oc PAWNEE NAME DATE tSSna AI1C AFT CO WICHITA KANSAS DESIGN KLEIN 2 2 TITLE GROUP A PAINE 3 ou WIR NG DIAGRAM DRAWN Le tIN T 2 T ELECTRIC TRIr OPT CHECK RgE HkcK0 116 STRESS PROJ RSa 5pJ rL j SIZE CODE IDENT DWC NO A PD 1 7NO1379 0770416 OTHECR C 71379 I74 SCALE NoE SR 10...
Page 620: ... o cDa 2 CLUTC rt2 4 W X J B L SLK _ oarr G uD CO fiT t PAWNE E O 1ISIN o KEA A C ltfTt WCITA KOANEA NAlIEAFT __0 _ C PAWNEE_ NA ME CAT Ca SFZCE O WCOE fDENT1 DW G NO oO v C 71379 077041e I S N Sa 4 4 oR G RP I A 5 ftWDI lectrc im OPTR Sheet 2 oTR O 2 20 92 r NO 37 0770414 OTHER C 171379 NCAH EONE SR 10100 I PACE 4 4 i Electric Trim OPT Sheet 2 of 2 20 92 ...
Page 621: ...___ ____ DI6 14 ___________ S i S 13 _______ 7 S _ wl g ____ _ c_ No tlAL __LG T________ ____ _ _ 7 S _ vT E v _ IR IGA MATERIAL LG TERMIALS SERIALS c 3s srTtc WIRE TABLE _ 5 cS _T _________ _________i CONCT NO PAWNEE DIVISION 4 _ _ _C_____ __ _ SST _ r 100 C PAWNXK _ 5 EL R u SS Y H _ NAME DATE ss aAA IICIAFT CO WICHITA K ANSAS 5 o L 7I Jc f r DESIGN PPsr sc s t 3 TITLE _ tr Gr ou c WIRING DIAGRA...
Page 622: ... I c I 07 10e4lo o FI 11 CONTROL WWiELMAi CONTRACT NO PAWNEE OliVION NAM C W r ATA 6 R PAMNS RAWN __ ELECTRIC TR I OFPT CH cam E WMIC f MAN 16KJ 1 CsD logT DOWO NOD 20 92B Te I lR f G 4 4 20 92B T _________ ________________________ w 1 tf 1 P Ha IKCOKllT W O pu r 139 070K OT C i w ________________ ___________ O COI g 0 1 1 4 mrrrgEetrc rm She 1of2 20 92B o cc 5 11 ...
Page 623: ... 5 I I 1 13t __ 1 4 lK F 9 CONTRACT NO PAWNEE DIVISION ___________________ _______ S 5800 I PAWNEC l AME DATE Ces a AIICRAFT CO WICNITA KANSAS DESIGN 1 l k q TITLE G ROup X _ IR NG DIAGRAM DRAWNi _ _ _ _ ELECTRIC TRI M OPT CH ECK g _ q 3 _ STIESI _ PROJ ZIPc l 5ftS SIZE CODE IDENT DWO NO A PD C 71379 077041G OTHER l________________________ ___ SCAE ON RO71 PGC 4 A Electric Trim Sheet 2 of 2 20 92C...
Page 624: ...VIAL LG T SERINALS Al c 3 20 5 2 HOU I N ____ IWIRE TABLE 6 6 K 40 C f w0U te I _ CONTaRACT PAWNEE IV110 4 5 14 4 G HOUoINl 0 ENB 1 PAWNIE 5 S I30 5 CjL CIBLLUI 159IFEL1 ur N T LCSWI AIECRAFT CO WICHTA KANSAS 1C 700 5b HpORls AsSY DMIGN SpNCE 3 71 TITLE OCI IO t R S rT L Wa GROUP 77 WIRING DIAGRAM A RTTNO OCIT DRAWN uACV EY 3 7 77 TL 5kLL WARNING SYSTEM VV EQUIPMENT TABLE __ O 2LF1 hNO O HEKTED CS...
Page 625: ..._ _ i 7 e LGA IMATN L a T1MU LA L WIRE TABLE 5 2135 LAMP COml r aftwN0 r _ a t _AKUA ____ _ I _2 ________ _____ cci MATNE O L IECE CO 1 4I 5 zs 1i _ VACU _UIM _ ______ _ _ _ _ _ _ _ _ _ __ _ _ aC 6OuLrT N o_ M _ tRI e WIRING DIAGRAM PAW No aa m AoHgg LLAr 11 o ll_ VACUuM OUT WI lN6G CHO 2 _ s5 z 45 EQUIPMENT TABLE y a LWE SYsrE 182 IA OaL I i AMUCA5Zo a JAPP Pow _ OMm I como I ow wSaNO s mWOm a CW...
Page 626: ...ACT NHO PAWN1 DIVISION IeoO PAIirE INAE DAT AIRCRAFT CO WICHIT K Z CiS008 OGIOI VACUUM PuMP DESON J e A 4 TrrLE CM se9 5 YT 67 R GROU P OU 9 WIRING DIAGRAM PRT DO sc r eo DRAWN KEN LUOy 1 03 STANDBY VACUUM PUMP EQUIPMENT TABLE MO CES 1000 IS APPLICABLE SUPERSDES PROJ SIZE COO I O DENT DWG NO VENDOR CODES PER S 14OO APD A 70 s S XXXEs c AP 077041G S XXX OR CMXXXX CESSNA ESEDED OTHR79 STD NO NONE 5R...
Page 627: ...G TIWRMINAL I SERIALS A S3 60 1SL c_ coirT REAt ____ WIRE TABLE 5 S 13 0 5 L CC UIT E KE CONTRACT NO PAWNEt DIVISION 4 S I 3Z C _ _C rCuiT BREAER l __ SOO E PAWNE A 27 0oc 4 buS B __TE S N AIR CAFT CO wCl T KANSAS I 22EQUIPE TASEIT ____ STRESSM _ WIRING DIAGRAM AN r NO oESCRlTlON oDRAWN ueglS5 o CIRCUIT BREAKE RS 7 S CHECK IOCLES E 4 o i SEQUIPMENT TABLE S CES 1000 IS APPLICABLE SUPERSEDES PROJ C ...
Page 628: ...RADIO RADIO RADIO PAI I y 15 1 FAN A C PITOT I MS4 EAT I NST C NAV BCN 5TROCE TAXI tDC ELECT FLAP _ OA DAI REF TO AMMETER REC6 PUMP COORO WARN QTY 5 v CONTRACT NO PAWN OIVIONW __ M oAM jCO S AIAHUFT CD WICHITA uKAA OINjAOEN I 6o Tm u5T SOv E ES o a WIRING O AGRA M _e s _ CIRCUIT BREAKERS No C 7i379 0770139 oT ILF C 71379 01 9 _ _ 3NONE 3SR933 rp S4 l I1 20 96 ...
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Page 632: ...493 1______ 8 5 2475 2 CONTACTOR PA2 4 5 15b2 4 q 524 4 S 2447 _ 7 0412007 GND STRAPA co AT IAL LO TPE ML AL 6 S 2443 Z CONTACTOR _ WIRE TABLE 5 5 1994 I SWITCH CONTRACT NO PAI DIVISION 4 2270020 BUS BAR _roo a PAv N 3 Cbbq545 INST CLUSTER NAME DATC C AICAFT CO C IT K A Z C 7707 2 8 DIO DE ASSf Y _DoN TJADEN Io TAINL CCI400Z 0101 IBATTER A55Y I s JAour E B L WIRING DIAGRAM PANT NO ocDESCRIPTION DR...
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Page 634: ...BAR PA 6 t8 _ S ______ ______________ q 5 122 2 CIRCUIT BR AEVR PA 8 5 S 8 q _ 3 3 7 1 95 uL __ e 15 30 ao ClRCuliT BREAKER 8 15 q_ ib 1 Mg 4 S 97l srn 7 i 1360 i5L CIRCuT BREAKER R GA MATtERIAL LG TtEMINALS _SE I t A L s s 3 0 iL lRcu BRE E R WIRE TABLE 5 5 13 0 5L CIRCUITONACT NORAR COoACT NCo 10 4 S2 2 O C RCu T BREAKER o 3 S 23 CIRCUIT BREAKER NAME DATC LCSSna AICT CO wC ANAS a 27OO 00 BuS BPR...
Page 635: ... RADIO i 3 4 1S D PA a I o L _ _ 5A4 T I T S I S r t 5 I PAN FAN VIC At A E ALT ALT FUEL URN STALL FUEL IN5T CAS NAV ECN STROBE TAX I PSI 4tP E PA SIw 10 PW S _ PAWY 5 __ REC A O P D I D _ _ AL r A___ __ 0 rCesna AlltlAFT CO WCHITA KANSAS OGt oup LLIN i WIRINSG DCDIAGCRA M OtAW L I o I p _ CICUIT BREAERS 7F4 P O WR_ A7 _ AOPUIS WiM fPAr A_4P __N _ C 713 7 9 1 7770 3 c NOC soo cs t P I 20 10o ...
Page 636: ...Z T c g FIREWALL AZ NCI INSTRUMErNT PANEL 11 i G 5 R L Ill BAT GNO o JA3 S 21 J1 JA I JAI zO 5I 137 C5 171 I 01I i CBIL B A I MATERIAL LO TRM4ALS R AL irlREWL ENGWIRE TABLE _N T COWTACT NO PAWNI DIVISION SO I PAWNl __ OATC s FNAME CessnaicAFT CO WICAITA co f K 2 D0_N 2031 IMAGNETo OESGN TJADEN eo TITLE CZ9250I 0oI05O IGNITION SWITC rOUP L __ T le60 WIRING DIAGRAM Q PC RT NDR DX Ci TOD OAWN DBIMUEL...
Page 637: ... 4GO s8 rs i KA 4 I C Z9Z5o 01O01S o rlON s wrc m oasm 1 TLI SEN i L Tn St I 5 43 A Srra co rAcroe I GRouPbamM a WIRING DIAGRAMI I NO o mo I OAWN aS BURRIS L S TARTER SY STEM 19 EQUIPMENT TABLg CHUCK m oP PIC CA w Il PaJ mPi l 1 4 zieoln a0 IcoeOCMr owm NO Sl e c m A mMe 0O 7a o I NO 0770139 94OM 00 upv my a0 7137 KAXXSM D NHI3 LI 1 WHMOM I Molt I I 20 104 ...
Page 638: ... ____ _ o PAWNEE 5 si 37 I HOUSING _ NAMEr DCATEL AC WICHITA AN 2 S 21k0 I SwT C H oESnJ TJADL hE k TITL I S 1560 5L CIRCuJIT BREAKER _ COUr liaFs 4 _ WIRING DIAGRAM PART NO DESoCRPTION ORAW N IS BURRIS 3 o FUEL PUMP EQUIPMENT TABLE CES DO00 IS ArrLICASLE SUPERSEDES PROJ C F 14 Zf BC SIZE CODZ IDENT DWG NO VENDOR CODOS PE S O4 9 r 070 39 W CES XXXX CXSSNA OPEC NO O R C 71379 0 7 I 3 9 S XXX 01 CMX...
Page 639: ... 1 _OU__NG WIRE TABLE rC33 _ _OuS __ _ 1_ 7 _AOUSA8 mnO T _TABLE______ f5 ff _ _ _A s E 5 5s LZ ADAPTE R A R E aLEAC C WCHT I S _3_0 _L __ClrCUiTEAC_ GOUl _M _ i WIRING DIAGRAM PA W OA mv R LgEIN ELECTRIC PRIEtR rTI8 EQUIPMENT TABLE CK F _ _ _ _ _ m o I rw inces ceeAPPLICLE llu llllsu P S com NOR E owS NO SmC O No m _____my ___ __APO ____IC j71379 07 013 2 a J 9 S t TC maO R 7_7 a MO M OTR q C sim...
Page 640: ...EAKER CONTRACT NO PAWNE DIVISION 4 rj 53iCAI wS475 PLUGS W 00 Io PAWNEE 3 Ce 9 02 OZ I tNST CLV rER AI NAMElc A aN Am tO CHITA K S 311 4 INODCATOR D OlGN J TIDEN N Io TITL i OSs50t zo NDNC J ulr R AI GROUP L _ WIRING DIAGRAM PANfT MO O CT T09 f OAAWN s BURR S e CARBURETOR AIR TEMP PA rrT 0 rCC I oE LEcN l T EQUIPMENT TABLE STRESS CES IOO IS APPLICASLI S UIaSOL DS IPOJ C L D_ II CODL ID NT DWC NO M...
Page 641: ...I _ 22i3b _ 75 1637 2 MOuV14 ___ ___ GA _ ATI AIL IaG TI A 8 s _ _ _ _ O Cb640S8 010 CLOCK ASSSY_ WIRE TABLE 5 5 2475 1 SATrEII CONTACTOR _ M__ cT NO 4 5 1090 _Z FUSEII4LOER _____ e 3 5 l6oq l FUSf I M Z_ C C ACIAF C mc 1 i 6A 2 S 17311 I OILPSSUIIM SwirTcH a T JAEN TInl C6a4503 0101 HoutNIT1 GR a WI WIRING DIAGRAM PA T I OmNo N AWN EMU EK HOURMETER EQUPMENT TABLE I g OPT icoo 4S PM 11c E mrio Fa ...
Page 642: ...IGITAL CLOCK I ISirALLED In 0 COVACT PO PAWNes DIVION owtucr to I ry wrrr Osa PANS ANAME AI SSl ICRFT CO wCAnTA KANAS GROUP W T IRIMG DIARAM op VS u_ s 30_ HOURMETER OPT S m ______c cN POJF SLL 2 GC IZE COOS OSNT DOW 1N Acco LIN 0770139 OTHER C 71379 3OCK NJONF o A3 1 o T 8 Z 20 109 ...
Page 643: ..._ __OUSIN PLUG o c 1 J _ OJ c Z O COD2 lO no I __ J4 _ _ _ _ IDIN _ _ _ CI IUIT BY I NQ _____WIRE TABLE 5 S l3QO SL CIP CUI PRCAKCER _ C NO S 13aa I INDo MG U IT YNAM ODATE AlCA IAF CO wCNITA KANIAS S lib 2 4 OtS NG 6 PL U Jr T3 N o x TIT AA B I 3 Z 34 i s P Oms u r o a A WQP 4 I WIRING DIAGRAM PA T N ame e e oaunI r4 o CYLINDER HEAD TEMP EQUIPMENT TABIL g SLE s OIL TEMPERATURE CIloo Il S lma PROJ...
Page 644: ... INST CLUSTERAP_ _ o 2 0 111 ____ U 1 t T_ AIRCRAFT C wInI A ICAN A Sci 4o Z HOUSING L ___ o G _____ DESI N WIRING DIAGRAM PAR TrNO DC RpTION D AWN BURR S 4 1 0 FUEL QUANTITY INDICATORS EQUIPMENT TABLE SRE m CES OOO 1S APpLICABLE SUPERSEDES POJ Cr l SI COD IDNT DWGC NO VENDOR CODES C 5 1 0 A2 S7 n 1 O C7S XXX CE CXN PEC NO R C 71379 L 7 OLI O 4 S XIS 5 OR 0 CNTXXXX CENA SUPERISDED BY OT ER _ElF I ...
Page 645: ... apa Dvso I CA0i0O3 oSOe r RN COOmR01oATuIR CI SOL WIRING DIAGRAM 1PART Nw orvzc o 1 5 URRI 4 eOA TURN COORDINATOR STD 4c bOO 1 0 _t c IXO T _ _ STlRa ESS c _ _ 1_ _ _ _ _ _ _ _ n C N cwm 0 1 APyuXASL suSensu PmOJ w wcw II 2g z CO I owE NO O c IuO I a oA _____ I C 7L 1379 SMX O _ NOIIE 1C1 3 PAGMI g 9 1 20 112 ...
Page 646: ...P1 1ALS b 5 1 37I1 I HOUISLNG WIRE TABLE 5 S IG 7 HOUSING CONTRACT NO PAWNERDIVISION 4 077076 DIODE AISS 1S0 I PA1NKR 5 2475 1 BATTERr CONTLrCT _ NAcM DAT S AIItA CRAFT CO WICHITA K ANS 2 5 OiO9 ZZ FuSE HCOIE R ousN J TIAOE TITLU S IO9O FUSE RHOOaERUO T3A0 WIRING DIAGRAM ART NO DCIPTI D RAW S BURRIS 34 0 CLOCK EQUIPMENT TABLE ST RE CES WOoI APPLICAL C IUVCPRLDo PIOJ CfI LL 4j SIZ Icoo IODET owt NO...
Page 647: ... 5 MAT ryaL i oml T atu I 119 01 1 PO 1 O L a IJ AMOUS oS SSS a WIRING DIAGRAM AT NO N SuR 4 8 bxrolTAML CLOCK OPT __ EQUIPMENT TABLE I c804000 1 PLiCAME N m pmj i Qawo g 21i Om CA looff D no 1 S t SSq No t42s 1 1 13 F 0 770139 L 11 cS cco oa I __ __ o CT Ir C 71379 _ _ _ _ _ Z __a 4 lr __ _ m D 1 C 4L NOML 0 R121 JA39 20 114 ...
Page 648: ...KET CI dA MATJLERIAL LGa ERSCNALIT T SERA I 5 X 41 9 HOUSIN6 SOCKET C I WIRE TABLE 5 5 640 9 7OVs INC_ PIN S 2D I 50 SI0 IVON PA ___ _____________________________________4 L 5 if 20 1 3I Z1 37 i NOISINC NAME DATE AIRCRAFTCH_ CO WICHITA IANSAS 5 18 31 1 CTCN TJADEN TITLE WIRING DIAGRAM 5 1340 CL IRCulr BaEAKE R op p PAR T DESICRIPTION A OEE RMUELLER s80 P DNALOAE LIGMTG STD 4 EOUIPMENRE TABLE R Y O...
Page 649: ... 1 tI __________ Ul I WI i______________ 7 S 1 40 L cIu a L A MjAtN AL I6a T m A qAl I e s M t HIOUING ________ w ttm a o I 4 8 lflJ0 t OUNI6 C AIEC 3 PAUIN_ 3 OC I _ M 1 AT 1 AI C0wiAT CO _IT KNmm cttoo o MCb __ E _ 1 o GR Tfl WIRING DIAGRAM A OIEi NIER AVIGATION LIGHTS EQUIPMENT TABLE C c aft s APPJcaML U Ic eC L4 jz a GM coow OmT us m coINAP M 44 AM NO _ili _ a sw I C 71379 0770139 0 WA 8 ol SR...
Page 650: ...o j I3 O 1OL CItLWUIT SeEL _r _ WIRE TABLE 5 S tli O I SWIT_ CWThACr NO AC P IN _ S I 5 7t UOUSING6 __ _ C rPAUE i oIlw AN AI C4AF CO ICHUA KA BAS t o SIh e 1 wouslNb SN TJADCN _ T CS 4O 001ot FLA 5E ASY GYOUa WIRING DIAGRAM _ PAR TNOD C OBEmERWE4 DA W FLASHING BEACON EQUIPMENT TABLE CHI LE5 LIGHT OPT CE 000 19 laLICA lSUPERSEDES J C z i o CODE DENT No 1X Co m NA Y NO OTHE L C 71379 0 oTD NO WOKE ...
Page 651: ...______ ____ _ DI Lb S 1 1 9 1 0I _ _ _ _ S_ _ e O N 5 L z B 7 ONL Z car i mI 1 _ _l____1 _ ___S IL 6 O 28fH M 5E t _ __ _ _ p 2470003 k J 10 COMMOL PNL WIRE TABLE 0 9 I O __ WtU SiA 5gqll1 5 3T tI HIHtMN L p CNlACT sO _6 2470003 U060 Ch0ziL P4L _ _ WIR TA 5 s 40tO 9 OKFI I P o i _W Etg BOMsZ_ _N 4 C_500_ OWOi F_ NE_ _ _ SL Y _ IB _ _ C a _ _ S IlsO 4 cIct ______ iLB2EI I ia I TAIRCRAFT CO WIC ETA ...
Page 652: ...L61b S LDEBR HBT7 __ I slb A t POT ks _ LelS __ 15 I 1 5I 6 4O 0 OUIN 115114 ____ LlI4 e ______ _ S 0___ 14 S 141 C OUsIu5 ____ RED LB3 _ Z2 _ IX3B I SCLCER It1 M525231 lB29 LAsPZ _ 22 2 __ ZLDE _S 31 ____________ 1T wlSsb54 l4 M IAULIRE LAMP B_ iLKLBII 2Z 0 SOLDER 5 l I _ II 051350Jt SOCKE T BK ____ O 2 _ R Ef 1 t Et R 5 1 10 520W l MOULiNo _ _ 2 222 SOLDER L _ A s 2DX 2 lmOUIH ____ tLK LB8 Z2 22...
Page 653: ...P A LI T T0 IMMIN6 AkSSY L65 nF O p 19 0 SE 5sT 5 t B71 13 0 IOXY6EN CONJSOLE L116 PEoeT AL L115 __ LBa 6 _ I La icTww 1 Q1 Z r D r y _I r s AScw wINT NT LIH S w C i oN W I AR l CR PAw nM b P t EN M Irns r Dom EN m T C _ UEBUEuER 3 8o0 INSTRUMENT LIGS5 BLK I A 7 C 7 1379 0770139 rTH IU S K l5Rc i II __________ _________ _________ __ _ ____ ___i i C O E B 3 II S I 20 120 ...
Page 654: ...Vt LvGRTS TO CAE i 1T0 I2 E tl 4 CO ACT P r O PAWNErE DVI8 hl 68M a PAW tI OlV _ _ A lD TL s AIICIlAFT CO W r AS o0t N TJADEN bl f T TIu a2 E 4h S bBo WIRING OIAGRAM O WNos 3BmRmeLR 43o INSTRU MENIT UlG TS PmJ L o P D O J J fict _ tl c l2X COO IlOimT m oP Lam c 713379 0770139 3C NO IE ME SR4633 PA66 r20 121 20 121 ...
Page 655: ...Oc 9 S7S3tT ca Sa ____ __ _ iTo7507 I I_ 22 0 _ ai3 2 sW 4 7 Is21 0 00oo co taaT0m Oc 6 ATINAL_ L IT AIIS I IIA I 17004 Z C LZ ASY __ _ WIRE TABLE 3473 5000 SOCKET ____ o_ r _ D 2 l2 004a I o m e L I NIS IBE PAW1II 4 12roxo CO ASk v _ _S 3 MaS9eAbiStiA RZHtObT T _ _ _AM c am ACiAFT CA wCHITA KAAS 2 24RtB L A fP O TJADEN e _ Tm I 45s7 oo SOOcT __ e1w k l tr WIRING DIAGRAM _ Pr oM a SPERt1JEILER 83 ...
Page 656: ... LUOUSINb _____ Lo6 j ____ _H___ ls I r a _eoroo toa l 1 fI UINb ZHOUIN _ OGA MATERIAL LG T MINALS I L tllo q A0uS o _______I WIRE TABLE _5 S 1 API A 1 10USIp 6O________ COSNTACT I VEDO4 CODS PERl 40 P A INE OUS N ________________ C I 0 F39 DIVISION 4 5 t40 S0U IWCI o O PAWIN EE C a 4lS XXXX C UNAL t IC SSn ICIA T CO P NCM KN S2 zD I IILCI DIGN T3L O T I ST TLC i123a 1 LcuJilT MeeEK GRoup Ar J 20 ...
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Page 658: ... l 5 s493 I tI _____ _________e LC I 8 ___ ___I l 1 I 5 4 S 3 1 GA0 MATRIlAL LC TEMtALU SERALS 6 5 1360 10L CIRCUnIT BREAKE WIRE TABLE 5 4591 LIGH T C Ow NO P at II DllVISION 4 1270082 DIODE ACSSY 0 M C I PAA 3 5 203 TERM ADAPTER AME AI t T 2 5 21iO I ITCH D SgN TJADEN 6e TITLE I 51360b 5L CI CLIT BREAER owGROUP A WIRING DIAGRAM PART NO o c t DRAWN 0BEUWELER 1 3 o LANDING LIGHT EQUIPMENT TABLE CH ...
Page 659: ...II IW _ F0LL _ tmZZN z 2Z 2 3 5 ia 5 1 f3 Z 5 _________2 I 1 i o PL IC C CA M WTIAL L T IS AL SIALS __5 _ _ __ _o_ou_ _ _ WIRE TABLE 4 qL 0 4OUbiNCa t a PAWN DIVISION _ _ __q_ _t__ O HON _ PAW S _3 OOZ SS TERMINAL BLOLr T C AICIAFT CA c 2t 0Tc DI SWGTCl SMM 35059 Tr I 5 iO 5iL CIRCuT BREAKR aouP M WIRING DIAGRAM r G A S TAMM r MAP LIGHT CONTROL WHEEL EQUIPMENT TABLE L OPTION CK5 0o0 1r APLIC ll B ...
Page 660: ...WNE C7 Iq S 6ET E AM TGe AIlCRAFT co CHITA KANSAS 2 5 2I60 3 SWITCH DC N_ _ _Sl KLI TITLE _ DAr 5 i360 5L CRCUrT BRK OUP A WIRING DIAGRAM PAT MO DESCRIPTION DRAWN g KL Nt ICE DETECTOR EQUIPMENT TABLE ST swsSS LIGHT OPT Tl8 CES 1000 IS APLICA LE 5UPERSEDES J SIZE CODE IDCNT w NO r o 1 9W s n coo OENTwc VENDOR CODES PIER S IdOO A737O NO CtIS XXXeCISSNA SPIC NO 1D S7 0 70 139 S XXX OR CMXXXX CESSNA S...
Page 661: ...i 10 41S 001 SOCKCTr 2z _m _ a I3 02 IKmE I N I I PAma a s 16c L Ifcrr aI _ ___ _ WIRING DIAG RAM C t I _ _t mcOSTr_ GA I ATWL Law s T S z1lfe0 BL I TCH ____ S R I WIRING DIAGRAM PA WV __________ _ ______ S MA P LIGIHT CONTROL W1HeEL EQUIPMENT TABLE OPT cr am Of AUP CA Lf UJ pB I o IMS sri 3a rZ COoa Ein ow NO vome coea Pn 6 60 pf 11 10 NO 0 j2inhA U oC_ 3 713 0770 3 __ 9U a D0R X r ac OTHRR C ao ...
Page 662: ...0502 aR EIGHTO____ ER AY NAME DA C S a AIRICIAFT CO T C PK AN SAS 5 75_ 5 C S DE IGN TJ CIN I O TITLE 05 305A tU M ERA S5 _R 1_ _ _ Z 15 u 54 SEG ESROUP ISC D G E 6 TITLE WIRING DIAGRAM PARTo I oDscIPTN DRAWN OeERPUELLE 4 o CIGR L IG H T E R EQUIPMENT TABLE CSTRCK eiSAL CrS 1OO IS APPLICASLE SUPIRSEDES POJ C Q 4 t J 8 SIZE CODE IDENT DWC NO VENDOR COD S P 5 1 APO 771NO CS XXXX CSNA SPC NO C 71379 ...
Page 663: ... T 4 i EQUIPMENT TABLE STS EJED TAIL WA NING IOPT CES SOOC IS APPLICABSLE SUPERSEDES PROJ r AL Z SIZE CODE DENT DW No jI S Ol p WOUS I I I I I I VENDOR CODES cEr S 40 APPOr o 5 _ _ _u __ 4 1HETED PITOT TD E E C XXXSIIXOCexxSNZCEA l PE 6 C 71379 7 1 0139 S XXX On C i XXENA zO CONTACT SE IOED V S OTON a4m o 5 I H 4 IXcr 1940 U51 I So HOC I a __r___________SC O PAGE 15 20 129 20 129 ...
Page 664: ...1416 o 14 I _ L I L C4iCUI F ____ I___ __l_ _ __ _1 I SOSO COMPR e aldO P i S i 6 It N4 4_ S 3I3 1 4ueINx it ____ 5 a 1010 u WE MIOl S 1 37 1 HOUSING dHE _______ __a_ TI___olo_ 9 S 203S 2 tU4 N I I SMOS HEJ i OC a S i035 15 CKifua l Rsg gi T i3C CT JNAJt OOU4G FAN A_ L___ IaI _ m _ _ 1 s SWITCIHU51 I o a O 0 oz i N P U N oAICIAIr 1 4 S iAOIT _ IAN1T 9 S 03S 24 14OIN0 _ CAP _ 6 TA0_ _____ t o r l i...
Page 665: ...f rt EF cD 3 HE4 HE A i ICD HE o I E9 0 RN REF 1 EZ N RE 5uRE 4 L z 1 OJ _ GB OC I C 713 79 Gt o 0 O _ __ SCAIR C N D TIONEP I 3 REF CE AIL AlK 2 r seiJ SE CbL oao cokWh1cT Poo PAWNEE OIVISION NAME DATE o n 1 i AClCkFT CO wCcerA cKANSAS am I3 OTtFAQCN TITL JRING DiNGRAM I o r F N rC F 3 4 C4 O IDI NT I NB MOAWN S sUpR 43 LAIR CONDITIONER OPT ca4cz opeLea 4 4 6V Un i __ES__ _ o _OTR ILWP c 71379 07...
Page 666: ... I NAM OATS 5 laAIRRF CO0 A KASAS ItL _________ __S 3 S f 2 2 S I irC H D7 o________ KE IW ______________ 2 S 0 CKr SKR __ low 0 C I5 _ WIRING D IAG RAM Sr r0 R KLFM _ fl OlL D PI _G F _ANTI ICE SYSTEM_ E207QUIPMICNT ____LEE L _GP T T2TA IE18 I TIMER _ _ COTw IS N v PW BNOo 2 20 SN TCNu WIRING DIAGRAM 1 w WHSmcoo PM PG4t0 M 1 Z OO o w 39o CM UoESSNA AP NO rT C 71379 077 039 2T032O ta _____ NN I100...
Page 667: ... CCNNL frL I frNA ME OAT CSna AICAFT CO c T 2 S Zi60 I SWITCH o___n i 2 TITL IRING _ 1360 5L CIRCUIT BREAKER GRoUP WIRING DIAGRAM PAR TO DoCT O o i 1 r WINDSHIELD ANTI ICE EQUIPMENT TABLE c l SS 5YSTEM OTP 7 CE 000O IS APPLICABLESIM J SSUPERE S 7DE z ooZ IoENT owc NO VNDO0 COO P SmP 4 7700 r39 X XXI OCESSA O O O C 71379 077013J crXXX 0o cMxxxx CC 4A sufCDMO mY OcHtN1 srt no Sc AL hNNE S OIOC I ct ...
Page 668: ..._ II MS31lOASO45S P _UG 14 14 0 _ S3CLCEfi _ _ _ _______ __ _ 14 14a 5 16320LER _ C 4 o01 SLIP RING ASSY A _ _ C 4 C 171_ eRUS BLCCK ASSY l______ 14_ _ 37 6 5 4 93 2 7 Cb1650OO fE TIMER WINE e GA I ATOmiL L tPowA U I S ERL 6 22 37C 2 SHUNT __ _ WIRE TABLE 5_ S 2C35 Z HOUSINCG__P I P ____PW___ Cs O S 2C35 1 HOUSING a I fA w _ 3 C66250 3 AuMETER _ O to AIRCAT C WH A 2 5 2160 1 SWITCH o____R LEM 1 i ...
Page 669: ...Z 14 I 0l I CE WOUSIN _____ 1I I I us 1 W S sl IJOU16VINb I 3I ____ ________ 3 I I 1 1 5 2 CIUTICH __ i_ o__iZ 2 o _ iW 5 u _____ _____N _ _ 1C C5 Il 210 OULtIN I 1 O L L l s4l 12 2 34 p I 0 I 1 TI H o C E TOC ___H ___ D22 2 5I 3 IS 1 I_________ S 1270o44 CALE b4 ____ NTA NO I 22N D _5 D I T 1 3473 500 CLE0 l I Ct Zootr A I Iz 7o84 t NAMEc rov C x C z o z AIICRAF CO C KNSAS 2 l 7084n CANK6L rOK __...
Page 670: ...N o S 70 5PLIC FL _ _ _o mGA MATRILAL Ia_ TIuIZL CS OSrALS 15 585RA9lI 5Z A R E0oTAET _____ AWIRE TABLE 14 11iZ Z CIC CUlT lBEAKLKER CONrAC NO PAWN I OIVISION ___________LNs 150to Z 1iu i9_0 It PAWNER 23 A Z1700310 CnAFLE At SS N OATY C l AllCRAFT CO W AC T KANSAS Z L Eqb Z O 1IOUSlIN C OagmN G sCAIF 3r11011 TTlll z1 s 5qz l O I OUSNCA a 51N G WIRING DIAGRAM PAT NO O 6 S TAMM snol iELECTRIC ELEVAT...
Page 671: ..._I 10 S 038 a2 HOUSING r 16 g ___I__ I TA 9 1 038 1 ouiiG I HOl a ___ _ 8 IC3010oz ACrJA ACCT ASS _____ cc 116 7 5 lo4 2 SWITCH NuAMM _S a L l5 u G 52035 1 HOUSING CeAP ______ ____ WIRE TABLE 5 5 2035 2 HOUSING PLUG 6N___c___ M NO w Mvm 4 5 IQ40 9 HOUSING PIN Do E C A r CATi 1 9 ous iN6 5 i g s L co HO S GC KAN 5 1906 i SWITCH 3____ Ss T3N TTxIG I 5 1360 IOL CIRCUIT BREAKEAR____ 2 GROUP WIRING DIA...
Page 672: ...__ _______HUSNGCOTRCTN PAWNE9DOVUION s as 3 _ _____I CSL AC _ ___ so C 444_0 325_ TRir_ AfcTrArTO ______ Vt__ W______ _KANSA 8 ZZ7005 PALAY ASSY NAM o ICA C O MCATA KANSA S 2349 a coNNECTOR oUS R LE WIRING DIAGRAM 2 I 7205P4 SwITCQ4 ocwn ptl 3 WIRING D IAGRAM N _ r OAwN R KLE IN ELECTRIC TRIM OPT _ EQUIPMENT TABLE S 9 39 8 CU4OW1000 APjeA IW pj V5I on l f Y Coc00a lOT WOO No cao CNO0 Po 1 4 104 14...
Page 673: ...I 8XI 0 zED bc 9 b C c _A 44 I L IBTO CiTRL W EEL p II I J CONTROL WC EL AWSX VI T CONTRACT NO PAWNEE DIVISION OO E PAWNEE NAME rDATE E S na AIClAFT CO WICHITA KANSAS DESIGN KLtEIN 2 _ TITLE GROUP L PAINE _ I4L WIlR N6 DIAGRAM SATRWN KL I m ELECTRIC TR7I OPT CHEICK eS E e ST ESSI _ PrOJ SIZE COODE IDENT DWG NO OT E C 71379 SCALE OiNE Se1010 I PAGE 4 3 1 Electric Trim OPT Sheet 1 of 2 20 139 ...
Page 674: ... 2 2 CLurC CaRN BL C C Z4 3 BLU WWAT R JWL RE 5 W baw gu 14 9 CONTRACT NO PIAWNEC OIVISION O_ I PAW49n NAM OAT S Sn I CA l t AFT CO WICHITA KANSA O I I L 2 _ TITUL GoOUr Pl E WIR NG DIAGRAM lo Aw KL Z ELECCTR tC TRI OPT CNECK egs Ht q POJ seffn 1 e_ 3 1 tl I SI COO0 IOCNT OWG NO 0 7013 5 OTHER 1379 07701 _O______ SCALE f No St to to I AE 14 3 Electric Trim OPT Sheet 2 of 2 20 140 ...
Page 675: ...S T CAUS a S BaS 3 SIT H ____WIRE TABLE _ s 2 350 3 ClNNeTR CzR CONTRACT NO PAWKE DIVSIO 4 _ 30 A BL Y ________________________ 3 2 7 35 1 Y s5 IRE DATM NS YLssnL a IICRAFT CO WIC A KANSSl Z S 23 a DSYET_ ON SPgPCJERk q t 3 TITLE Z _ 3 4 st T ______ ou wl 4 Z WIRING DIAGRAM PART NO ofESCRIPTIOm DRAWN SKgNZ ER C R Ct3 I EQU PMENT TA LE o o CK tLEC TRIC TRIM OPT EQUIPMENT TABLE STRSS CES IOOO IS APP...
Page 676: ...So _ I _ I 3 I I co l uL f i TO camoL WMS L t ilL Tfli l COMTUOL WWE L AW CONTRACT NO PAWNe OIV i ues o CEssa AIRCRAFTCO W 0E PAWNEE o P WI 4 WRNOA DIAR AM oDwN SPE3 _ ELECTRiC TRiM OPT RED 13 7137 c zc O __ I __ _______ _____ I AoP _ v NO 139 07701 OTHER713 Electric Trim Sheet 1 of 2 20 140B 20 140B ...
Page 677: ...UN F RNF 5 IF I I Id 2 i CONTRACT NO PAWNEE DIVlSION 11S0S0 E PAWNEE NAME DATE Cen a AIRCRAFT CO WICHITA KANSAS DESIGN S q TITLE GROUP tI IR NG DIAGR AM O N S E R 3 E LT IC TI R IRI OPT CBECK m e AIr I SCTRCES I L e 1V DROJ DA T StIT CODE IDEN T DWC NSO EO TlEti C 71379 07 0 SCALE oIE CSe C7 3 I T4 I Electric Trim Sheet 2 of 2 20 140C 20 140D blank ...
Page 678: ...5 DRAWP 3BEMUELS p_ l _ STALL WARNING SYSTEM5AA Q TO CKr T KI EQUIPMENT TABLES 20TR2ES 1 O ATE CS LCu L 5 1uRS40TD ILEsU R OJ NG I SOO Tcr tu E I C5O Et Dw q NO 4C i E S U I A ER Axt D n AiO ON Z CESo X7CES00 SPElC nO R N A5 NO u J A _ r0 5 1 1 I iL WAR G rour 5 i _ WIRNER cDA RAM Z N K E4 21 13 NlT s6n O x 3 c f a M tnK auNipa eE FC i3 5 1 t 6b M3b l T14KU 5ER 5KsR Sz b 3 s IO HOIS IN G LLX GArcs...
Page 679: ...Jts IS IT __ _________ j_ _ oA MATMAL Li Tl3INlAI SE rALl _ a L AMP WiWIRE TABLE 5 1 t55 2P tcmucr M 5 zii VAC UUI SITC H _ I _ S N 5 1 37 1 J ousi m6 1NAu o ATR ACSaAIIC AFT CO C TA KANSAS 5 1 37 Z HOUlIMG oa____ R KLEIM 1 ei TiTL 7 S 1iO L cllurt wILAKi o ROUP w _ _ WIRING DIAGRAM _ r T NO 0 ow 0 a KLIAl IlAo i VACUUM Ocr WAItNG EQUIPMENT TABLE _esl YsrTF Tl8Z s _11M A s o l 0 0I croeo n j IP ot...
Page 680: ...O NOPAWNI I 1ton S1I00 I PAlIV l NAME DATE essn AIIRCAFT CO WIC IA s 2 C165008 0101 ACUUM PUMP DESIGN B t3 TITLE WIRING I M58I9 7 BKR GROUP WIRING DIAGRAM PART N0 DESCRITON DRAWN K LUNDY 10 3 4 STANDBY VACUUM PUMP EQUIPMENT TABLE CE MODEL TI CES KOO I APPLICASLE SUPRSEDES POJ i SIZE CODE IDENT DWG NO V N I CO A UOO NO 79 0770139 CCS XXX O C XA OPEC E NO C 71379 S XXXOR CMXXXX CESbMA BSUPERSEDED BY...
