Beechcraft TRAVEL AIR 95 Shop Manual Download

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Summary of Contents for TRAVEL AIR 95

Page 1: ...RAVEL AIR 95 TD 2 thru TD 302 B95 TD 303 thru TD 452 B95A TD 453 thru TD 533 D95A TD 534 thru TD 707 E95 TD 708 thru TD 721 SHOP MANUAL 95 590001 1 C 95 590001 1 C4 Reissued September 15 1967 Revised June 24 1983 ...

Page 2: ...PUBLISHED BY COMMERCIAL PRODUCT SUPPORT BEECH AIRCRAFT CORPORATION WICHITA KANSAS 67201 U S A Member of GAMA General Avianon A Raytheon Company Manyforturers Association ...

Page 3: ...1969 3 6 C September 15 1967 6 40 thru 6 47 C September 15 1967 3 6A and 3 6B C1 November 30 1976 6 48 AMEND lil March 1969 3 7 C2 November 4 1977 6 49 thru 6 60 C September 15 1967 3 8 C September 15 1967 7 1 thru 7 3 C3 August 10 1978 3 9 C1 November 30 1976 8 1 C3 August 10 1978 3 10 thru 3 15 C September 15 1967 8 2 C3 August 10 1978 3 16 and 3 17 C 6 October 1971 8 3 C September 15 1967 3 18 ...

Page 4: ... Door Estallation 4 17 illus 4 17 Aircraft Finishes 2 17 Adjustment 3 23 4 17 Removal 4 17 illus 4 17 Air Filter Replacement Gyro 3 31 Installation 4 17 illus 4 17 Teleflex Cable Removal Alternator 3 35 Removal 4 17 illus 4 17 and Installation 4 15 Belt Tension 3 37 Teleflex Cable Installation Down Spring Elevator Troubleshooting 3 61 and Removal 4 15 Installation 3 5 Anchoring and Mooring 2 10 Wi...

Page 5: ...sassembly 5 5 Forward L H Window Installation Radiator Inspection 3 25 illus 5 6 and Removal 4 18 Control System 3 23 illus 3 26 Wear Tolerances 5 5 Front Seat Removal and Controls Rigging 3 24 Main TD 1 thru TD 251 Installation 4 20 Fuel Filter 2 17 Assembly 5 9 illus 5 8 Fuel System illus 3 41 3 42 Fuel Discharge Nozzle Removal Disassembly 5 7 3 44 3 45 3 46 anctinstallation 4 15 illus 5 8 Cells...

Page 6: ... Removal 4 20 and Installation 4 12 Installation 4 9 Fifth and Sixth Installation Mounting Wing 4 4 illus 4 3 Removal 4 9 and Removal 4 20 Unfeathering Accumulator 2 15 Publications Front Installation and Supplementary Beechcraft Removal 4 20 N Publications 1 5 Selector Valve Fuel Removal and Installation 4 11 Vendor Publications 1 3 Shimmy Dampener 2 14 Nose Gear Retract Rod PumnpsŒHeanger Fuel 4...

Page 7: ...ire and Tube Mainten System 3 52 illus 3 53 Bendix Fuel Injection 3 70 ance 3 20 Troubleshooting 3 73 Engine 3 66 Window Starter 3 63 Engine Driven Deicer 3 72 Aft Removal and Installation 4 19 Surface Deicer Pressure 3 73 Generator 3 64 Cabin Door Removal and Wing Flap Electrical System 3 64 Heater System 3 60 Installation 4 19 Landing Gear System 3 65 Center Removal and Install Light Weight Rese...

Page 8: ...e immediately forward of the tie down lug On later serial airplanes the placard is attached to the lower right hand side of the fuselage adjacent to the flap WARNING Use only genuine BEECHCRAFT or BEECHCRAFT approved parts obtained from BEECHCRAFT approved sources in connection with the maintenance and repair of Beech airplanes Genuine BEECHCRAFT parts are produced and inspected under rigorous pro...

Page 9: ...ines No PC 106 Williams port Pa CARBURETOR Construction Operation and Adjustmerit Marvel Schebler Products Div Borg Warner Decatur Illinois Overhaul Instructions for Models MA 4 5 and MA 4 5AA Marvel Schebler Products Div Decatur Illinois FUEL INJECTION SYSTEM Operation Service and Maintenance Instructions for Type 530 No PD3530 Simmonds Precision Products Inc Tarrytown New York Bendix RSA 5 Fuel ...

Page 10: ...rhaul Iristructions Service Bulletin HES 62 77F Harrison Radiator Div General Motors Corp Buffalo New York COWL FLAP ACTUATOR Overhaul and Parts Breakdown Motor Driven Actuator No 4154 00 Dukes Astronautics Co South Gate California VACUUM PUMP Service Manual operation service and overhaul instructions including parts cata log Pesco Products Div Borg Warner Corp Bedford Ohio Overhaul Manual G 450 S...

Page 11: ...rt Worth Texas HEATER BLOWER Overhaul Instructions Vaneaxial Fan Part No M4861H 1A with Motor M 2916V Dynamic Air Engineering Inc Santa Ana California WHEELS BRAKES AND TIRES Maintenance Instructions for Wheels Brakes and Tires Used on the BEECH CRAFT Model 95 Travel Air P N AP 116 Goodyear Tire and Rubber Company Los Angeles California Maintenance Instructions for Goodyear 6 50 8 Brake Assembly 9...

Page 12: ...mblies and 95 32669 and 95 32926 Nose Wheel As semblies 98 33281 Servicing and Maintenance Instructions for Goodyear Multi Disc Brake Assembly 130409 Maintenance Instructions for the Beechcraft New matic Autopilot 1 6 ...

Page 13: ... the items which the customer sees and consequently can influence directly his decision to come back again or to go elsewhere The section includes a three view drawing giving the major dimensions of the Travel Air a table of hangar clearance dimensions and an access opening illustration A full page illustration shows the special tools with their part numbers which will make maintenance of the Trav...

Page 14: ... 2 Wing tip to ground 4 8 Wing tie down fittings to ground 3 0 Tail bumper to ground 2 11 HANGAR CLEARANCES AIRPLANE ON JACKS Shock struts extended wheels clear level flight attitude VHF antenna to ground 11 8 1 2 Wing tip to ground 5 0 Wing tie down fittings to ground 3 9 Tail bumper to ground 4 6 2 2 ...

Page 15: ...18 Airplanes prior to Serial TD 303 25 36 Airplanes prior to Serial TD 534 13 77 Airplanes Serial TD 303 and after 25 94 Airplanes Serial TD 534 and after Airplanes TD 638 and after have a One Piece Windshield Figure 2 1 Dimensions of Aircraft 2 3 ...

Page 16: ...13500 257606 272000 15250 1 000 0000 25250 49000 68000 im o IaM i31000 207000 247830 262 7263 268610 0 3885 Note VER CALnS BILIZER 1 Subtract 10 12 inches from given stations to ar rive at horizontal stabilizer stations for airplanes prior to serial TD 303 FUSELAGE 2 The station locations of the vertical stabilizer on air craft serial TD 303 and after are the same as those Airplane Serials TD 303 ...

Page 17: ...bilizer 5 Tail cone 6 Rudder bellerank and elevator down spring 7 Elevator bellerank and turnbuckles 8 Cable inspection 9 Landing gear actuator 10 Control cable pulleys and nose gear retract idler arm 11 Hinge bolts for nose wheel strut 12 Rudder tab actuator sprocket 13 Nose baggage door 14 Aft baggage compartment 15 Elevator bellerank elevator down spring and turnbuckles 16 Elevator tab cables 1...

Page 18: ...ell transmitter 8 Aileron bell crank 9 Auxiliary fuel cell transmitter 10 Wing tip spar fitting 11 Auxiliary tank siphon valve 12 Auxiliary tank access 13 Firewall terminal bus starter relay L H only 14 Engine access 15 Removable cowl nose cap TD 126 and after 16 Carburetor air filter 17 Removal wing leading edge cap 18 Wing mounting bolts 19 Flap access 20 Landing gear bolt 21 Aileron cable inspe...

Page 19: ...ARD WING NUT TORQUE WRENCH ADAPTER TS 1222 1 UPPER FRONT AND LOWER REAR WING BOLT NUT WRENCH TS 1222 2 UPPER REAR WING BOLT NUT WRENCH TS 1222 3 UPPER AND LOWER FRONT AND LOWER REAR WING BOLT WRENCH TS 1222 4 UPPER REAR WING BOLT WRENCH TC922 2 95910001 PROPELLER TORQUE WRENCH ADAPTER KIT 300 30 MODEL 300 IPi IS TO BE USED WITH SERVICE JACK THE MODEL 300 SERVICE JACK 50 590013 TS 1222 3 TS 1222 1 ...

Page 20: ...ace the 95 590017 sling adapters with 95 590017 1 sling adapters and add a 95 590016 23 spacer between Attach the hand towbar to the tow lug on the nose gear each sling adapter and the spar carry lower torque knee thru fitting Install with upper rear wing CAUTION attach bolts b Attach the sling assembly P N 95 590016 1 to When towing with a tug observe turn the sling adapters limits of the nose ge...

Page 21: ...OVED INSTALL 95 590017 ADAPTER HERE WITH WING INSTALLED 95 590016 23 SPACER WING ATTACH BOLT SPAR CARRY 95 590017 ADAPTER THRU FITTING SPAR CARRY THRU FITTINGWING SPAR FITTIN 95 590017 1 ADAPTER WING ATTACH BOLT VIEW B VIEW A Figure 2 7 Hoisting The Aircraft ...

Page 22: ...reens should be cleaned at each periodic oil change To clean the On aircraft TD 668 and after a pro suction screen remove the hex head plug at the rear tection feature is incorporated into the of the oil sump and pull out the screen To cleanthe external power circuit to protect pressure screen remove four bolts that secure the against a ground power unit with screen housing to engine accessory sec...

Page 23: ...o TD 533 except TD 506 allow contaminated fuel to drain from the system Fuel Regulator finger strainer 50 hours The four sump drains extend through the bottom of TD 506 TD 534 and after the wing skins the two selector valve drains are located at the system low spot to drain the intercon NOTE necting lines and extend through the bottom of the fuselage center section skin The fuel strainers are The ...

Page 24: ...a11 nicks or sharp edges which could damage the All measurements are made with the aircraft resting brake linings Worn dished or distorted brake discs on the gear should be replaced The fluid reservoir accessible through the forward baggage compartment should be f The shock strut pistons must be clean Remove checked regularly and a visible fluid level maintained foreign material by wiping the stru...

Page 25: ... cap and close the air supply valve the 38 49 or 65 cubic foot cylinder installed depend ing on the aircraft model The cylinders may be SERVICING THE PROPELLER UNFEATHERING located behind the nose cone or in the nose baggage ACCUMULATORS compartment To ensure proper operation the accumulator should To fill the oxygen cylinder close the shutoff valve in be checked periodically for correct pressure ...

Page 26: ...UTLET INSTALLATION OUT LET OUT LETS OXYGEN REGULATOR ALTITUDE COMPENSATED REGULATOR FILLER VALVE FOUR OUTLET INSTALLATION NOSE CONE NOSE BAGGAGE MOUNTED CYLINDER MOUNTED CYLINDER Figure 2 8 Oxygen System 2 16 ...

Page 27: ...omes jerky a little grease pro perly applied as follows should improve the operation g Reassemble the lock For service other than lubrication return the lock to the manufacturer FULLY EXTENDED RETAINING RING SPRING GUIDE 3 4 APPROX APPLY GREASE A NO GREALISGHTLY ERE NLY SPRING GUID BE IN THIS AREA MAIN ASSY COUNTERBALANCE SPRING Figure 2 9 Servicing Roton Locks AIRCRAFT FINISHES NOTE Paint Removal...

Page 28: ...ce of aircraft with laquer thinner or methyl ethyl ketone to remove shop primer exposed The following list is included to be used as a refer sealer and other shop soils ence should it become necessary to touch up or match an interior or exterior paint Each paint is listed d Lightly roughen all scratches with a nylon pad according to specific type and whether an exterior or to insure a satisfactory...

Page 29: ... 94 515 Do not use thinner or aromatic abrasive cleaners to clean the windows they will EXTERIOR AND INTERIOR PRIMERS damage the surface of the plastic Aliphatic naphtha and similar solvents are highly Interior Aluminum MIL P 8585 inflammable and extreme care must be Interior Magnesium Enmar EX 1479 taken when using them Exterior Aluminum Enmar EX 2016G or MIL P 8585 CLEANING DEICER BOOTS Exterior...

Page 30: ...318 1 Ignition Panel Light 327 Instrument Lights 327 Landing Gear Position Lights 327 Landing Lights 4553 4596 L G Visual Indicator Light 356 327 Map Light 303 Nose Baggage Light 307 O A T Light 327 Overhead Instrument Light 303 Post Lights 327 Reading Lights WEMAC 1870 Rotating Beacon A 7079B 24 Tab Position Indicator Light TD 1 thru TD 707 1819R TD 708 and after 1819 Tail Light 1203 Taxi Light N...

Page 31: ...phs or line drawings show the exact locations of the components and their adjustment or other maintenance procedures wherever practical cable tensions pressures measurements clearances and the like are tabulated directly on the illustration or shown on the details Detailed explanations of procedures have been limited to those instances such as rigging the landing gear where the proper sequence of ...

Page 32: ... chain reinstall new b Disconnect any electrical wiring safety wire c Rotate control column arm over to a near vert ical position and slide the control column off of the CONTROL COLUMN ARM INSTALLATION housing a Slide the control column on the control column RIGGING THE CONTROL COLUMN CHAIN housing b Install the chrome collar and attach with the two a With the control wheel in the neutral position...

Page 33: ...by measuring the f Check the surface travel to insure it agrees deflection in inches rather than degrees Given be with that shown on figure 3 2 low are the distances that points on the rudder and rudder tab should travel from 0 to the extreme in g Make sure that rudder movement corresponds to each direction Definite physical characteristics of the movement of the rudder pedals the surface such as ...

Page 34: ...ove the rig pin The rudder must be in the neutral position for this f Adjust elevator travel at the elevator stops on the inspection bellcrank in the fuselage tail section accessible through inspection openings on the fuselage under the horizontal b Carefully attach a dial indicator to the surface of the stabilizer Refer to figure 3 3 for elevator travel M rudder above the trim tab in line with th...

Page 35: ...AP TRANSMITTER AND INDICATOR TD 668 and After op 3 Flap actuator To adjust loosen mounting bolts and move fore and aft or rotate slightly LIMIT SWITCHES To adjust loosen mounting screw nuts slide switch forward or aft on bracket o C 1 Down limit switch 2 Up limit switch Figure 3 4 Flap System 3 6 ...

Page 36: ...dicular to the tab surface toward the indicator The reading on the dial indicator is the tab free play and it should If the rod end on the push rod assembly is worn not exceed 0 084 inch the push rod assembly should be replaced When connecting the tab push rod assembly to the tab e Ifthe free play exceeds 0 084 inch inspect allcom horn tighten the castellated nut against the rod ponents of the tab...

Page 37: ...ring connected the loads in the elevator system In Steet Bushing are to be as follows measured with hand force on control wheel a Remove the existing bushing from the tab horn and ream the hole in the tab to 3276 3291 inch inside diameter Airplanes Prior to Serial Airplane Serial TD 303 TD 303 and after b Using a clean rag dampened with methyl ethyl ketone or equivalent clean the hole in the tab h...

Page 38: ...utral positon tension to the alleron control cables The trimmer does not change the rigging of the system but should be removed d If the trim tab is not in the neutral position upon before checking cable tension To remove unscrew the two completion of step c adjust push rod to place tab in neutral body halves by holding the clutch body housing outer half position and turningthe clutch body nut inn...

Page 39: ...72 inch pounds you would add the required amount of nose heaviness O 2 inch pounds to give the total amount of tail heavy balance that must be compensated for Use this formula to determine the amount of weight to add Y X B Y Distance in inches from hinge center line to center line of the balance weight X The unknown weight to be added Using 3 inches as an example of the distance Y we have 3X 0 92 ...

Page 40: ...STEEL BE WITH JIG MUST BE HORIZONTALLY LEVEL Figure 3 6 Balancing the Alleron 3 11 ...

Page 41: ...t exceed 17 5 inch pounds Use this formula to figure the tail heaviness Static Tail Heaviness D W S D Distance in inches from hinge center line to point where spindle supports elevator W Scale reading of platform scale in pounds S Weight of spindle in pounds used to support trailing edge of elevator Remove the elevator horn cover and add or remove solder to bring the elevator balance within requir...

Page 42: ...JIG MUST BE HORIZONTALLY LEVEL I D s e i W Figure 3 7 Balancing the Elevator 3 13 ...

Page 43: ...the tail heaviness Static Tail Heaviness D W S D Distance from hinge center line to point where the spindle supports the rudder W Scale reading of platform scale in pounds S Weight of spindle in pounds used to support trailing edge of rudder Remove the rudder horn cover and add or remove solder to bring the rudder balance within required limits Coat the weight with a corrosion preventative materia...

Page 44: ...JIG MUST BE HORIZONTALLY LEVEL S w Figure 3 8 Balancing the Rudder 3 15 ...

Page 45: ...etting is obtained leave the disconnected upon the retraction of the gear the gears in the retracted position and screw the stop uplock arm may damage the top wing skin Place bolt down against the main strut To assure a firm the uplock block in the lower position seating insert a 003 feeler gage under the bolt head and adjust the bolt until a firm steady effort b Disconnect nose wheel door linkage...

Page 46: ...OR ADJUSTMENT C MAIN GEAR OUTBOARD DOOR ADJUSTMENT L G LIMIT SWITCHES STMENT C o CHECKINGMAIN GEAR DOWN LOCK TENSION MAIN GEAR UP LOCK SAFETY SWITCH ADJUSTMENT 1 UPLOCK ROLLER 2 UPLOCK BLOCK Figure 3 9 Landing Gear System Issued October 1971 3 17 ...

Page 47: ...ntinue this procedure Each pressure switch is connected into the pitot and until a snug firm fit is obtained when the door is static system The pressure switch in the gear up completely closed circuit is actuated by the pressure differential that exists between the pitot and static air system and p Connect main gear inboard door linkage retract will close with increasing pressure at approximately ...

Page 48: ...NCE AND ADJUSTMENT 4 Place the landing gear position switch in the UP position No maintenance is required for the landing gear safety system other than replacing defective units 5 Clamp a section of soft rubber tubing over the or checking the electrical wiring for condition pitot head inlet making certain the connection is security of attachment and tightness of electrical airtight Connections The...

Page 49: ...the wheel flanges and remove the self locking nuts and washers from the wheel bolts NOSE WHEEL TRAVEL STOP ADJUSTMENT Separate the wheel halves and remove the tire The travel stop must be adjusted so the nose wheel Smooth wheel abrasions nicks and burrs with a travel is stopped when the shimmy dampener is fine file and retouch with zinc chromate primer and 1 32 to 1 4 inch from its maximum travel ...

Page 50: ...take up slack in the actuator wire Tighten the screw Connect the hoses from a pressure pot to the bleeder and locknut down on the brake actuator wire Pull fitting on the brake and bleed the system from the the brake control to the on position and pump the wheel cylinder up Disconnect the fluid supply line brakes to see if the pedals are solid íf the brake at the reservoir attach a hose to it and p...

Page 51: ... 690 AND TD 694 TD 697 DETAIL C a 2 1 DISC CLIP 2 ANVIL SIDE LINING 3 PISTON SIDE LINING 4 PISTON TD 708 AND AFTER TD 691 THRU TD 707 EXCEPT TD 694 TD 697 LINING TORQUE FLANGE o TORQUE PLATE BACK PLATE o INSULATOR a STATIONARY DISC DISC PISTON PRESSURE PLATE PISTON SHIM ROTATING DISC CYLINDERS PRESSURE PLATE TORQUE PLATE HOUSING Figure 3 11 Brake System 3 22 ...

Page 52: ...taining plate The locating pins for the lining section are peened into the retaining plate See figure 1 It is not necessary to drill out these locating pins to remove the brake lining To remove the lining apply a screwdriver or a similar prying tool between the retaining plate and the lining the lining should then pop off Replace the lining by fitting a new lining section over the locating pins in...

Page 53: ......

Page 54: ...erminal to properly seal the door the brake housing and the torque flange indicates the need for lining replacement Anvil lining worn to If the door does not open freely the main door 5 32 inch thick measured from the rubbing surface latch may not be retracting enough This can be to the back at the lining center should be replaced corrected by removing the upholstery panel below Piston lining worn...

Page 55: ...e ductstat switch is in the straight upright position before securing the control wire on aircraft prior CERAMIC to Serial TD 453 and in the straight downward AREA position on airplane Serial TD 453 and after SPARK PLUG INSPECT FOR WELL CARBON HERE OVERHEAT THERMOSTAT Figure 3 12 Aircraft Heater Spark Plug The overheat thermostat is controlled by an adjust ing screw on the bottom of the thermostat...

Page 56: ...n or wash down is en countered The following information is intended to serve as a guide for testing Janitrol heaters without removal from the aircraft This test will determine whether TESTING THE PITOT SYSTEM FOR LEAKS leakage through the combustion chamber is within the allowable limits or if the heater should be A functional test of the pitot system can be made by overhauled using an observer i...

Page 57: ...STATIC BUTTON STATIC UNE DRAIN EMERGENCY STATIC AIR SOURCE AND DRAIN B INSTRUMENTS PITOT Figure 3 15 Pitot and Static System ...

Page 58: ...n prior to TD 534 Thru TD 707 638 accessible through the inspection opening in a Start only one engine and set the throttle to the left side of the baggage compartment Hoses obtain 2200 rpm with outer surfaces checked or cracked particu larly at the bends or connecting points or which have become hard should be replaced Replace b Adiust the appropriate vacuum regulator behind the mstrument panel t...

Page 59: ...ELECTOR E E 11 111 E I i a VACUUM REGULATOR VACUUM REGULATOR E E E VACUUM PUMP VACUUM PUMP TD 1 Thru TD 533 OPTIONAL CHECK VALVE CHECK VALVE VACUUM VACUUM REGULATOR REGULATOR VACUUM GAGE GYRO HORIZON DIRECTIONALGYRO L H VACUUM PUMP R H VACUUM PUMP TD 534 Thru TD 670 Figure 3 16 Vacuum System 3 30 ...

Page 60: ...ment adjustable orifice on the LH side of the aircraft forward of the instrument panel near the top of the upholstery panel See Figure 1 g Loosen the check nut and rotate the orifice body counterclockwise to increase the pressure and clockwise to decrease the pressure to obtain a reading of 2 5 5 0 inches of Hg on the gyro pressure indicator with the engine operating between 600 and 650 rpm h Tigh...

Page 61: ...Insert opposite Page 3 31 Amendment ll ADJUSTABLE ORIFICE PRESSURE MANIFOLD NOT INSTALLED ON MODELS 33 35 36 Figure 1 Page 2 of 4 lssued February 1969 ...

Page 62: ...low pressure section of the regulator section with the solenoid attached and rotate the adjusting screw clockwise to obtain a reading of 7 5 5 psi on the pneumatic pressure gage with the engine operating at 2200 rpm and the deicer OFF c Tighten the check nut on the low pressure section of the regulator d Loosen the check nut on the high pressure section of the regulator section without the solenoi...

Page 63: ... nut and adjust the turn and slip orifice to 2 2 inches of Hg with the engines operating at 2200 rpm Rotate the adjusting screw counterclockwise to increase the pressure and clockwise to decrease the pressure d Tighten the check nut remove the test gage and reinstall the plug in the orifice e Reinstall the glareshield and or radio panel EVT GYRO TEST GAGE PRESSURE MANIFOLD AUTOPILOT MASTER VALVE B...

Page 64: ...ines and set the throttles at gyro indication 2200 rpm The pressure gage should read between 3 5 to 4 5 To replace the filter assembly on the instrument remove the air filter body cover by taking out the four fillister head machine screws Lift out the CLEANING THE SUCTION RELIEF VALVE snap ring which holds the filter in place remove SCRE EN the filter and replace it with a new one Replace the air ...

Page 65: ...O DIRECTIONAL GYRO DIRECTIONAL HORIZON GYRO HORIZON GYRO ORIFICE PRESSURE LINE PRESSURE VENT LINE GAGE O MANIFOLD FILTER PRESSURE RELIEF VALVE FILTER AIR PUMP FILTER Figure 3 18 Pressure System TD 708 And After 3 32 ...

Page 66: ...on for No 1 cylinder by means of the advance timing marks on the rear face of the starter ring gear This is done by attaching an ignition timing pointer to the Adjustment Screws ring gear with the pointer accurately lined up with the timing mark on the rear face of the gear The crankshaft is then rotated O O in its normal direction of rotation until the pointer is in alignment with the crankcase p...

Page 67: ...ours The impulse coupling magneto can be used Any time the magneto harness cable outlet plate is only on the left side of the engine when removed check the height of all distributor block viewed from the rear or accessory housing contact springs using a flush pin gage This dimen end sion is determined by measuring from the top of the block outlet tower down to the top of the spring see illustratio...

Page 68: ...t be reset To adjust voltage setting remove cover and turn adjusting screw clockwise to increase voltage and GENERATOR BRUSH WEAR LIMIT counterclockwise to decrease voltage setting Generator brushes should be replaced before their CAUTION maximum wear limits are reached The minimum permissible brush length is one half its original If adjusting screw is turned down clockwise length beyond the norma...

Page 69: ...r relay 17 Nav light flasher omit when rotating beacon used 6 Flap motor circuit breaker and switches 18 Landing gear limit switches 7 Paralleling relay 19 Flap limit switch 8 R H relay starter 20 Landing gear motor 9 Landing gear warning switch 21 Dynamic brake relay 10 Landing gear warning horn 22 Wing flap control 11 Stall warning horn 23 Batteries 12 Flasher 24 Nose landing light Figure 3 21 E...

Page 70: ...reconnect the linkage rod sible brush length is 3 8 inch When replacing a worn to the bellcrank brush the new brush should be properly seated Wrap a strip of 00 sandpaper rough side out around the starter commutator and allow the brushes to ELECTRICAL UTILIZATION LOAD CHART ride against the sandpaper Rotate the starter until the brushes match the contour of the commutator Starter brush should be r...

Page 71: ...th a special high low temperature grease which is intended to last the lifetime of the Anti ice indicator post cable under normal operating conditions However light 1 04 in extremely hot or dusty climates relubrication of the cable may be necessary every two years of serv Only one indicator light will be operating at any ice given time To remove a cable disconnect the casing nut from the Optional ...

Page 72: ...ith anti seize accordance with the FLARE FITTING AND HOSE compound in accordance with the TABLE OF THREAD FITTING TORQUE CHART FLARE FITTING AND HOSE FITTING TORQUE CHART WRENCH TORQUE FOR TIGHTENING HOSE END FITTING AND ANB18 NUT POUND INCH HOSE ASSEMBLIES POUND INCH TUBING ALUMINUM ALLOY OD TUBING FLARE STEEL TUBING INCHES AND 10061or AND 10078 FLARE AND 10061 MI NI MUM MAXI MUM MINIMUM MAXIMUM ...

Page 73: ... stop screw so that the engine Check the idle mixture by moving the cockpit mix idles at approximately 550 rpm Turn the idle adjust ture control lever with a smooth steady pull to ing screw toward the rich position till the engine rolls ward Idle Cut off and observe the tachometer for from richness then turn the screw toward the lean any change Return the mixture control to Full position till the ...

Page 74: ...n the firewall on air craft prior to serial TD 174 except TD 127 BOOST PUMP ENGINE DRIVEN FUELPUMP AUXIDARY TANK ENGINE PRIMERS C AlN TANK CARBURETOR CHECKVALVE Figure 3 23 Fuel System Airplanes Prior to TD 453 except TD 127 and TD 444 3 41 ...

Page 75: ...L EXCEPT TD 127 PRIMER MAIN FUEL TANK MAIN FUEL TANK FUEL PRESSURE GAGE DRAIN O o TANK OVERFLOW AUX FUEL TANK AUX FUEL TANK L T VENT AND CHECK VALVE CDRAIN TD 174 AND AFTER FUEL STRAINER FUEL STRAINER ELECTRIC F UEL PUMP TD 174 AND AFTER FUEL DRAIN CHECK VALVE Figure 3 24 Fuel System Schematic Airplanes Prior to TD 453 Except TD 127 and TD 444 ...

Page 76: ... 113 172 MAIN TANK 39 GALLON STANDARD 25 GALLON OPTIONAL DRAINS FUEL STRAINER BOOST PUMP FLUSH TYPE VENT SELECTOR VALVES RE TURN LINE AUXILIARY FUEL IN RcNTI N PUM CHECK VALVE r TO FUEL GAGE THROTTLE BODY ASSEMBLY Figure 3 25 Fuel System TD 127 TD 444 TD 453 thru TD 533 3 43 ...

Page 77: ...SS FEED ENGINE SUPPLY I 1 INLET OUTLET CHECK VALVE CHECK VALVE R H SELECTOR L H SELECTOR AUXILIARY AUXILIARY VALVE VALVE PUMP DRAIN DRAIN PUMP FUEL STRAINER FUEL STRAINER DRAIN DRAIN CROSS FEED LINES TO CABIN HEATER MAIN TANK MAIN TANK 39 GAL STD 39 GAL STD VENT 25 GADL OPN D2R5AAL OPT min 31HB VENT CHECK VALVE CHECK VALVE L L VENTC V S LECT R CH VEVEN PRESSURE DRAIN RETURN DRAIN VENT DRAIN Figure...

Page 78: ...ng station 113 172 MAIN TANK 40 GALLON STANDARD j 25 GALLON OPTIONAL DRAINS 7 BOOST PUMP FUEL STRAINER FLUSH TYPE VENT SELECTOR VALVES 7 FLOW DIVIDER INJECTION REGULATOR FUEL PUMP TO FUEL FLOW GAGE CHECK VALVE Figure 3 27 Fuel System TD 506 TD 534 and After 3 45 ...

Page 79: ...PLY OUTLET DRAIN OUTLET L H SELECTORVALVE FUELSTRAINER R H SELECTOR VALVE BOOST PUMP DRAIN DRAIN CROSS FEEDLINES MAIN TANK MAIN TANK VENT 40 GAL STD 40 GAL STD VENT Œ0EEE 25 GAL OPT 25 GAL OPT DRAIN DRAIN VENT AUXiLIARY TANK SELECTORVALVE AUXIMARY TANK VENT 31 GAL OPT 31 GAL OPT DRAIN DRAIN Figure 3 28 Fuel System Schematic TD 506 TD 534 and After ...

Page 80: ...tely 30 revolutions INLET PRESSURE PS1 REGULATED PRESSURE The low rpm adjustment is made while the aircraft PSI is on the ground To make the adjustment pull the propeller lever back against the detent and observe 3000 17 0 the rpm setting If the rpm varies from the specified 2500 18 0 low rpm setting of 2000 rpm the low rpm setting 2000 19 0 must be adjusted The low rpm adjustment is made 1500 20 ...

Page 81: ...adjusting ring to increase or decrease the pop off pressure 5 Set the adjusting ring on the valve so that the pop off pressure is from 15 17 psi 6 Relock the adjusting ring to the valve body with the cotter pin LIGHTWEIGHT AUTOMATIC PUMP DRIVEN SURFACE DEICER SYSTEM The following description applies to deicer systems utilizing Goodrich control valves but is applicable also to systems incorporating...

Page 82: ...s then reapplied to the boots tem also contains a gage in the cockpit to register system pressure and a standard reset type circuit Through the electric timer the solenoid operated breaker to protect the deicer system electrical control valves cause all of the boots to be inflated circuit simultaneously therefore the system is described as a single inflation type Since the control valves operate s...

Page 83: ...o y abilizer Boot R H Wing Boot Control Control L H Wing Boot Valve Valve Overboard MIO I Y lyy Overboard Vent Vent Oil Separator Oil Separator Pressu Gage Vacuum Pump Vacuum Pump Figure 3 34 Lightweight Automatic Pump Driven Surface Deicer System With Tavco Valves 3 50 ...

Page 84: ...he deicer boots should inflate and remain inflated while the switch is retained a Cap the overboard port of the control valve in in the MANUAL position Check for correct system either the left or right nacelle pressure b Connect a source of clean air to the inlet port c Release the deicer switch permitting it to of the capped control valve A minimum inlet pres return to the OFF position the deicer...

Page 85: ...ecessary to apply slim nose pliers Mter 5 to 8 seconds the relay returns the distri to the pin projection in order to pull the poppet butor valve to the original or evacuate position from the valve In the evacuate position the air flow is routed through an integrated venturi which creates a 3 Thoroughly clean the control valve bore and vacuum in the deicer supply lines to hold down the poppet with...

Page 86: ... TAIL BOOT LEFT TAIL BOOT VENTURI NOZZLE DISTRIBUTOR VALVE RIGHT WING BOOT LEFT WING BOOT DEICE PRESSURE GAGE PRESSURE MANIFOLD TO AIR PUMPS TO AIR PUMPS PRESSURE SIDE I I I Figure 3 35 Surface Deicer Pressure TD 708 And After 3 53 ...

Page 87: ...n about four hours however the boot may be inflated to check the repair after a minimum of 25 minutes The deicer boots are installed as a permanent instal lation and should not be removed except when vul j Apply one light coat of A 56 B cement to the canized repair at the factory is required patched area extending beyond the buffed area to restore the conductive surface Allow the cement to dry tho...

Page 88: ...er before beginning the clean air pockets If the boot does not follow the chalk line ing operation Wét a clean cloth with toluol and care on the leading edge pull it up immediately with a fully clean the rough back surface of the boot Change quick motion and reposition properly Now complete cloths frequently to avoid contamination of the clean the installation by activating the adhesive surfaces e...

Page 89: ... the boot for bonding 14 25 at Wing Station and 14 03 at Wing a Mask the perimeter on the ribbed side with 1 2 inch tape to prevent excessive curling of the feather 120 38 Station 132 25 ed edges after the cement is applied b Sand the smooth sides thoroughly with No 280 Figure 3 36 Stall Strip Installation paper abrasive and clean with naphtha The boot is now ready to install on the blade d When d...

Page 90: ...ANTI ICE S O D PUMP PROPELLER ANTI ICE INSTALLATION Figure 3 30 Propeller Anti Icer TD 1 Thru TD 452 ...

Page 91: ...Ca i 91 CD ANTI ICE RESERVOIR AND PUMP PROPELLER ANTI ICE INSTALLATION Figure 3 31 Propeller Anti Icer TD 453 and After ...

Page 92: ... e Allow the second cement coat to dry about 30 f Remove the masking carefully so that the 1 4 minutes before placing the boot into position Do this inch glue line around the boot remains undisturbed by aligning the feed end center with the propeller hub mark and working outward It is necessary to stretch g Remove any trapped air with the aid of a hypoder the boot lengthwise over the blade in the ...

Page 93: ... Remove obstructions or repair leaks 2 Heater will not shut off a Defective ductstat a Connect voltmeter across automatically ductstat leads and operate con trol As the ductstat is pulled out voltage should decrease If not replace ductstat 3 Heater backfires inter a Loose connection in control a Check electrical connections mittently circuit or loose ignition lead to spark plug b Mixture too rich ...

Page 94: ... Beech craft Certified Service Station ALTERNATOR TROUBLE SYSTEM EFFECT PROBABLE CAUSE 1 Output Transistor Shorted a High system voltage a F terminal of generator has been grounded b Battery overcharge b Poor ground in system or poor con nection at generator or regulator c Lights burning out c Regulator too hot d Ground in wiring between F termi nals of generator and regulator e Defective transist...

Page 95: ...Ground in wiring between F termi nals of generator and regulator e Defective transistor f Shorted field in generator g Defective diode 10 Transient Suppression a Output transistor may short a Reverse battery polarity Diode Open from transients depends on b High positive transient from exter application nal source 11 Filter Capacitor Open a Poor switching may or may a Defective connection not fail ...

Page 96: ...ay d Check relay for operation Replace if necessary 2 Power on with master a Master switch defective a Check switch for operation switch off Replace if necessary b Battery relay contacts stuck b Replace relay STARTER TROUBLE PROBABLE CAUSE CORRECTION 1 Both starters inoperative a Circuit breaker tripped in a Reset starter switch circuit b Starter relay inoperative b Check continuity of starter sys...

Page 97: ...e air jet to remove grit g Defective voltage regulator g Replace regulator h Defective ammeter h Replace ammeter 2 No generator output a Circuit breaker tripped a Reset b Open circuit b Check continuity of circuit c Loss of residual mag c Flash generator field netism d Defective generator control d Test switches Replace if switch or current relay defective 3 Low generator output a Generators not p...

Page 98: ...of a Readjust switch shut off when gear is re adjustment tracted b Defective switch b Replace switch 2 Landing gear fails to a Safety switch not closing a Readjust switch retract b Up limit switch remaining b Replace switch open 3 Landing gear motor fails a Down limit switch does not a Readjust limit switch to shut off when gear is open extended b Defective down limit switch b Replace switch 4 Lan...

Page 99: ...tle to one tenth of its range e Defective spark plugs e Clean and adjust or replace spark plug or plugs f Defective ignition wire f Check with electric tester and replace any defective wires g Defective battery g Replace with charged battery h Improper operation of h Clean points Check timing magneto breaker points of magnetos i Water in carburetor or 1 Drain carburetor or fuel fuel injector injec...

Page 100: ... timing h Check magnetos for timing and synchronization i Defective spark plug ter i Replace connectors on spark minal connectors plug wire j Incorrect valve clearance j Adjust valve clearance 4 Failure of engine to a Throttle lever out of a Adjust throttle lever develop full power adjustment b Leak in the induction system b Tighten all connections and replace defective parts c Restrietion in carb...

Page 101: ... g Defective temperature gage g Replace gage 8 Excessive oil a Law grade of 011 a Use only oil which conforms to consumption engine specifications h Defective bearing b Inspect sump for metal particles If metal particles are present overhaul of engine is required c Worn piston rings c Install new rings d Incorrect installation of d Install new rings pisten rings MAGNETOS TROUBLE PROBABLE CAUSE COR...

Page 102: ...mproper internal timing or improperly meshed distributor gears e Magneto improperly timed e Check magneto to engine timing to engine f Advance breaker out of f Check magneto internal timing adjustment internal timing off g Retard points opening too g Check timing of retard points late or impulse coupling or impulse coupling timed wrong 2 Engine Roughness a Defective spark plugs a Try new spark plu...

Page 103: ... defective 6 Low fuel pressure or fuel a Clogged fuel strainer either a Remove and clean strainer with starvation finger strainer in the throttle pressurized air Inspect strainer body or fuel strainer in the for deterioration prior to rein wheel wells stalling 7 Fluctuations of fuel pres a Dirty fuel filter screen a Remove the hex nut on the side sure gage needle of the throttle body Remove and cl...

Page 104: ...or not g Blow out lines and inspect connected connections 2 Deicers do not deflate a Cycling valve not operating a Check cycling control cable for or deflate slowly properly proper adjustment and possible mechanical interference b Plumbing blocked or not b Blow out lines and inspect connected connections c Check valve malfunctions at c Observe check valve Unplug cycling valve assembly outlet repai...

Page 105: ... f Piping lines kinked blocked f Inspect lines and connections or not connected blow out lines g Leak in system g See System Checkout Air Leakage Test 2 Deicer boots inflate too a Piping lines kinked par a Inspect lines and connections blow slowly either or both blocked or not connected out lines engines operating at securely minimwn cruise rpm for a period of eight b Leak in system b See System C...

Page 106: ...boot puncture d Repair as prescribed in this section or replace e Distributor valves not e See Items 4 and 5 Troubleshooting functioning Chart f Piping lines kinked f Inspect lines and connections blocked or not connec blow out lines ted g Leak in system g See system checkout locate and repair 2 Deicer boots inflate too a Piping lines kinked a Inspect lines and connections slowly either or both pa...

Page 107: ...re in c Disconnect lines at the outlet distributor valve ports of the distributor valve and check valve operation with a gage If trouble is not found in the distributor valve inspect boots and lines for leaks or blockage 5 One or more boots inflate a Exhaust port of distri a Reroute exhaust line to low but do not deflate readily butor valve not vented to pressure area with pressure gage at normal ...

Page 108: ...blies of the Travel Air Step by step procedures are given only where it is considered necessary because the process is complex such as the removing and installing of the wing and the installing of the wing panel leading edge A table of torques on major assemblies is included in this section 4 1 ...

Page 109: ...he shaft to the fuselage the wire to the engine case If grounding is n Remove the lower aft nacelle fairing assembly impractical remove the cable outlet plate on o Remove the leading edge cover of the wing the rear of the magnetos or disconnect all the located between the fuselage and nacelle spark plug leads p Remove the clamps securing the wiring bundles to the wing inboard leading edge Disconne...

Page 110: ... WING FITT1NG NAS143 12 WASHER NAS143 12 WASHER WET BOLT TORQUE 2480 TO 2600 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHERS WING FITTING BOLT BORES AND EXPOSED BOLT THREADS WITH MIL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND TD 3 thru TD 24 TD 2 TD 25 thru TD 721 AN NAS143 12 WASHER MAY BE USED BETWEEN THE NUT AND THE NAS143 12 OR 95 110025 1 WASHER TO PROVIDE BOLT GRIP ADJUSTMENT 95 31 68 Figu...

Page 111: ...S143 10 WASHER FUSELAGE FITTING WET BOLT TORQUE 1180 TO 1300 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHERS WING FITTING BOLT BORES AND EXPOSED BOLT THREADS WITH MIL C 16173 GRADE 2 CORROSION PREVENTIVE COMPOUND TD 3 thru TD 24 TD 2 TD 25 thru TD 721 AN NAS143 10 WASHER MAY BE USED BETWEEN THE NUT ANDTHE NAS143 10 WASHER OR THE 95 110025 3 WASHER TO PROVIDE BOLT GRiP ADJUSTMENT 95 31 66 Figure 4 1...

Page 112: ...S WING FITTING WET BOLT TORQUE 2880 TO 3000 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHER WING FITTING BOLT BORES AND EXPOSED THREADS WITH MIL C 16173 GRADE 2 COAROSION PREVENTIVE COMPOUND CHECK WASHER FOR A SMOOTH CONTINUOUS OUTER RADIUS 55 31 15 Figure 4 16 Lower Forward Wing Bolt Installation C4 4 5 ...

Page 113: ...LETE RADIUSAND POSITION RADIUS TOWARD FITTING WET BOLT TOROUE 2480 TO 2600 INCH POUNDS COAT THE COMPLETE BOLT NUT WASHERS WING FITTING BOLT BOAES AND EXPOSED BOLT THREADS WITH MIL C 16173 GRADE 2 CORROSt0N PREVENTIVE COMPOUND TD 3 thru TD 24 TD 2 TD 25 thru TD 721 AN NAS143 12 WASHER MAY BE USED BETWEEN THE NUT ANDTHE NAS143 12 OR 95 110025 1 WASHER TO PROVIDE BOLT GRIP ADJUSTMENT 95 31 67 Figure ...

Page 114: ...each side Each bolt must be inserted by hand without of the upper nacelle binding If a bolt cannot be easily inserted i Connect the plumbing between the wing root rib reposition the wing until the bolt moves freely and the fuselage in the fittings Do not screw or drive the bolt j Connect the flap wire bundle and plumbing in the into the fittings aft wheel well k Replace all clamps securing wiring ...

Page 115: ...spection replacement cycle of the wing decrease its lift or lower the trailing edge of the heavy wing attach bolts if both wings are full up to increase its lift as follows 1 Using a grease pencil outline the position of a Before removing any wing attach bolt draw an the wing on the fuselage outline of the wing position on the fuselage with a grease 2 Place the airplane on a 3 point jack and raise...

Page 116: ...rations DO NOT INSTALL corrosion cracks and mechanical damage The cadmium THE BLACK P N H 20 NUTS these nuts plating may display areas that appear rubbed discolored or have been dry film lubricated with molybdenum polished These areas are usually the result of prevailing disulfide When MIL C 16173 Grade II installation procedures and are of no significance A bolt corrosion preventive compound is a...

Page 117: ...e wing bolt wrenches do not Lubricated Bolt identification Placard Location bottom out on the wing fittings This could Figure 4 1D result in damage to the wing fittings and erroneous torque readings the nut with MIL C 16173 Grade 11 corrosion preventive compound 5 Chart 2 k Check that the decal shown in figure 4 lD is i Torque the nut to the wet torque value shown in affixed to the appropriate loc...

Page 118: ...bove the surface of the part The presence of the leakage Minute electrical arc burns caused by improper field denoting the discontinuity is detected by the use of operation of the test equipment can result in finely divided ferromagnetic particles over the surface of eventual failure of the part the part Some of the particles are magnetically gathered and held by the leakage field to form an outli...

Page 119: ...s positioned between the heads of the Inspection of the upper and lower spar caps should be wet horizontal equipment The magnetic particle accomplished in the following manner suspension is flowed on the nut and the appropriate current is applied through the central conductor to achieve a Examine the forward and aft sides of the spar cap adequate field strength Using the described procedure where ...

Page 120: ... moving a straight edge over the surface or by sighting down the length of the spar cap surface NOTE Install the flap track rollers four rollers per If unusual conditions are encountered that cannot be flap and two rollers per track in the flap track resolved locally contact the Commercial Service brackets with the flanges facing each other Department of Beech Aircraft Corporation for evaluation U...

Page 121: ......

Page 122: ...s and remove the removing the main strut assemblies flap motor g Reinstall the flap motor by reversing the above When reinstalling the landing gear lubricate all fitfings with removal procedure grease Specification MIL G 7711 Torque the nuts on the main gear hinge bolts 250 to 800 inch pounds There is no REMOVING AND INSTALLING THE LANDING specified torque for the nose gear attaching bolts Operate...

Page 123: ... VERTICAL STABILIZER Front and rear spar mounting 50 70 inch pounds bolts HORIZONTAL STABILIZER The mounting bolts in the 50 70 inch pounds front and rear spar and the bolt that attaches the elevator horn hinge to the rear spar bracket PROPELLER 650 675 inch pounds LANDING GEAR Main gear brace support arms 200 250 inch pounds Main gear hinge bolts 250 800 inch pounds Main wheel halves Goodyear 140...

Page 124: ...N The B 1322 shim must be installed or the propeller re taining bolts may fail due to relative movement of the two flanges c Install the O ring on the engine shaft d Position the propeller on the engine Install the propeller mounting bolts and torque the bolts to 650 plus 25 minus 0 inch pounds Safety wire the bolts e Install the two high pitch stop assemblies f Check the propeller installation fo...

Page 125: ...a Aircraft prior to Serial TD 453 except TD 127 and TD 444 and aircraft TD 506 TD 534 and after To remove the fuel pump disconnect all fuel pump plumbing and remove the bolts and pump Replace the fuel pump gasket when reinstalling the fuel pump and make certain that the pump actuator arm is in line with fuel pump plunger in the engine accessory case Aircraft serials TD 618 and after use straight t...

Page 126: ...ALLING THE MAIN FUEL CELLS CAUT ON The parts of the aerobatic reservior type fuel cells baffled and non baffled fuel cells are not interchangable When installing a new fuel cell use only those items pertaining to that particular cell being installed Extreme care should be used when installing the finger fuel strainer to prevent damage to the fuel cell The long finger fuel strainer approximately 9 ...

Page 127: ... the wing g Disconnect the fuel cell plumbing at the access hole on the underside of the wing h Unsnap the fuel cell and remove it from the wing cavity i Reinstall the fuel cell by reversing the above removal procedure NOTE If the fuel cell is to be stored for a period of 10 days or longer coat the inside of the cell with light engine oil to prevent cracking and deterioration C3 4 11 ...

Page 128: ...inner fuel cell liner described below and in Service Instruction 0365 281 door at the inboard access door Serials TD 722 and after were delivered from the factory d Disconnect the plumbing at the inboard and with the equivalent of kit 35 9009 S installed outboard ends of the fuel cell e Remove the drain plug from the inboard aft a Remove the fuel cell as described in corner of the fuel cell REMOVI...

Page 129: ...E MAIN FUEL CELLS for further d Remove the three landing gear motor attaching instructions on installing the fuel cell bolts and remove the landing gear motor e Reinstall the landing gear motor by reversing the above removal procedure and safety the three attaching bolts NOTE REMOVING AND INSTALLING THE LANDING Installation of Kit 35 9009 S is required on a GEAR ACTUATOR first time basis only for ...

Page 130: ... aircraft prior to TD 534 except TD 506 support the brake disc to prevent it from dropping and striking the axle when the wheel is removed c Disconnect the brake hydraulic line remove the brake assembly at taching bolts and remove the brake assembly INSTALLING THE WHEEL AND BRAKE ASSEMBLY a On aircraft prior to TD 534 except TD 506 place the brake housing on the axle and position the housing on ax...

Page 131: ...lts that attach the iris valve to the fiberglass plenum and lift the blower and iris valve from the plenum d Disconnect the heater ignition lead from the spark plug and the heater igniter e Disconnect the combustion air flexible tubing from the combustion air inlet at the heater f Remove the fiberglass plenum from the heater by removing the clamp and asbestos strip g Disconnect the fuel inlet line...

Page 132: ...disconnect the iris valve control e Remove the clamp securing the fiberglass plenum to the heater and lift plenum and blower assembly forward f Disconnect the ignition lead at the spark plug and remove the plenum and blower assembly g Remove the fuel inlet cover and disconnect the combustion fuel inlet line h Remove the screws securing the fuel inlet shroud assembly and re move the shroud assembly...

Page 133: ... the newly prepared clamps between the shoulders on the lower end of the cable housing and attach the safety wire remaining in the door to the upper end of the cable g Pull the cable into position by gripping it with vise grip pliers below the shoulders at the lower end Pull on the safety wire attached to the upper end while tapping on the vise grip pliers to drive the cable through the door chann...

Page 134: ...taining screws and move the latch tongue guide outboard to create additional ten sion on the latch tongue Air leaks around the upper portion of the door may be caused by improper adjust ment of the upper door latch This may be corrected by removing the small upholstery panel above the door window and adjusting the length of the upper latch control cable Shorten the cable sufficiently by screwing i...

Page 135: ...e trim strip from around the inside of WINDSHIELD INSTALLATION the window a Clean the sealer from the canopy section where d Remove the screws and nuts attaching the storm the old windshield was removed using toluol window strike to the window frame b Trim the tooling tabs from the windshield place e To facilitate reinstallation mark the location of the windshield in position and mark the areas wh...

Page 136: ...ecessary i Install the trim strip m Reinstall the upholstery panels j Clean and paint as necessary k Reinstall the center upholslery panel CABIN DOOR WINDOW REMOVAL 1 Reinstall the inboard door handle ash tray and a Remove the inboard door handle ash tray and arm rest arm rest CENTER WINDOW REMOVAL AND INSTALLATION b Remove the center upholstery panel a Remove the emergency release pin c Remove th...

Page 137: ...ck support rod from the mounting brackets and fold the seat back forward a Place the seat in position and align the seat guides with the mounting track c Remove the attaching bolts and seat b Release the fore and aft adjustment lock and FIFTH AND SIXTH SEAT INSTALLATION slide the seat onto the mounting track Engage the fore and aft lock and make certain the seat is se a Position the seat and secur...

Page 138: ...basis only Repair procedures such as welding brazing building up with weld material and machining to size etc cannot be given a blanket endorsement since each such case must be evaluated individually This section is intended rather as a guide to normal overhaul its goal being the restoration of the parts to full serviceability As the necessity arises or the information becomes available overhaul i...

Page 139: ...O ring 15 Felt pad 13 14 15 16 16 Felt lubricating liner 28 17 Bearing 17 18 Barrel 18 1290 SShimpmyr dampener go 21 Adapter ring 25 29 22 Snap ring 23 Fork assembly 31 24 Lower torque knee pin 30 24 23 25 Torque knees 26 Upper torque knee pin 27 Torque knee bushing 28 Upper torque knee bushings 29 Piston 30 Lower torque knee bushings 31 O ring Figure 5 1 Nose Landing Gear Shock Strut Assembly Air...

Page 140: ...the collar to the barrel and slide the collar and shim il one is installed off Do not unscrew the air valve assembly until all the barrel Keep the shim with the collar to avoid mis_ air pressure has been released or it may be placing it blown off with considerable force and cause in jury or damage j Pull the barrel assembly out of the nose gear brace assembly c If the leak seems to be coming from ...

Page 141: ...axle and in b Slip the snap ring adapter ring and scraper ring stalling the bracket washer and retaining nut over the top of the piston and work down the piston o Fill the dry strut with 475 cc or 16 fluid ounces of c Install the upper half of the torque knee on the barrel MIL H 5606 hydraulic fluid and install the O ring assemblY shim if one was originally installed plug and snap ring Tap the sna...

Page 142: ...brace Be sure that the air pressure is released prior d Slip the collar over the barrel and measure the to disconnecting the torque knee The torque amount of shim necessary Remove the colar insert knees provide the extension stop for the lower the shim and reinstall the collar and secure Safety the shock absorber cylinder assembly and when dis bolts connected the piston is free to slide out of the...

Page 143: ...BUSHING 16 BEARING 17 SCRAPER ADAPTER 18 SCRAPER 19 SNAP RING 20 PISTON 21 LOWER TORQUE KNEE 22 LOWER TORQUE KNEE PIN 7 23 PLUG 24 FORK ASSEMBLY 11 25 UPPER SHOCK ABSORBER BRACE BEARING 8 26 LOWER SHOCK ABSORBER 26 BRACE BEARING 10 9 13 27 LOWER TORQUE KNEE BUSHING 28 O RING 12 29 NOSE GEAR BRACE 1 ASSEMBLY 17 19 15 14 27 Figure 5 3 Nose Landing Gear Shock Strut Assembly Airplane Serial TD 403 and...

Page 144: ...mum 0 5005 in hardware Chrome plated portion of absorber f Disengage the rebound control assembly from the assembly piston 20 O D minimum 1 862 in piston assembly by holding the pin assembly head of the rebound control assembly with a long screwdriver in Upper 9 and lower 16 bearings serted through the top of the barrel assembly and re I D maximum 1 866 in moving the retaining nut Bushing 28 O D m...

Page 145: ...ead 13 13 Rebound control assembly pin 14 14 Felt lubricating liner 27 16 15 Upper torque knee bushings 17 16 Bearing 28 17 Scraper ring 18 Adapter ring 20 19 Snap ring 26 2 22 20 Piston 21 Lower torque knee bushings 23 22 Lower torque knee pin 24 25 23 Packing O ring c s 24 35 815081 washer 25 Pin retaining nut 26 Torque knees 27 Upper torque knee pin 28 Torque knee bushing Figure 5 4 Main Landin...

Page 146: ...pter and snap ring up the piston assembly and into the lower end of the barrel NOTE assembly If the strut has been properly refilled a little i Fit the two MS28782 24 plastic back up rings with fluid will escape through the air valve body If the AN6227 24 O ring between them in the groove no fluid escapes slowly actuate the strut sev at the bottom of the rebound control assembly Dip the eral times...

Page 147: ...dapter Ring 13 Snap Ring 17 21 g 14 Piston U 15 Upper Torque Knee 16 Upper Torque Knee Pin 17 Lower Torque Knee 18 18 Lower Torque Knee Pin 19 19 Axle Socket 22 20 Upper Torque Knee Bushing 23 21 Lower Torque Knee Bushing 22 Brazed Retaining Bolt 23 A de 2245 etr orque Knee Bushing Figure 5 5 Main Landing Gear Shock Strut Assembly Airplane Serial TD 252 thru TD 523 5 10 ...

Page 148: ...r Torque Knee Pin 12 Spacer 13 Piston 10 14 Upper Torque Kree 15 Center Torque Knee Bushing 16 Lower Torque Knee 11 17 Lower Torque Knee Bushing 14 12 18 Lcover Torque Knee Pin 15 19 A de Socket 13 20 Axle 16 21 Brazed Retaining Bolt ss 22 Gear Brace 23 Cross Arm 21 20 Figure 5 6 Main Landing Gear Shock Strut Assembly Airplane Serial TD 524 and after 5 11 ...

Page 149: ...the actuator drive shaft 7 are combined as one unit Upper and lower bearings 10 L D maximum 1 866 in a Remove the motor 1 from the actuator and remove Bushing 25 O D minimum 433 in the gear 2 from the face of the motor b Remove the snap ring 3 from the end of the shaft Bushing 25 L D maximum 315 in 19 and remove the gear 4 from the shaft When replacement of the scraper ring 11 and all O e Remove t...

Page 150: ...tor 4 11 Screw 3 12 Actuator Hand Crank 29 13 Spacer 2 14 O Ring Seal 15 Screw 1 16 Hand Crank Shaft Housing 17 Retainer Nut 18 Half ring 19 Worm Gear Shaft 26 Bearing 20 Bearing 27 Snap Ring 21 Lock Nut 28 Actuator Retract Arm 22 Seal 29 Bearing 23 Bearing 30 Grease Fill Plug 24 Bearing 31 Ball Check 25 Seal 32 Sector Gear Stop Assembly 28 27 9 Figure 5 7 Landing Gear Actuator 5 13 ...

Page 151: ...ne j Remove the snap ring 21 from the shaft 7 and slide NOTE the nose gear actuator retract arm 28 off the shaft k Remove the bearing 29 from the housing At assembly when installing the actuator drive shaft through the sector gear make sure the scribe marks on each piece match The same Clean all parts in solvent to remove the grease and oil applies when installing the nose gear actuator Check all ...

Page 152: ... piston slowly and push it out the lower floating piston with a threaded rod Pull down the open end of the piston rod and remove the O ring on the threaded rod and at the same time push down 14 on the upper piston so it will follow the column of fluid down in the piston rod and prevent the entry of air A h Remove the remaining compression spring 15 tool which will aid in compressing the spring and...

Page 153: ...ng 1500 reverse of the above stated procedure Lubricate all lbs pressure in the valve through the elbow 2 Remove parts with MIL H 5606 hydraulic fluid prior to assem the pressure and place it in the nozzl e 8 The valve bly should open with application of 2 lbs pressure or less If this is not the case the valve is not serviceable FLAP MOTOR GEARBOX OVERHAUL Figure 5 11 a Cut and remove all safety w...

Page 154: ...sher 4 Oil Seal Washer 16 Counter Shaft Bearing 5 Armature Shaft Washer 17 Bearing Cup 6 Motor Housing End Plate 18 Thrust Washer 7 Gear Housing Gasket 19 Worm Wheel Gear 8 Cover Plate 20 Flap Control Shaft 9 Sleeve Bearing 21 Spacer 18 10 Counter Shaft 22 Washer 11 Set Screw 23 Shim Washer 12 Washer 24 Retaining Pin Figure 5 11 Flap Motor Gearbox ...

Page 155: ...screw 4 from the nut assembly Lubricate the O rings with MIL L 6086 Grade M gear lube before inserting the piston in the housing c Drill out rivet 5 on later models remove shoulder pin 5 rivet 1 and remove actuator rod end 6 from the Pour MIL L 6086 Grade M gear lube into the piston until it screw 4 The bearing 7 and bushing can now be removed is about two inches from being full Slide a bearing on...

Page 156: ...djusting bushing 10 and check nut 9 If there is more than 025 inch end play measured from the screw 8 to the housing 6 f Check the end play between the actuator screw 4 and the acutator is not within tolerance If the end the actuator housing The end play must not exceed 0 005 play can not be reduced to 025 or less with the inch The nut 2 must be free to rotate and provide smooth adjusting bushing ...

Page 157: ...te all moving parts with MIL G 23827 Readjusting adjusting bushing 3 and check nut 2 may reduce the end play The nut must remain free to rotate and provide smooth a Install bearing 4 on the nut assembly 5 operation through its full travel b Install bushing 9 and bearing 4 on the actuator screw 8 TESTING FOR FUEL CELL LEAKS c Install the actuator screw 8 in the nut assembly 5 Although the chemical ...

Page 158: ...ested for leakage by sealing off all openings and inflating the empty d A regulator that can be set to provide U4 psi cell to 1 4 psi with a mixture of shop air and ammonia gas 6 inches of water from a supply of shop air then checking for visible indications of leakage on a cloth saturated with phenolphthalein solution To set up and e Two flasks or bottles approximately one conduct the leakage tes...

Page 159: ...or beakers fuel cell and manometer as indicated in Figure 5 15 d Reactivate these two surfaces by moistening them with a piece of cheesecloth dampened in methyl ethyl ketone 6 Inflate the fuel cell to 1 4 psi with a mixture of Place the patch on the damaged area when the surfaces are shop air and ammonium gas A 6 inch difference in the two tacky making contact first at the center of the patch Then...

Page 160: ...ea in accordance with the manufacturer s instructions Never working out all air bubbles and wrinkles If the cutout is use catalytic resin which has been exposed to air more than large enough to cause the patch to sag place a suitable thirty minutes If the repair is large prepare small amounts support coated with automobile wax or waxed paper behind of resin as required Make sure that your hands ar...

Page 161: ...have been noted by Electrical symbols used in diagrams appear on pages placing them in emphasized manner such as dotted 6 3 and 6 4 P52A4N Suffix Wire Size A W G Wire Segment Letter Wire Number Circuit Function Letters A list of circuit function designation follows A Armaments B Photographic C Control surfaces autopilot D Instruments other than flight or engine instrument ammeter landing gear posi...

Page 162: ...ar and Throttle Warning Instrument Lights 6 13 With Safety System Circuit 6 43 Landing Gear and Warning Horn 6 11 Light Circuits Oil Temperature 6 15 Cabin Lights 6 56 Pitot Heat 6 12 Instrument Lights 6 57 thru 6 58 Propeller Anti Icer 6 29 Landing Lights 6 55 Stall Warning 6 12 Navigation Lights 6 52 thru 6 53 Starter 6 7 thru 6 9 Nose Baggage Compartment Lights 6 54 Turn and Bank 6 12 Optional ...

Page 163: ...ar ious combinations on most of the fol lowing type switches and relays 2 Position 3 Position 2 Pole Pressure Switch MOTORS Low Current High Current 2 Wire 3 Wire CIRCUIT BREAKERS O SAO O SAO O SAO Push Pull Toggle Push to Reset TERMINAL BOARDS BUS BARS Terminal Board N Terminal Board with Bus Bar Open Bus Bar 6 3 ...

Page 164: ...re Connection Quick Disconnect A 8 U e Multiple Conductor Shielded Wire Twisted Wiring Cables Plug and Receptacle GROUND CONNECTORS LIGHTS Case Ground Ground Connection Connection c Press to Test Light Light MISCELLANEOUS Battery Capacitor Heating Element Thermocouple A Speaker or Ele trical Ins t 6 4 ...

Page 165: ...RH ENGINE LH ENGINE 1 Right Magneto 2 Filter Units 3 On Off Switches 4 Left Magneto 5 Right Magneto 6 Left Magneto IGNITION CIRCUIT TD 1 thru TD 173 and TD 185 except TD 127 6 5 ...

Page 166: ...J2 O O RH ENGINE o o LH ENGINE 1 Right Magneto 2 Filter Units 3 Off On Switches 4 Left Magneto 5 Right Magneto 6 Left Magneto 7 Bus Bar IGNITION CIRCUIT TD 174 thru TD 452 Except TD 185 and Ï D 444 6 6 ...

Page 167: ...6A P16 Ò 1 Main Bus Bar 6 Radio Bus Bar 2 External Power Receptacle Optional 7 Battery Master Relay 3 Starter RH Engine 8 Battery Master Switch 4 Starter Switch 9 Starter LH Engine 5 Starter Relays 10 Batteries BATTERY AND STARTER CIRCUIT TD 1 thru TD 185 except TD 127 6 7 ...

Page 168: ...P6 V REG P5 TO LH VREG Illb Qi 1 Main Bus Bar 7 Radio Bus Bar 2 Starter Switch RH Engine 8 Battery Master Relay 3 Starter Switch LH Engine 9 Starter LH Engine 4 External Power Receptacle Optional 10 Key Switch Assembly 5 Starter RH Engine 11 Batteries 6 Starter Relays BATTERY AND STARTER CIRCUIT TD 186 thru TD 452 except TD 444 6 8 ...

Page 169: ...ry Master Relay 3 L H Starter Magneto Switch 11 Batteries 4 Left Engine L H Magneto 12 Battery Master Switch 5 Left Engine R H Magneto 13 L H Starter 6 R H Starter Magneto Switch 14 L H Starter Relay 7 Right Engine L H Magneto 15 R H Starter Relay 8 Right Engine R H Magneto 16 R H Starter IGNITION BATTERY STARTER CIRCUITS TD 127 TD 444 TD 453 thru TD 533 6 9 ...

Page 170: ...t Breaker Switch Type 15 Amp 10 Circuit Breaker Switch Type 5 Amp 3 Landing Light RH 11 Rotating Beacon Light 4 Circuit Breaker Switch Type 15 Amp 12 Navigation Lights LH 5 Landing Light LH 13 Circuit Breaker Switch Type 5 Amp 6 Circuit Breaker Switch Type 5 Amp 14 Taxi Light Optional 7 Flasher 15 Landing Light Nose 8 Navigation Lights RH 16 Taxi Light Gear EXTERIOR LIGHTING CIRCUIT TD 1 thru TD 5...

Page 171: ...Connectors 2 Circuit Breaker 30 amp 12 Landing Gear Motor 3 Safety Switch 13 Circuit Breaker 5 amp 4 Up Limit and Up Indicator Switch 14 Down Limit and Down Indicator Switch 5 Heater Blower Switch 15 Warning Horn Switch 6 Circuit Breaker 5 amp 16 Throttle Warning Horn Switch RH Engine 7 Landing Gear Position Switch 17 Throttle Warning Horn Switch LH Engine 8 Up and Locked Indicator 18 Flasher 9 Do...

Page 172: ... Prior To Serial TD 403 Airplane Serial TD 403 and After F10 I 1 Main Bus Bar 2 Switch type Circuit Breaker 5 Amp 3 Pitot Heating Element 4 Circuit Breaker 5 Amp 5 Stall Warning Light 6 Stall Warning Detector Switch And Heater 7 Stall Warning Horn 8 Circuit Breaker 5 Amp 9 Turn And Bank Indicator TURN AND BANK STALL WARNING AND PITOT HEAT CIRCUIT TD 1 thru TD 533 6 12 Issued March 1969 ...

Page 173: ...tch Panel 6 Tachometer Lights RH Engine Lights RH 7 Tachometer Lights LH Engine 22 Tab Position Indicator Lights 8 Gyro Horizon Lights 23 Landing Gear Visual Indicator Light 9 Directional Gyro Lights 24 Instrument Light 10 Clock Lights 25 Circuit Breaker 10 Amp prior to TD 453 11 Suction Gage Light 3 Amp TD 453 thru TD 533 12 Radio Lights 26 On Off Switch 13 Engine Gage Cluster Lights 27 Cabin Lig...

Page 174: ... 2 3 D1A 1 NO D17 OFF COMM NC CS C7 D2 2 3 D1 UP 1 D16 Serials TD 3 through TD 52 1 Main bus bar 2 Circuit breaker 5 Amp prior to TD 303 and 15 Amp TD 303 and after 3 FLap position switch 4 Down limit switch 5 Connectors 6 Flap motor 7 Up limit switch 8 Flaps down indicator 9 Flaps up indicator FLAP CONTROL AND POSITION INDICATOR CIRCUIT TD 1 thru TD 533 6 14 ...

Page 175: ... C A GND C GND A 1 Main bus bar 2 Circuit breaker 5 amp 7 Circuit breaker 3 Right engine oil temperature gage 8 Right engine carburetor air temperature gage 4 Right engine oil temperature bulb 9 Right engine carburetor air temperature bulb 5 Left engine oil temperature gage 10 Left engine carburetor air temperature gage 6 Left engine oil temperature bulb 11 Left engine carburetor air temperature b...

Page 176: ... Generators 1 Main Bus Bar 7 LH Voltage Regulator 2 Ammeter RH Generator 8 On Off Switch 3 Circuit Breaker 30 Amp 9 LH Generator 4 RH Generator 10 Paralleling Relay 5 On Off Switch 11 Ammeter LH Generator 6 RH Voltage Regulator 12 Circuit Breaker 30 Amp GENERATOR CIRCUIT TD 1 thru TD 173 TD 185 TD 303 thru TD 533 6 16 ...

Page 177: ... Breakers For Optional 40 Amp Generators 1 Main Bus Bar 7 LH Generator 2 Ammeter RH Generator 8 Paralleling Relay 3 Circuit Breaker 30 Amp 9 Key Switch Assembly 4 RH Generator 10 Ammeter LH Generator 5 RH Voltage Regulator 11 Circuit Breaker 30 Amp 6 LH Voltage Regulator GENERATOR CIRCUIT TD 174 thru TD 302 except TD 185 6 17 ...

Page 178: ...ost Pump FUEL BOOST PUMP CIRCUIT TD 1 thru TD 533 RETRACT Kl2 KB EFXFTEND K10 Kl4 KSA EXTEND K11 A K9 RETRACT K13 1 Main Bus Bar 2 Circuit Breaker 5 Amp 3 Right Hand Cowl Flap Switch 4 Right Hand Cowl Flap Motor 5 Left Hand Cowl Flap Switch 6 Left Hand Cowl Flap Motor COWL FLAPS CIRCUIT TD 1 thru TD 173 and TD 185 6 18 ...

Page 179: ...TE K10 BLACK EFFECTIVE TD 223 THRU TD 533 9 1 Main Bus Bar 2 Circuit Breaker 5 Amp 3 Right Hand Cowl Flap Switch 4 Right Hand Cowl Flap Motor 5 Left Hand Cowl Flap Switch 6 Left Hand Cowl Flap Motor 7 Cowl Flap Position Indicator Lights COWL FLAPS CIRCUIT TD 174 thru TD 533 except TD 185 6 19 ...

Page 180: ... Transmitter 3 Fuel Quantity Indicator RH Tanks 4 Fuel Selector Switch 5 Right Auxiliary Fuel Tank Transmitter 6 Circuit Breaker 5 Amp 7 Fue1Quantity Indicator LH Tanks 8 Left Main Fuel Tank Transmitter 9 Left Auxiliary Fuel Tank Transmitter FUEL QUANTITY INDICATOR CIRCUIT TD 1 thru TD 142 6 20 ...

Page 181: ...er 3 Fuel Quantity Indicator RH Tanks 4 Fuel Selector Switch 5 Right Auxiliary Fuel Tank Transmitters 6 Circuit Breaker 5 Amp 7 Fuel Quantity Indicator LH Tanks 8 Left Main Fuel Tank Transmitter 9 Left Auxiliary Fuel Tank Transmitters 10 800 Ohm Resistors 11 Potentiometer FUEL QUANTITY INDICATOR CIRCUIT TD 143 thru TD 402 6 21 ...

Page 182: ...d Inboard Outboard Outboard 1 Main Bus Bar 6 Fuel Selector Switch 2 Circuit Breaker 5 Amp 7 Auxiliary Tank Transmitters LH 3 Resistor 25 ohm 10 watt 8 Main Tank Transmitter LH 4 Fuel Gage LH 9 Main Tank Transmitter RH 5 Fuel Gage RH 10 Auxiliary Tank Transmitters RH FUEL QUANTITY INDICATOR CIRCUIT TD 403 thru TD 452 6 22 ...

Page 183: ...1C I 2 Inboard Inboard Outboard Outboard 2 2 2 2 1 E66 1 1 E65 1 1 Main Bus Bar 7 Fuel Gage RH 2 Circuit Breaker 5 Amp 8 Fuel Selector Switch 3 Resistor 50 ohm 25 watt 9 Tank Transmitters LH 4 Resistor 25 ohm 10 watt 10 Main Tank Transmitters RH 5 Fuse 1 2 Amp 11 Main Tank Transmitters RH 6 Fuel Gage LH 12 Auxiliary Tank Transmitters RH FUEL QUANTITY INDICATOR CIRCUIT STANDARD 39 GALLON MAIN CELLS...

Page 184: ... Inboard Inboard Outboard _ _ Outboard 20 2 2 02 1 E66 1 1 E65 1 1 Main Bus Bar 7 Fuel Gage RH 2 Circuit Breaker 5 Amp 8 Fuel Selector Switch 3 Resistor 50 ohm 25 watt 9 Tank Transmitters LH 4 Resistor 25 ohm 10 watt 10 Main Tank Transmitters RH 5 Fuse 1 2 Amp 11 Main Tank Transmitters RH 6 Fuel Gage LH 12 Auxiliary Tank Transmitters RH FUEL QUANTITY INDICATOR CIRCUIT OPTIONAL 25 GALLON MAIN CELLS...

Page 185: ...3A18 E35 or E36A18 MAIN AUX E41A18 E43A18 or or E30A18 E36 E39A18 E35A18 E37 E26A18 or or or or S E71 E4 1 E 18 E E32 8 E72 E47 E46 Outboard of Inboard Inboard or Outboard E31A18 E27A18 25 Gal Main And 31 Gal Aux Tanks Optional 1 Main Bus Bar 6 Fuel Selector Switch 2 Circuit Breaker 5 Amp 7 Auxiliary Tank Transmitters LH 3 Resistor 50 ohm 25 watt 8 Main Tank Transmitters LH 4 Fuel Gage LH 9 Main T...

Page 186: ... Changeover Switch 2 Resistor 3 Ohm 10 Watt 9 Switch Type Circuit Breaker 20 Amp 3 300 F High Temperature 10 Air Valve Switch Control 11 Fuse 4 Heater Ductstat 12 Landing Gear Up Limit and Up Indicator 5 Heater Ignitor Switch 6 Heater Fuel Pump 13 Heater Blower Switch 7 Solenoid Valve 14 Heater Blower CABIN HEATER CDICUIT TD 1 thru TD 202 except TD 127 6 26 ...

Page 187: ...tallation on Airplanes Serial TD 453 thru TD 533 1 Main Bus Bar 9 300 F High Temperature Control 2 Switch type Circuit Breaker 10 Solenoid Valve 20 Amp 11 Heater Ductstat 3 Air Valve Switch 12 Heater Blower 4 Fuse 13 Heater Fuel Pump 5 Changeover Switch 14 Landing Gear Up Limit and 6 Heater Ignitor Up Indicator Switch 7 Heater Fuel Pump 15 Heater Blower Switch 8 Resistor 3 Ohm 10 Watt CABIN HEATER...

Page 188: ...AY 1 Main Bus Bar 8 Resistor 3 Ohm 10 Watt 2 Switch type Circuit Breaker 20 Amp 9 300 F High Temperature Control 3 Air Valve Switch 10 Solenoid Valve 4 Fuse 11 Heater Ductstat 5 Changeover Switch 12 Landing Gear Up Limit 6 Heater Ignitor and Up Indicator Switch 7 Heater Fuel Pump 13 Heater Switch CABIN HEATER CIRCUIT Standard TD 453 thru TD 533 6 28 ...

Page 189: ...8 D64 18 D63 18 D65 18 1 Bus Bar 2 Circuit Breaker 5 Amp 3 Anti icer Pump 4 Circuit Breaker 5 Amp 5 Resistor 75 ohm 10 watt 6 Quantity Gage 7 Potentiometer 8 Transmitter Propeller Anti icer Circuit TD 453 thru TD 533 6 29 ...

Page 190: ... P23A18NN C P150A18 BATTERY CIRCUIT WITH OPTIONAL ALTERNATOR TD 578 thru TD 604 except TD 602 RADIO P25B2 P26A2 C P21A10 I P24A20 TO NOSE BAGGAGE TO P25A18 COMPARTMENT STARTER P21B2 P25A18 LIGHT P 58A 18 Ë RELAY PS7A18 YELLOW El RED P22A18 P27A2N 1 Bus Bar P60A18 2 Battery Master Relay 3 Battery Master Switch 4 Batteries two 12 volt Standard P23A18N Standard one 24 Volt Optional PS6A18 5 Klipvolt ...

Page 191: ...4A20 LR LH J5A20 R os SW 80 y J9A18N K13A18 1 Bus Bar 2 Ignition Vibrator J2B18 J1C18 3 Left Magneto 4 Right Magneto 5 Ignition Starter Switch I AL 6 Starter Relay SW 3 J6A20 i L GND 7 Starter RET 3 J7A20 LR 8 External Power Relay RH J8A20 R 9 External Power Receptacle s J9B18N 10 Diode SW 80 11 Circuit Breaker 5A BATO K 14A 18 T IGNITION AND STARTER CTRCUIT TD 534 and after 6 31 ...

Page 192: ...P348 B P19A16 P9A16 P20A8 P10A8 Gc 30 P14A16 SC P4a16 P18A8 PBA8 P15A16 1 Bus Bar P5A16 2 Ammeter 3 Circuit Breaker 30A rN 4 Voltage Regulator i 5 Generator Switch L Gea alraelirg Relay R GENERATOR CIRCUIT TD 534 and after 6 32 ...

Page 193: ...8N BRAELAERY P31B18 P39A18 RED P P30B18 P23A18N P35A18N BLACK G P55A18N P34A18 P33A10 P38A18 P37A18 BLUE F P34B18 RED P PDGA18 H 22221 P 2A13N DLA K G P54A18N 1 Circuit Breaker 50A 2 Ammeter 8 Condensor 3 Alternator 9 Circuit Breaker 10A 4 Fuse 2A 10 Overvoltage Warning Light 5 Switch 11 Overvoltage Relay 6 Battery Master Switch 12 Voltage Regulator 7 Regulator Selector Switch 13 Relay ALTERNATOR ...

Page 194: ...3B18 1 RED P B ra4xis PL5A18N M 9 BLUE F P37A18 IH 22422 P32A13N O ELACK GND P54A18N P31A18 P30A10 P56A18 P39A18 IH P30B18 RED P P38A18 ry BLUE F L I IH saisis P35A101I PS5A18N O DLACK GND 1 Circuit Breaker 50A 7 Regulator Selector Switch 2 Ammeter 8 Condensor 3 Alternator 9 Circuit Breaker 10A 4 Fuse 2A 10 Overvoltage Warning Light 5 Alternator Switch 11 Overvoltage Relay 6 Battery Master Switch ...

Page 195: ...A18 E32A18 E42A18 I 2 2 1 E43A18 E 1 2 241 E31A18 JUMPER WIRE IS NOT USED ON ALL AIRCRAFT E27A18 E3 B18 E27 8 1 Bus Bar 2 Circuit Breaker SA 3 Resistor 4 Fuel Gage 5 Fuel Gage Transfer Switch 6 Main Tank 25 gallon 7 Aux Inboard Transmitter 8 Aux Outboard Transmitter FUEL QUANTITY INDICATOR CIRCUIT OPTIONAL TD 534 and after 6 37 ...

Page 196: ...rd Fuel Transmitter TO 6 Outboard Fuel Transmitter ANTI ICE INDICATOR 50 0 50 0 25W 25W E29A18 E25A18 28 E42A18 E43A18 1 E32A18 E41A18 N B 1 1 2 2 E31A18 E27A18 E31B18 3 E27B18 JUMPER WIRE IS NOT USED ON ALL AIRCRAFT FUEL QUANTITY INDICATOR CIRCUIT STANDARD TD 534 and after 6 38 ...

Page 197: ...IONAL WITH SURFACE DEICER MSA18N W4A18 L 1 Bus Bar 2 Circuit Breaker SA 3 Stall Warning Detector Switch and Heater 4 Stall Warning Horn 5 Pressure Switch 6 Engine Hour Meter STALL WARNING AND ENGINE HOUR METER CIRCUIT OPTIONAL TD 534 and after a F3A18 F4A18N 1 Bus Bar 2 Circuit Breaker SA 3 Indicator T URN AND S LIP TD 534 and after Issued March 1969 6 39 ...

Page 198: ...A18F D E4EA1P I E6A18N OIL TTMPERATURE CIRCUIT TD 534 and after LH H 1 L H Cylinder Head Thermocouple Bulb 2 Cylinder Head Temperature Gage 3 R H Cylinder Head Thermocouple Bulb H RH CYLINDER HEAD TEMPERATURE CIRCUIT TD 534 and after 1 Bus Bar Q1A18 2 Circuit Breaker 5A 3 Fuel Boost Pumps Q2A18 RH LH FUEL BOOST PUMPS TD 534 and after 6 40 ...

Page 199: ...or 14 L G Safety Switch Gi A18 G14A18 15 Flight Hour Meter Gl4B18 3 3 I DN UP 281 G13B18N 1 G9A18 G21A13 G13A18N G12A18 1 G2A18 G8A18 G4E20 D6A G1EA10 G4A20N G9A18 TD 659 Amy D7 THRU TD 707 mm G20A18 TO R ND HEATER NC DN G6B18 GB BLOWER L SWITCH G6A18 L R G7B18 G3A18 DNNC O G21A18 I M1A18 G3A18 G8A18 1000 G10A 18 G7B18 19W Ë G7A18 C2 3 C1 CD G11A18 2 1 G4A18N G16A10 Gl7A10N Gl8A10 G 19A 10 21 RED ...

Page 200: ...18 M1A18 C2 3 C1 2 C 0 1 Gl1A18 G18A10 G16A10 G17A10N Gl9A10 21 R ED WHITE 1 Bus Bar 9 L G Motor 2 Circuit Breaker 30A 10 L G Up Limit Switch 3 Circuit Breaker SA 11 L G Warning Horn Flasher 4 L G Indicator Light 12 L G Warning Horn 5 L G Control Switch 13 Resistor 6 L G Dn Limit Switch 14 L G Safety Switch 7 Throttle Warning Switch 15 Flight Hour Meter 8 L G Dynamic Brake Relay LANDING GEAR AND T...

Page 201: ... L BLACK 18 R RED 18 K5A18 K11A18 OR OR L RED 18 R BLACK 18 1 Bus Bar 2 Circuit Breaker 5A 3 Cowl Flap Indicator RED 4 Cowl Flap Switch RED 5 Cowl Flap Actuator C BLACK W ITE W TE K20A18N K19A18N OR OR WHITE 18 WHITE 18 L H R H COWL FLAP CIRCUIT TD 534 and after 6 45 ...

Page 202: ...tor E13818 5 Calibrating Rheostat 6 Anti ice Transmitter E13A18 10W FUEL QUANTITY INDICATOR E7 1A 18 E21A18 ANTI ICER CIRCUIT TD 534 and after 1 Bus Bar 2 Circuit Breaker 5A 3 Propeller Anti ice Pump H3A18 PROP ANTI ICE PUM P CIRCUIT OPTIONAL TD 534 and after 6 46 ...

Page 203: ... 3 Switch 4 Relay 5 Time Delay Relay 6 Deicer Valve II30A20 DEICER CIRCUIT OPTIONAL TD 534 thru TD 707 8 H33A22N C P52A20 H25B20 H30E20 AFT H25C20 H30D20 H28B20 H28A20 4 5 3 H29A20N 6 H26A20 _ g AUTOMATIC I 2 7 1 H25A20 H27A20N C OFF H26B20 1 Bus Bar 2 Circuit Breaker 5A 3 Switch MANUAL 4 Relay 5 Time Delay Relay 6 Deicer Valve H30A20 DEICER CIRCUIT OPTIONAL TD 708 and after 6 47 ...

Page 204: ...2 Circuit Breaker 3 Resistor 4 Cigarette Lighter CIGARETTE LIGHTER CIRCUIT TD 534 and after 10A F 1A18 1 Bus Bar F1A18 2 Circuit Breaker 10A 3 Pitot Heat 4 Stall Warning Heater i l V F2A18N F2A18N OPTIONAL WITH SURFACE DEICER L H R H STANDARD OPTIONAL PITOT HEAT AND STALL WARNING HEATER CIRCUIT TD 534 and after 6 48 Issued March 1969 ...

Page 205: ... TD 534 thru TD 637 C H36A14 H6A14 NOTE CIRCUIT IS SHOWN H6A14 WITH AIRCRAFT ON GROUND H20A20 H1145 H13A20 H7Al H8HA114N2 H9A20 1 Bus Bar 2 Circuit Breaker 20A 3 Air Valve Switch B C H17A20 4 Heater Blower Switch 5 Fuse 5A H14A20 7 r Irgnitor H18A20 8 Overtemp Thermostat 9 Duct Stat Heat Control 10 Heater Fuel Pump H10A20N 11 Heater Fuel Solenoid Valve 12 Up Limit Switch 13 Heater Blower H19A20 HE...

Page 206: ...4 j H11A14 H13A20 H15A20 H15A20 H7A18 H9A20 H15B20 H8A14N A BC H33A20N 1 Bus Bar H14A20N 2 Circuit Breaker 20A I 3 Air Valve Switch B C 4 Heater Blower Switch H14A H17A20 OPTIONAL FOR USE 5 Fuse SA WITH ARC RT302A 6 Resistor 317A 1 DUAL 318S 7 Heater Ignitor H18A20 AND KING KA 11 8 Overtemp Thermostat RADIOS 9 Ductstat Heat Control H10A20N 10 Heater Fuel Pump 11 Heater Fuel Solenoid Valve 12 Up Li...

Page 207: ...A20 H8A14N B f E 1 Bus Bar H16B20 2 Circuit Breaker 20A T 3 Air Valve Switch 4 Heater Blower Switch B C 5 Fuse 5A H17A20 6 Resistor H14A20 7 Heater Ignitor 8 Overtemp Thermostat H18A20 9 Ductstat Heat Control 10 Heater Fuel Pump H10A20N 11 Heater Fuel Solenoid Valve 12 Up Limit Switch 13 Heater Blower H19A20 14 Heater Blower Select Switch NOTE CIRCUIT IS SHOWN WITH 15 Heater Igmtor Switch AIRCRAFT...

Page 208: ... L 13F 18 L15A 8N CONNECTED AS SHOWN BY DOTTED LINE WHEN FLASHER IS NOT USED 1 Bus Bar 2 Circuit Breaker 5A 3 Navigation Lights Flasher Optional 4 Left Wing Tip Lights 5 Right Wing Tip Lights 6 Tail Light NAVIGATION LIGHTS CIRCUIT TD 534 thru TD 707 6 52 ...

Page 209: ...18 LH L17CC20 L36 20N CONNECTED AS SHOWN BY DOTTED L36A20N LINE WHEN FLASHER IS NOT USED 1 Bus Bar 2 Circuit Breaker SA 3 Navigation Lights Flasher 4 Left Wing Tip Lights 5 Right Wing Tip Lights 6 Tail Light NAVIGATION LIGHTS CIRCUIT TD 708 and after 6 53 ...

Page 210: ...it Breaker 10A 3 Rotating Beacon L7A18 L9Alb L8A18N L10A18N O O ROTATING BEACON CIRCUIT TD 534 and after NO BOATTERY P24A20 RELAY C NC BLACK 1 Switch 2 Light NOSE BAGGAGE COMPARTMENT LIGHT CIRCUIT TD 708 and after 6 54 ...

Page 211: ... Landing Light L6A18N L4A18N STANDARD OP TIONAL NOSE CONE NOSE GEAR LANDING LIGHTS CIRCUIT TD 534 and after 1 Bus Bar 2 Circuit Breaker 5A 3 Wing Ice Light L31A18 L32A18 LH RH O O O O D B B D C C L33A18 L34A18N WING ICE LIGHTS CIRCUIT OPTIONAL TD 534 and after 6 55 ...

Page 212: ...637 8 L21A18 L21B18 L21C18 1 Bus Bar 2 Circuit Breaker 5A 3 Cabin Light Switch 4 Cabin Lights L42A18 L41A18N L40A18N g e e E e L20A18N L20D18N L20E18N TO L20C18N OVERHEAD OPTIONAL L20B18N INSTRUMENT LIGHTS CABIN LIGHTS CIRCUIT OVERHEAD AND VENT TD 638 and after 6 56 ...

Page 213: ...28E18 L28D18 1 Bus Bar WIRE L22A18 IS CONNECTED TO CABIN LIGHTS 2 Circuit Breaker SA CIRCUIT BREAKER WHEN OPTIONAL LIGHTS ARE 3 Rheostat INSTALLED 4 Landing Gear Visual Indicator Light 5 Rheostat Light 6 Trim Tab Indicator Light CONNECT WITH POST LIGHTS ON OPTIONAL 7 Fuel Selector Panel Lights INSTALLATION 8 Circuit Breaker And Switch Panel Lights 9 Compass Light 10 Overhead Lights 11 Instrument L...

Page 214: ...B18 C B W B W L29Q18 L23C18 r B W I Œ 8 W C I B W I C L20G13N L29R18 L23D18 1 Bus Bar 8 W 2 Circuit Breaker 5A C 3 Rheostat 4 Landing Gear Visual Indicator Light 5 Rheostat Light 6 Trim Tab Indicator Light C I 8 W 7 Fuel Selector Panel Lights 8 Switch Panel Light Assembly 9 Compass Light L20B18N 10 Instrument Lights 11 Glareshield 12 O A T Light L20F18N I 13 Switch INSTRUMENT LIGHTS CIRCUIT TD 708...

Page 215: ...ZON PRESSURE R ANTI ICE L29S18 R HOUR METER SUCTION A D F GAGE R R R R I SCSEURE 2nd ALTIMETER OR AIRSPEED L29K18 L29L18 L29M18 L29N18 L29P18 L29Q18 L29R18 L29S18 COMPASS RgRRgRR RR RR RRgRR R TURN DIRECTION RATE OF OMNI OMNI RH ENGINE LH ENGINE BANK GYRO CLIMB GAGE GAGE 1 Bus Bar 2 Circuit Breaker 5A 3 Rheostat 4 Instrument Lights 5 Compass Light OPTIONAL INSTRUMENT LIGHTS CIRCUIT TD 534 thru TD ...

Page 216: ...CHOMETER PRESSURE ANTI ICE 8 W L29S18 A F SUCTION W HOUR METER GAGE E DE ICE 8 W W PRESSURE W 777 777 777 2nd ALTIMETER OR AIRSPEED L29K18 L29L18 L29M18 L29N18 L29P18 L29Q18 L29R18 L29S18 COMPASS Iw w w Zw w I Iw w Iw Iw w Iw lw ey TURN DIRECTION RATE OF OMNI OMNI RH ENGINE LH ENCINE BANK GYRO CLIMB GAGE GAGE 1 Bus Bar 2 Circuit Breaker 5A 3 Rheostat 4 Instrument Lights 5 Compass Light OPTIONAL IN...

Page 217: ...n MUST be accomplished within each 12 month period for compliance with the Federal Aviation Regulations To the extent that the airplane is operated in excess of 100 hours per year Beech Aircraft Corporation strongly recommends that the airplane be inspected at 100 hour intervals rather than annually The 100 hour interval between performance of the procedures specified herein should NEVER be exceed...

Page 218: ... and wiring 19 Flaps I1 Instrument filters 20 Pitot heat 12 Engine controls 21 Stall warning 13 Windows and cabin door 22 Power check 14 Seat belts and seats 23 Induction heat 15 Electrical wiring and equipment 24 Gyros 16 Emergency exit hatch Inspect the emergency exit hatch seal and latching mechanism for condition security of attachment and proper operation POWER PLANT NOSE SECTION l Service oi...

Page 219: ... 1 Brake lining and dises 1 Doors 2 Wheels and tires 2 Visual indicator 3 Landing gear strut 3 Nose gear up tension 4 Gear doors and linkage 4 Assist step when installed 5 Retract mechanism 5 Downlock tension 6 Strut fluid level NOSE GEAR GENERAL 1 Wheel and tire 2 Landing gear strut 1 Aircraft cleaned and serviced 3 Retract rod ends 2 Aircraft lubricated First 100 hours and every 200 hours therea...

Page 220: ...periods do not constitute a guarantee that the item will reach the period The time periods for inspection noted in this handbook are without malfunction as the aforementioned based on average usage and average environmental factors cannot be controlled by the conditions manufacturer SPECIAL CONDITIONS CAUTIONARY NOTICE NOTE Airplanes operated for Air Taxi or other than normal On Condition items ar...

Page 221: ...alve assembly On condition Parking brake valve On condition All hose On condition POWER PLANT I Engine 2000 0 360 Engine l400 10 360 Engine Engine controls On condition Exhaust system On condition Starter Inspect at engine overhaul and overhaul or replace on condition Generator or alternator On condition I Oil cooler Engine overhaul Propeller 1200 hours Propeller governor 1200 hours or at engine c...

Page 222: ...haft Every 2000 hours FUELSYSTEM Fuel cells On condition Fuel quantity transmitter On condition Fuel drain valve On condition Fuel system check valves On condition Fuel selector valve Inspect every 600 hours Overhaul every 1200 hours Fuel boost pump Overhaul 1200 hours All hose On condition INSTRUMENTS Turn and slip indicator On condition Altimeter Every 24 months per FAA Directive Directional gyr...

Page 223: ...ic brake relay On condition Battery master relay On condition Paralleling relay On condition All other relays On condition Voltage regulator On condition Heater vibrator points Every 2000 hours of heater operation Starter Inspect at engine overhaul and overhaul or replace on condition Starter relay On condition Generator or alternator On condition UTILITYSYSTEM Cabin heater Overhaul every 500 hour...

Page 224: ...Oxygen regulator Every 2000 hours or 48 months Oxygen cylinder Hydrostatically test every 5 years no replacement duration ICC Regulation Oxygen cylinder lightweight Hydrostatically test every 3 years replace every 24 years or 4 380 refills ICC Regulation All hose On condition MISCELLANEOUS Wing Bolts Replace 10 Years After Initial Inspection or On Condition See Section 4 C4 8 5 ...

Page 225: ...witch Gear Safety System G9A18 19 R H Throttle Switch Gear Safety System 20 Test Switch Gear Safety System DN G27A18 21 Pressure Switch 70 MPH GEA13 e o Gl4B18 G23A18 010A10 GIB20 G20A18 N 2 N a GK R2 4 6 1 3C 2 1 TEST 4 ON OFF Gl0A18 GllA18 Gl2A18 Gl3B18N G27A18 05 2 Gl3A18N c2 3 c1 G28A18 2 e o G21A10 G21A1 Gl7A Gl8A10 Gl6A10 Gl9A10 M1A18 C G26A15 G24A18 OR OR OR G25A18 RED BLACK WHITE G7B18 G3A...

Page 226: ...r 7 Up Position Light 8 Down Position Light C6A14N FLAP CBCUIT TD 534 thru TD 667 TO INSTRUMENT LIGHTS 1 2 CIRCUIT o o BREAKER T T C1A14 C12B20 C11B20 C10A18 UP DOWN 0 C C13A20N RED WHITE BLUE C7A14 C2A14 4321 NC NC U R NO A NO CBA14 C5A14 1 Bus Bar 2 Circuit Breaker 15A 3 Flap Position Switch 4 Up Limit Switch 5 Down Limit Switch 6 Flap Motor C6A14N 7 Position Indicator 8 Printed Circuit Board 9 ...

Page 227: ... P44A8N P43A18 P44A18 P37A14 A PSSB18N PT8B18 P78C18 P78D18 F P56A18 L L O P41A18 rs n P39A18 8 Y T I P38B18N C P39A18 P40B18 P36A18 D 1 Dus Bar 7 Fuse E 2 Circuit Breaker SOA 8 Alternator Switch 3 Circuit Breaker 10A 9 Master Battery Switch i 4 Ammeter 10 Regulator Select Switch P85A18 5 Alternator 11 Overvoltage Warning Light G 6 Capacitor 12 Voltage Regulator Overvoltage Relay o ALTERNATOR CIRC...

Page 228: ...16CIS P78D18 P46B18N R H P39A1P3 1 BLACK L BMCK BLACK L BL CK P46A 8N P85A18 P36A18 1 Sus Bar P50B18 2 Circuit Breaker SOA 3 Circuit Breaker 10A 4 Ammeter P36B18 5 Alternator 6 Capacitor P45B18N I L H 7 Fuse SA 8 Alternator Out Relay 9 Alternator Switch PS3B18N PS3A18N 10 Battery Master Switch P45A18N 11 Regulator Selector Switch 12 Alternator Out Light 13 Alternator Out Light Test Switch 14 Volta...

Page 229: ...ve the safety wire and the vibrator retain 1 Disassemble the spray nozzle by unscrewing ing ring 1 the fuel strainer and two piece core from the nozzle body b Remove the vibrator 2 and radio noise shield 3 2 Clean the parts in Stoddard solvent NOTE 3 If soaking fails to thoroughly clean the parts scrub them with a soft non metallic brush Be careful that O ring packing 5 does not drop out of place ...

Page 230: ...S o dn I amd Assy Airplane Serials TD 453 and after Airplane Serials TD 638 and after 18 Combustion Air Intake Duct 19 Iris Valve 20 Intake Blower Assembly 21 Heater Safety Switch 22 Igmt1on Assembly 23 Heater Duct Thermostat 24 Overheat Fuse 25 Heater Resistor 26 Copilots Outlet 27 Cabm Heat Circuit Breaker Airplane Serials TD 453 and after 28 Rear Seat Outlet IGNITOR 29 Cop11ots Outlet Control 3...

Page 231: ... S 112 000 B LEFTWING DOWN BALANCE CABLE RIGHT WING DOWN F S 68 00 NOTE RIG AUTOPILOT SERVO CABLES AFTER RIGGING BASIC CABLES LEFTWING DOWN SURFACE TRAVEL W S 23 881 AILERON AILERON TAD 20 1 Above 10 1 Above 20 1 Below 10 1 Below RIGHT WING DOWN aa W S 34 375 DETAIL A FWD E W S 45 000 WS 66 000 W S 94 I I W S 108 281 3 40 50 60 70 80 90 100 110 Figure 3 5 Rigging the Alleron Control System TEMPERA...

Page 232: ...ching the right actuator to the aileron and wing tip With the bellcrank parallel to thewing rib right flap set the aileron in neutral by adjusting the length of the push pull tube Loosen the locknuts on both ends and turnthe tube d Turn the jackscrew on the right actuator in or out to to shorten or lengthen align the right flap with the left Tighten securely the locknuts on all rod ends Rig cables...

Page 233: ...ELEVATOR ELEVATOR TP wn or ELEV DOWN oow FWDI F S 233 50 NOSE UP NOSE DOWN DETAIL D F S 117 105 ELevAToR DOWN SPRING INSTALLATION PRIOR TO AIRPLANE SERIAL TD 303 te F S 112 000 era 6 ELEVATOR NEUTRAL POSITION 2 50 09 WCHES T D 303 THRU T D 351 sperryS 2 77 06 INCHES TD 380 THRU TD 410 DO NOT USE RIG PIN ABOVE SERIALS ONLY DETAILB ELEVATOR DOWN SPRING INSTALLATION 33 40 50 60 70 80 90 100 110 TD 30...

Page 234: ...DER TAB RIGHT DETAIL D RRUUDD GHT F 5 233 50 NOTE RIG AUTOPILOT SERVO CABLES AFTER RIGGING BASIC CABLES DETAIL A SURFACE TRAVEL RUDDER RUDDER TAL Prior to TD 303 25 1 L R 30 1 L R 40 TD 303 After 30 1 L 34 1 R RUD TAB RIGHT RUD TAB RIGHT RUD TAB LEFT F 5 117 185 RUD TAB LEFT RUDDER RIGHT FWDi RUDDER LEFT DETAIL B F 5 112 00 to _ pa sper 0 33 40 50 60 70 80 90 100 110 Figure 3 2 Rigging the Rudder ...

Page 235: ...DETAIL A DETAIL B DETAIL D DETAIL G Effective TD 534 and after DETAIL Q DETAIL H DETAIL C DETAIL F DETAIL I OPN ME L K DETAIL O DEDTAIL DETAIL E Figure 2 5 Lubrication Diagram 2 8 ...

Page 236: ... 6 MIL G 7711 100 hrs 1 Main gear door hinges 10 SAE 20 100 hrs DETAIL P DETAIL F 1 Nose steering mechanism 5 MIL G 7711 100 hrs 1 Optional utility baggage door SAE 20 100 hrs DETAIL Q latch mechanism 3 1 Heater iris valve 1 MIL M 7866 AR DETAIL G 1 Rudder trim tab actuator 1 MIL G 23827 AR NOTES 2 Rudder trim tab hinge 1 MIL G 6711 100 hrs Precaution should be taken wher using MIL G 23827 and MIL...

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