Cessna 150 1974 Owner'S Manual Download

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Summary of Contents for 150 1974

Page 1: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 2: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 3: ...the industry Specific benefits and provisions of the warranty plus other important benefits for you are contained in your Customer Care Prograni book supplied with your aircraft Warranty service is available to you at any authorized Cessna Dealer throughout the world upon presentation of your Customer Care Card which establishes your eligibility under the warranty FACTORY TRAINED PERSONNEL to prov...

Page 4: ...ted and optional flashing beacon installed Maximum wing span if optional conical camber wing tips and optional strobe lights are installed If standard wing tips without strobe lights are installed wing span is 32 81 2 PRINCIPAL DIMENSIONS 0 r 3 3 _ 4 F o r T r a i n i n g P u r p o s e s O n l y ...

Page 5: ... ________ 5 1 SECTION VI OPERATIONAL DATA ______________ 6 1 SECTION VII OPTIONAL SYSTEMS______________ 7 1 This manual describes the operation and performance of the Model 150 the Trainer and the Commuter Equipment described as Optional denotes that the subject equipment is optional on the Model 150 Much of this equipment is stand ard on the Trainer and Commuter iii F o r T r a i n i n g P u r p ...

Page 6: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 7: ...eviated check list covering the Before Take Off and Before Landing phases of aircraft operation is provided on a plastic card and normally stowed in the map compartment This abbreviated check list is a convenient reference of key items to be rechecked immediately prior to taxiing into position for take off and before entering the final approach for landing The flight and operational characteristic...

Page 8: ... ice or snow from wing tail and control surfaces Also make sure that control surfaces contain no internal accumulations of ice or debris If night flight is planned check operation of all lights and make sure a flashlight is available Remove control wheel lock Check ignition switch OFF 11 Turn on master switch and check fuel quantity indicators then turn master switch OFF 11 Check fuel shutoff valv...

Page 9: ...check the system may contain additional water and the wing tank sump drain plugs and fuel line drain plug should be removed to check for the presence of water Check propeller and spinner for nicks and security Check carburetor air filter for restrictions by dust or other foreign matter Check landing light for condition and cleanliness Check nose wheel strut and tire for proper inflation Disconnect...

Page 10: ...AKE OFF 1 Cabin Doors Latched 2 Flight Controls Check for free and correct movement 3 Elevator Trim Control Wheel TAKE OFF1 setting 4 Throttle Setting 1700 RP M 5 Engine Instruments Within green arc 6 Suction Gage Check in green arc 4 6 to 5 4 inches of mercury 7 Magnetos Check RPM drop should not exceed 150 RPM on either magneto or 75 RPM differential between magnetos 8 Carburetor Heat Check oper...

Page 11: ...a maximum performance climb is necessary use speeds shown in the Maximum Rate Of Climb Data Chart in Section VI 2 Throttle Full OPEN 3 Mixture Rich unless engine is rough CRUISING 1 Power 2000 to 2750 RPM 2 Elevator Trim Control Wheel Adjust 3 Mixture Lean to maximum RPM BEFORE LANDING 1 Mixture Rich 2 Carburetor Heat Apply full heat before closing throttle 3 Airspeed 70 to 80 MPH flaps up 4 Wing ...

Page 12: ...NDING 1 Touchdown Main wheels first 2 Landing Roll Lower nose wheel gently 3 Braking Minimum required AFTER LANDING 1 Wing Flaps Up 2 Carburetor Heat Cold SECURING AIRCRAFT 1 6 1 Parking Brake Set 2 Radios and Electrical Equipment OFF 3 Mixture Idle cut off pulled full out 4 Ignition and Master Switches OFF 5 Control Lock Installed F o r T r a i n i n g P u r p o s e s O n l y ...

Page 13: ...1 7 F o r T r a i n i n g P u r p o s e s O n l y ...

Page 14: ...l Radios Opt 14 Tachometer 15 Optional Instrument Space 16 Fuel and Oil Gages 17 Suction Gage Opt 18 Ammeter 19 Over Voltage Warning Light 20 Map Compartment 21 Cabin Air Heat Control Knobs 22 Wing Flap Switch Figure 2 1 23 Cigar Lighter Opt 24 Mixture Control Knob 25 Throttle With Friction Lock 26 Microphone Opt 27 Elevator Trim Control Wheel 28 Carburetor Heat Control Knob 29 Electrical Switches...

Page 15: ...ach wing From these tanks fuel flows by gravity through a fuel shutoff valve and fuel strainer to the carburetor Refer to figure 2 2 for fuel quantity data For fuel system servicing information refer to Servicing Requirements on the inside back cover LONG RANGE FUEL TANKS Special wings with long range fuel tanks are available to replace the FUEL QUANTITY DATA U S GALLONS USABLE FUEL UNUSABLE TOTAL...

Page 16: ... the tanks should be re topped after each refueling to assure maximum capacity rFu I 22 5 GALS I i ON c ID I I L CODE ENGINE PRIMER FUEL SUPPLY c J VENT MECHANICAL LINKAGE CARBURETOR TO ENGINE CYLINDERS Figure 2 3 RIGHT FUEL TANK THROTTLE MIXTURE CONTROL KNOB F o r T r a i n i n g P u r p o s e s O n l y ...

Page 17: ...he master switch should be used simulta neously however the BAT side of the switch could be turned ON separately to check equipment while on the ground The ALT side of the switch when placed in the OFF position removes the alternator from the electrical system With this switch in the OFF position the entire electrical load is placed on the battery Continued operation with the alternator switch OFF...

Page 18: ... TO IGNITION STARTER SWITCH TO WING FLAP SYSTEM TO LANDING LIGHT OPT TO WING TIP STROBE LIGHTS OPT TO FLASHING BEACON OPT TO PITOT HEAT SYSTEM OPT TO NAVIGATION LIGHTS AND OPTIONAL CONTROL WHEEL MAP LIGHT TO TRANSMITTER RELAY TO DOME LIGHT TO RADIO OPT TO RADIO OPT TO OPTIONAL TURN COORDINATOR OR OPTIONAL TURN AND BANK INDICATOR TO INSTRUMENT AND COMPASS LIGHTS TO FUEL QUANTITY INDICATORS F o r T ...

Page 19: ... master switch and leaving the BAT portion turned on FUSES AND CIRCUIT BREAKERS Fuses on the left lower portion of the instrument panel protect the majority of electrical circuits in the airplane Labeling below each fuse retainer indicates the circuits protected by the fuses Fuse capacity is shown on each fuse retainer cap Fuses are removed by pressing the fuse retainers inward and rotating them c...

Page 20: ...e Do not turn on any of the lights protected by the fuse until the malfunction has been corrected LIGHTING EQUIPMENT EXTERIOR LIGHTING Conventional navigation lights are located on the wing tips and top of the rudder Optional lighting includes a single landing light or dual land ing taxi lights in the cowl nose cap a flashing beacon on the top of the vertical fin and a strobe light on each wing ti...

Page 21: ...beled WING FLAPS on the lower center portion of the instrument panel Flap posi tion is mr chanically indicated by a pointer housed in the left front door post To extend the wing flaps the flap switch must be depressed and held in the DOWN position until the desired degree of extension is reached Releasing the switch allows it to return to the center off position Normal full flap extension in fligh...

Page 22: ... adjustable pilot and front passenger seats with two position reclining backs By raising a lever at the front of the seat on the inboard side the seat can be adjusted fore and aft A control knob near the center of the front edge of the seat is used to adjust the reclining angle of the seat back To recline the back pull the knob forward firmly and lean back against the seat The control will remain ...

Page 23: ...t first and then pulling the harness over the head by pulling up on the release strap STARTING ENGINE Ordinarily the engine starts easily with one or two strokes of primer in warm temperatures to six strokes in cold weather with the throttle open approximately 1 4 inch In extremely cold temperatures it may be necessary to continue priming while cranking Weak intermittent firing followed by puffs o...

Page 24: ...onducted during ta d and addi tional warm up before take off should be restricted to the checks out lined in Section I Since the engine is closely cowled for efficient in flight cooling precautions should be taken to avoid overheating on the ground MAGNETO CHECK The magneto check should be made at 1700 RPM as follows Move ignition switch first to R position and note RPM Next move switch back to BO...

Page 25: ...artering tail winds require caution Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude Use the steerable nose wheel and rudder to maintain direction Figure 2 5 2 11 F o r T r a i n i n g P u r p o s e s O n l y ...

Page 26: ...unups over loose gravel are especially harmful to pro peller tips When take offs must be made over a gravel surface it is very important that the throttle be advanced slowly This allowsthe air plane to start rolling before high RPM is developed and the gravel will be blown back of the propeller rather than pulled int o it When unavoid able small dents appear in the propeller blades they should be ...

Page 27: ...th to minimize the drift angle immediately after take off The airplane is accelerated to a speed slightly higher than normal then pulled off abruptly to prevent possible settling back to the runway while drifting When clear of the ground make a coordinated turn into the wind to correct for drift ENROUTE CLIMB CLIMB DATA For detailed data see Maximum Rate Of Climb Data chart in Section VI CLIMB SPE...

Page 28: ...ion VI the mixture should be leaned as follows pull the mixture control out until engine RPM peaks and begins to fall off then enrichen slightly back to peak RPM Carburetor ice as evidenced by an unexplained drop in RPM can be removed by application of full carburetor heat Upon regaining the origi nal RPM with heat off use the minimum amount of heat by trial and error to prevent ice from forming S...

Page 29: ...ourth turn move the control wheel forward of neutral in a brisk motion 4 As rotation stops neutralize rudder and make a smooth re covery from the resulting dive Application of aileron in the direction of the spin will greatly increase the rotation rate and delay the recovery Ailerons should be held in a neutral position throughout the spin and the recovery Intentional spins with flaps extended are...

Page 30: ...ethod of drift correction and land in a nearly level attitude Excessive nose strut inflation can hinder nose wheel alignment with the airplane ground track in a drifting crosswind landing at touchdown and during ground roll This can be counteracted by firmly lowering the nose wheel to the ground after initial contact This action partially com presses the nose strut permitting nose wheel swiveling ...

Page 31: ...are as follows With Preheat 1 With ignition switch OFF and throttle closed prime the engine four to ten strokes as the propeller is being turned over by hand NOTE Use heavy strokes of primer for best atomization of fuel After priming push primer all the way in and turn to locked position to avoid possibility of engine drawing fuel through the primer 2 Propeller Area Clear 3 Master Switch ON 4 Thro...

Page 32: ...e in the intake air duct creating a fire hazard in the event of a backfire If this occurs maintain a cranking action to suck flames into the engine An outside attendant with a fire extinguisher is advised for cold starts without pre heat During cold weather operations no indication will be apparent on the oil temperature gage prior to take off if outside air temperatures are very cold After a suit...

Page 33: ...make every effort to fly not less than 2 000 feet above the surface weather permitting even though flight at a lower level may be consistent with the provisions of government regulations 2 During departure from or approach to an airport climb after take off and descent for landing should be made so as to avoid pro longed flight at low altitude near noise sensitive areas NOTE The above recommended ...

Page 34: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 35: ...nature constitute an electrical emergency and should be dealt with immediately Electrical power malfunctions usually fall into two categories excessive rate of charge and insufficient rate of chargeo The paragraphs below describe the recommended remedy for each situation EXCESSIVE RATE OF CHARGE After engine starting and heavy electrical usage at low engine speeds such as extended taxiing the batt...

Page 36: ...loss of RPM and eventual engine roughness may result from the formation of carburetor ice To clear the ice apply full throt tle and pull the carburetor heat knob full out until the engine runs smooth ly then remove carburetor heat and readjust the throttle If conditions require the continued use of carburetor heat in cruise flight use the mini mum amount of heat necessary to prevent ice from formi...

Page 37: ...l pressure is accompanied by a rise in oil tempera ture there is good reason to suspect an engine failure is imminent Re duce engine power immediately and select a suitable forced landing field Leave the engine running at low power during the approach using only the minimum power required to reach the desired touchdown spot FORCED LANDINGS PRECAUTIONARY LANDING WITH ENGINE POWER Before attempting ...

Page 38: ...are for ditching by securing or jettisoning heavy objects located in the baggage area and collect folded coats or cushions for protection of occupant s face at touchdown Transmit Mayday message on 121 5 MHz giving location and intentions 3 4 1 Plan approach into wind if winds are high and seas are heavy With heavy swells and light wind land parallel to swells 2 Approach with flaps 40 and sufficien...

Page 39: ...rocal of the original heading 4 If necessary adjust heading primarily with skidding motions rather than rolling motions so that the compass will read more ac curately 5 Maintain altitude and airspeed by cautious application of elevator control Avoid overcontrolling by keeping the hands off the control wheel and steering only with rudder EMERGENCY LET DOWNS THROUGH CLOUDS If possible obtain radio c...

Page 40: ...rol to hold a straight heading 6 Apply carburetor heat 7 Clear engine occasionally but avoid using enough power to dis turb the trimmed glide 8 Upon breaking out of clouds apply normal cruising power and resume flight FIRES ENGINE FIRE DURING START ON GROUND Improper starting procedures such as pumping the throttle during a difficult cold weather start can cause a backfire which could ignite fuel ...

Page 41: ...will provide an incombustible mixture 8 Execute a forced landing as described in paragraph Emergency Landing Without Engine Power Do not attempt to restart the engine ELECTRICAL FIRE IN FLIGHT The initial indication of an electrical fire is the odor of burning in sulation The immediate response should be to turn the master switch OFF Then close off ventilating air as much as practicable to reduce ...

Page 42: ...ilter ice Lean the mixture for maximum RPM if carburetor heat is used continuously 6 Plan a landing at the nearest airport With an extremely rapid ice build up select a suitable off airport landing site 7 With an ice accumulation of 1 4 inch or more 011 the wing leading edges be prepared for significantly higher stall speed 8 Leave wing flaps retracted With a severe ice build up on the horizontal ...

Page 43: ...g end of the unit see figure 3 1 Ell OPERATION 1 NORMAL OPERATION As long as the function selector switch remains in the ARM position the ELT automatically activates following an impact of 5g or more 2 ELT FAILURE If g switch actuation is questioned following a minor crash landing gain access to the ELT and place the function selector switch in the ON position 3 PRIOR TO SIGHTING RESCUE AIRCRAFT C...

Page 44: ...eactivates transmitter Used during shipping storage and following rescue ARM Activates transmitter only when g switch receives 5g or more impact 3 ANTENNA RECEPTACLE Connection to antenna mounted on top of the tailcone 3 10 Figure 3 1 the ELT can be heard transmitting place the function seledor switch in the OFF position then immediately return the switch to ARM F o r T r a i n i n g P u r p o s e...

Page 45: ...ion which contradicts the FAA approved markings and placards it is to be disregarded MANEUVERS UTILITY CATEGORY This airplane is certificated in the utility category and is designed for limited aerobatic flight In the acquisition of various certificates such as commercial pilot instrument pilot and flight instructor certain maneuvers are required by the FAA All of these maneuvers are per mitted in...

Page 46: ...lways be exercised to avoid excessive speed which in turn can impose excessive loads In the execution of all maneuvers avoid abrupt use of controls AIRSPEED LIMITATIONS CAS The following is a list of the certificated calibrated airspeed CAS limitations for the airplane Never Exceed Speed glide or dive smooth air Maximum Structural Cruising Speed Maximum Speed Flaps Extended Maneuvering Speed 162 M...

Page 47: ...SI red line 30 60 PSI green arc 100 PSI red line Empty 1 75 gallons unusable each standard tank E red line 1 50 gallons unusable each long range tank TACHOMETER Normal Operating Range At sea level At 5000 feet At 10 000 feet Maximum Allowable 2000 2550 RPM inner green arc 2000 2650 RPM middle green arc 2000 2750 RPM outer green arc 2750 RPM red line SUCTION GAGE GYRO SYSTEM Normal Operating Range ...

Page 48: ...vide ct by 1000 and this value used as the moment 1000 on the loading problem Use the Loading Graph to determine the moment 1000 for each addi tional item to be carried then list these on the loading problem NOTE Loading Graph information for the pilot passengers and baggage is based on seats positioned for average occupant and baggage loaded in the center of the baggage areas as shown on the Load...

Page 49: ... POUNDS A tie down net is proVided to secure baggage in the baggage area The net attaches to six tie down rings Two rings are located on the floor just aft of the seat backs and one ring is ated two inches above the floor on each cabin wall at the aft end of area Two additional rings are located at the top aft end of area At least four rings should be used to restrain the maximum baggage load of 1...

Page 50: ... 6 Lbs Gal Standard Tanks 22 5 Gal Maximum 135 5 7 Long Range Tanks 35 Gal Maximum 4 Pilot and Passenger Sta 33 to 41 340 13 3 5 Baggage Area 1 or Passenger on Child s Seat Sta 50 to 76 120 Lbs Max 25 1 6 6 Baggage Area 2 Sta 76 to 94 40 Lbs Max 7 TOTAL WEIGHT AND MOMENT 1600 56 5 8 Locate this point 1600 at 56 5 on the Center of Gravity Moment Envelope and since this point falls within the envelo...

Page 51: ...I f r H I I I r I I 35 MAX L 200 I H H 30 I _ I I I 11 I I I I I I L I I 150 I _ ___ I I _ ____ 20 1 _ 22 5 MAX LOADING GRAPH 20 100 _ __ l 10 i 10 _ 50 r 1 1 _ I I 0 I I I I 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 LO MOMENT 1000 POUND INCHES NOTES 1 Line representing adjustable seats shows the pilot or passenger center of gravity on adjustable seats positioned for an average occupant Ref er to the ...

Page 52: ...0 r r i E 4 1350 IJ o4 p 1300 e i Q 1250 r r i 3 1200 1150 1100 CENTER OF GRAVITY I I I MOMENT ENVELOPE I I 1 i I I I I I I 1 i I J I I I I I 1J 35 40 45 50 55 60 LOADED AIRCRAFT MOMENT 1000 POUND INCHES F o r T r a i n i n g P u r p o s e s O n l y ...

Page 53: ...hed to the nose wheel When towing with a vehicle do not exceed the nose gear turning angle of 30 either side of center or dam age to the gear will result If the airplane is towed or pushed over a rough surface during hangaring watch that the normal cushioning action of the nose strut does not cause excessive vertical movement of the tail and the resulting contact with low hangar doors or structure...

Page 54: ... to craze Follow by carefully washing with a mild detergent and plenty of water Rinse thoroughly then dry with a clean moist chamois Do not rub the plastic with a dry cloth since this builds up an electrostatic charge which attracts dust Waxing with a good commercial wax will finish the clean ing job A thin even coat of wax polished out by hand with clean soft flan nel cloths will fill in minor sc...

Page 55: ...mical liquids A 50 50 solution of isopropyl alcohol and water will satisfactorily remove ice accumula tions without damaging the paint A solution with more than 50 alcohol is harmful and should be avoided While applying the de icing solution keep it away from the windshield and cabin windows since the alcohol will attack the plastic and may cause it to craze ALUMINUM SURFACES The clad aluminum sur...

Page 56: ...olvent read the instructions on the container and test it on an obscure place on the fabric to be cleaned Never satu rate the fabric with a volatile solvent it may damage the padding and back ing materials Soiled upholstery and carpet may be cleaned with foam type detergent used according to the manufacturer s instructions To minimize wetting the fabric keep the foam as dry as possible and remove ...

Page 57: ...iness Certificate FAA Form 8100 2 2 Aircraft Registration Certificate FAA Form 8050 3 3 Aircraft Radio Station License if transmitter installed FCC Form 556 B To be carried in the aircraft at all times 1 Weight and Balance and associated papers latest copy of the Repair and Alteration Form FAA Form 337 if applicable 2 Aircraft Equipment List C To be made available upon request 1 Aircraft Log Book ...

Page 58: ...wer green arc range Excessive ground runup should be avoided Engine runup also helps to eliminate excessive accumulations of water in the fuel system and other air spaces in the engine Keep fuel tanks full to minimize condensation in the tanks Keep the battery fully charged to prevent the electrolyte from freezing in cold weather If the aircraft is to be stored temporarily or indefinetely refer to...

Page 59: ...e factory and are followed by the Cessna Dealer Organization The complete familiarity of Cessna Dealers with Cessna equipment and factory approved procedures provides the highest level of service possible at lower cost to Cessna owners CESSNA CUSTOMER CARE PROGRAM Specific benefits and provisions of the CESSNA WARRANTY plus other important benefits for you are contained in your CUSTOMER CARE PROGR...

Page 60: ... require servicing inspection and or testing at special intervals Since Cessna Dealers conduct all service inspection and test pro cedures in accordance with applicable Service Manuals it is recommend ed that you contact your Dealer concerning these requirements and begin scheduling your aircraft for service at the recommended intervals Cessna Progressive Care ensures that these requirements are a...

Page 61: ...se items are listed below CUSTOMER CARE PROGRAM BOOK OWNER S MANUALS FOR YOUR AIRCRAFT AVIONICS e POWER COMPUTER SALES AND SERVICE DEALER DIRECTORY DO S AND DON TS ENGINE BOOKLET The following additional publications plus many other supplies that are applicable to your aircraft are available from your Cessna Dealer SERVICE MANUALS AND PARTS CATALOGS FOR YOUR AIRCRAFT ENGINE AND ACCESSORIES AVIONIC...

Page 62: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 63: ...t to 12 500 feet All figures are based on zero wind 22 5 and 35 0 gallons of fuel for cruise McCauley 1Al01 PCM6948 or HCM6948 propeller 1600 pounds gross weight and standard atmospheric conditions Mixture is leaned to maximum RPM Allowances for fuel reserve headwinds take offs and climb and variations in mixture lean ing technique should be made as no allowances are shown on the chart Other indet...

Page 64: ...17 128 138 FLAPS DOWN IAS MPH 40 50 60 70 80 90 100 CAS MPH 40 50 61 72 83 94 105 Figure 6 1 I STALL SPEEDS MPH CAS Gross Weight ANGLE OF BANK 1600 lbs a CONDITION Do 21 Flaps 55 57 63 78 UP Flaps 49 51 56 70 20 I Flaps 48 49 54 67 40 POWER OFF AFT CG Figure 6 2 6 2 F o r T r a i n i n g P u r p o s e s O n l y ...

Page 65: ...D FT MIN GAL FT MIN FROM FT MIN FROM S L GAL S L GAL 1600 76 670 0 6 73 440 1 6 70 220 3 0 NOTES 1 Flaps retracted full throttle mixture leaned to smooth operation above 5000 ft 2 Fuel used includes warm up and take off allowances 3 For hot weather decrease rate of climb 15 ft min for each 10 F above standard day temperature for particular altitude LANDING DISTANCE FLAPS LOWERED TO 40 POWER OFF HA...

Page 66: ...6 3 9 8 2200 40 77 3 2 7 1 11 1 10 000 2700 68 116 5 1 4 4 6 8 2600 61 109 4 6 4 9 7 6 2500 54 102 4 1 5 4 8 5 2400 48 93 3 7 6 1 9 4 2300 42 82 3 3 6 8 10 6 12 500 2650 60 110 4 5 5 0 7 8 2600 56 106 4 3 5 3 8 2 2500 50 97 3 9 5 8 9 1 2400 44 86 3 5 6 5 10 1 NOTES 1 Maximum cruise is normally limited to 75 power WITH LEAN MIXTURE RANGE MILES STANDARD LONG RANGE 22 5 GAL 35 GAL 390 605 410 635 445...

Page 67: ...AXIMUM GLIDE SPEED 70 MPH IAS PROPELLER WINDMILLING FLAPS UP ZERO WIND 12 000 u i ffffffi z w w 0 co 5 10 15 20 GROUND DISTANCE STATUTE MILES Figure 6 5 6 5 F o r T r a i n i n g P u r p o s e s O n l y ...

Page 68: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 69: ...tion The kit consists of two shields to partially cover the cowl nose cap opening the addition of heat ducting from the right exhaust manifold for additional cabin heat a carburetor airbox heat outlet cap and insulation for the engine crankcase breather line Once installed the crankcase breather insulation is approved for permanent use in both cold and hot weather GR OUND SERVICE PLUG RECEPTACLE A...

Page 70: ... transmission The switch is located under the glare shield and is labeled TRANS 1 and 2 Placing the switch in the upper position labeled 1 switches the microphone to the upper transmitter the lower position labeled 2 switches the microphone to the lower transmitter I FUEL TANK QUICK DRAIN VALVE KIT Two fuel tank quick drain valves and a fuel sampler cup are available as a kit to facilitate daily d...

Page 71: ...ndicator is available to replace the standard airspeed indicator in your airplane The true airspeed indicator has a calibrated rotatable ring which works in conjunction with the airspeed indicator dial in a manner similar to the operation of a flight computer TO OBTAIN TRUE AIRSPEED rotate ring until pressure altitude is aligned with outside air temperature in degrees Fahrenheit Then read true air...

Page 72: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 73: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 74: ...lter changes one addi tional quart is required when the filter element is changed OIL AND OIL FILTER CHANGE After the first 25 hours of operation drain engine oil sump and clean the oil pressure screen If an optional oil filter is installed change filter element at this time Refill sump with straight mineral oil non detergent and use until a total of 50 hours has accumulated or oil consumption has...

Page 75: ...F o r T r a i n i n g P u r p o s e s O n l y ...

Page 76: ...F o r T r a i n i n g P u r p o s e s O n l y ...

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