Cessna 150 1969 Owner'S Manual Download

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Summary of Contents for 150 1969

Page 1: ...1 ee a L __j MORE PEOPLE BUY AND FlY CESSNA AIRPLANES THAN ANY OTHER MAKE 1969 WORLD S LARGEST PRO DUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 OWNER S MANUAL...

Page 2: ...5 mi 6 2 hrs 117 mph 565 mi 6 1 hrs 93 mph 880 mi 9 4 hrs 93 mph 670 fpm 12 650 ft 735 ft 1385 ft 445 ft 1075 ft Standard Trainer 975 lbs f0051bs 980 lbs 1010 lbs 120 lbs 10 2 16 0 26 gal 38 gal 6 qts...

Page 3: ...a Service Department stands ready to serve you The following services are offered by most Cessna Dealers FACTORY TRAINED PERSONNEL to provide you with courteous expert service FACTORY APPROVED SERVICE...

Page 4: ...gear depressed and an optional flashing beacon installed OV rall length of airplane with optional bullet shaped propeller spinner When standard propeller spiMer Is Installed length Is 23 77 l _ 8 7 Y...

Page 5: ...LOW UP SYSTEM 4 9 SECTION V OPERATIONAL DATA 5 1 SECTION VI OPTIONAL SYSTEMS 6 1 ALPHABETICAL INDEX tn d ex 1 Thls manual describes the operation and performance of the Standard Model 150 the Trainer...

Page 6: ...lity that the wing tank sumps contain waler Thus the wing tank sump drain plugs and fuel line drain plug should be removed to check for presence of water c Check propeller and spinner for nicks and se...

Page 7: ...over briefly all of the points that you should know for a typical flight The flight and oper ational characteristics of your airplane are normal in all r espects There are no unconventional characteri...

Page 8: ...os Check 75 RPM maximum differential between magnetos 9 Flight Instruments and Radios Set 10 Optional Wing Leveler OFF TAKE OFF NORMAL TAKE OFF 1 Wing Flaps Up 2 Carburetor Heat Cold 3 Throttle Full O...

Page 9: ...RE LANDING 1 Mixture Rich 2 Carburetor Heat Apply full heat before closing throttle 3 Airspeed 65 to 75 MPH 4 Wing Flaps As desired below 100 MPH 5 Airspeed 60 to 70 MPH flaps extended NORMAL LANDING...

Page 10: ...icator IS Bearing lndicator Opt 16 Riaht Fuel Quantity Indicato r 17 Sucllon Ca e Opt 18 Ammeter 19 Oil Temperature Gage 20 011 Pressure G ige 21 Map Compartment 22 Cabin Atr and Heat Control Knobs 23...

Page 11: ...ngine from two tanks one in each wing From thes e tanks fuel flows by gr avity thr ough a fuel s hutoff valve and fuel strainer to the carburetor Refer to figure 2 2 for fuel quantity data For fuel sy...

Page 12: ...FUEL TANK W i ll lllllllllllilill illlilllilllll RIGHT FUEL TANK FUEL 0 FUEL SHUTOFF 22 s G AlS VALVE ON CODE _ _ _o _ o FUEL SUPPLY FUEL SYSTEM SCHEMATIC CARBURETOR TO ENGINE CYLINDERS Figur e 2 3 c...

Page 13: ...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 e...

Page 14: ...NETOS l N RESISTOR Figure 2 4 2 4 SCHEMATIC TO WING FLAP SYSTEM TO LANDING AND TAXI LIGHTS OPT TO FLASHING BEACON OPT TO PITOT HEA T SYSTE OPl TO NAVIGATION LIGHTS AND OPTIO NAL CONTRO L WHEEL MAP LIG...

Page 15: ...particles in the atmosphere particularly at night can produce vertigo and loss of or ientation CABIN HEATI NG AND VENTILATING SYSTEM The temperature and volume of airflow into the cabin can be r egula...

Page 16: ...DIAGRAM USE UP All ERON ON RIGHT WlNG AND NEUTRAL ELEVATOR NOTE Strong quartering tallwlnds require cauUoo Avoid sudden bu rat of the throttle and aharp braking when tile airplane i In tlllB attitude...

Page 17: ...o keep it running After starting if the oil gage does not begin to show pressure with in 30 seconds in the summertime and about twice that long in ver y cold weather stop engine and investigate Lack o...

Page 18: ...ists An absence of RPM drop may be an indication of faulty grounding of one side of the ignition system or should be cause for suspicion that the magneto timing is set in advance of the setting specif...

Page 19: ...he climb to the obstacle The ex ception to this rule would be in a high altitude take off in hot weather where climb would be marginal with flaps 10 Flap deflections of 30 and 40 are not r ecommended...

Page 20: ...uced to 20 immediately after full power is applied Upon r each ing a safe a irspeed the flaps should be slowly retracted L o Lhe full up position CRUISE Normal cruising is done between 65 and 75 power...

Page 21: ...or heat is r ecommended during flight in very heavy rain to avoid the possibility of engine s toppage due to excessive water ingestion The mixture setting should be readjusted for smoothest operation...

Page 22: ...y firmly lowering the nose wheel to the gr ound after initial contact This action partially com presses the nose strut per mitting nose wheel swiveling and positive ground steering COLD WEATHER OPERAT...

Page 23: ...ck 9 Pull carbur etor heat knob full on after engine has started Leave on until engine is running smoothly 10 Lock primer NOTE If the engine does not start during the first few attempts or if the engi...

Page 24: ...ormal and steady the airplane is r eady for take off When operating in sub zero temperature avoid using partial carbu r etor heat Partial heat may increase the carburetor air temperature to the 32 to...

Page 25: ...s section which contradicts the FAA approved markings plac ards and check lists it is to be disregarded MANEUVERS UTILITY CATEGORY This airplane is not designed for purely aer obatic flight However in...

Page 26: ...requirement for execution of any maneuver and care should always be exercised to avoid excessive speed which in turn can impose excessive loads In the execution of all maneuver s avoid abrupt use of c...

Page 27: ...10 000 feet Maximum Allowable WEIGHT AND BALANCE 2000 2550 inner green arc 2000 2650 middle green arc 2000 2750 outer green arc 2750 red line The following information will enable you to operate your...

Page 28: ...envelope and if the loading is acceptable 3 4 NOTE The Weight and Balance Data s heet noted above is in cluded in the aircraft file The Loading Graph and Center of Gravity Moment Envelope shown in th...

Page 29: ...TIE DOWN LOADS 120 POUNDS TIE DOWN NET ATTACH POIN TS A cargo tic down net is provided to secure baggage in the baggage area The net attaches to six tie down rings Two rings are locatCCI on the floor...

Page 30: ...ER AND I FUEL LONG RANGE TANKS 35 GAL MAX 6 CAL I FUEL STANDARD TANKS 22 5 CAL MAX 6 CAL BAGGAGE IN AREA CD OR PASSENGER ON CHILD S SEAT 120 MAX t BAGGAGE TN AREA 40 MAX 35 MAX 30 1 22 5 MAX 20 LOADIN...

Page 31: ...0 CENTER OF GRAVITY 1550 MOM ENT ENVELOPE NORMAL CATEGORY 00 0 1500 UTILITY CATEGORY z 1450 I E o z 1400 E o 1350 ex u el 1300 0 1250 w 8 1200 1150 1100 35 40 45 50 55 60 LOADED AIRCRAFT MOMENT 1000 P...

Page 32: ...s are necessary and about other seasonal and periodic services GROUND HANDLING T he airplane is most easily and safely maneuver ed by hand with a tow bar attached to the nose wheel NOTE Whe n using th...

Page 33: ...tic and may cause it 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 t...

Page 34: ...ice removal with chemical liquids A 50 50 solution of isopropyl alcohol and water will s atisfactorily remove ice accumulations without damaging the paint A solution with mor e than 50 alcohol is harm...

Page 35: ...Before using any solvent read the instructions on the container and te st it on an obscure place on the fabric to be cleaned Never satu rate the fabric with a volatile solvent it may damage the paddi...

Page 36: ...Aircraft Company r ecom mends the 100 hour periodic inspection for your airplane The procedure for this 100 hour inspection has been carefully worked out by the factory and is followed by U1e Cessna...

Page 37: ...ght Computer and Service Policies be carried in the air craft at all times Most of the items listed are r equired by the United States Federal Aviation Regulations Since the regulations of other natio...

Page 38: ...lug should be r emoved to check for presence of water OIL FILLER When preflight check shows low oil level service with aviation grade engine oil SAE 40 above 40 F and SAE 10W30 or SAE 20 below 40 F Mu...

Page 39: ...y maintenance of the filter is recommended NOSE GEAR TORQUE LINKS Lubricate When operating under dusty conditions more frequent lubrication is r ecommended EACH 100 HOURS BRAKE MASTER CYLINDERS Check...

Page 40: ...ow cost service PUBLICATIONS Various publications and flight oper ation aids a re fu rnished in the air craft when delivered from the factory These items are listed below OWNER S MANUALS FOR YOUR ArRC...

Page 41: ...ean mix ture from 2500 feet to 12 500 feet All figures are based on zero wind 22 5 and 35 0 gallons of fuel for cruise McCauley 1A101 DCM6948 propeller 1600 pounds gr oss weight and s tandard atmosphe...

Page 42: ...6S 73 82 91 100 109 118 127 136 Flaps Down IAS 40 so 60 70 80 90 100 CAS 49 SS 63 72 81 89 98 Figure 5 1 I Power Off STALLING SPEEDS MPH CAS I Gross Weig I ANGLE OF BANK I 1 I IAu I 1600 lbs CONDITION...

Page 43: ...IMB USED CLIMB USED CLIMB ff FT MIN GAL FT MIN s g L FT MIN S L GAL 1600 73 I 670 I 0 6 69 I 440 I I 6 65 I 220 I 3 0 NOTES I F1aps retracted lull throttle mixture leaned to smooth operation above 500...

Page 44: ...2 530 830 2300 49 93 3 8 5 9 9 2 550 860 2200 43 84 3 4 6 6 10 3 560 870 2100 37 71 3 0 7 5 l l 7 540 835 7500 2700 74 117 5 5 4 1 6 3 480 745 2600 66 111 4 9 4 6 7 1 505 790 2500 58 105 4 4 5 1 7 9...

Page 45: ...w w z ai ai w w 0 Ill z C w J MAXIMUM GLIDE SPEED 65 MPH IAS PROPELLER WINDMILLING FLAPS UP ZERO WIND 12 000 10 000 8000 6000 4000 2000 5 10 15 20 GROUND DISTANCE STATUTE MILES Figure 5 5 5 5...

Page 46: ...d fuel tanks for greater endurance and range Each tank has a total capacity of 19 gallons Usable fuel in each long range tank for all flight conditions is 17 5 gallons COLD WEATHER EQUIPMENT WINTERIZA...

Page 47: ...ed c ir cuit in the external power system s upplies the needed jumper across the contacts so that with a dead batter y and an external power source applied turning the master switch ON will close the...

Page 48: ...ansmitter TRUE AIRSPEED INDICATOR A true airspeed indicator is available to r eplace the standard airspeed indicator in your airplane The true airspeed indicator has a calibrated r otatable ring which...

Page 49: ...action effectively cor rects adverse yaw induced by the ailerons A separately mounted pus h pull control knob labeled WING LVLR is provided at the lower center of the instrument panel to turn the sys...

Page 50: ...he Turn Coordinator used with the wing leveler system will not be affected by loss of vacuum since it is designed wilh a back up system enabling it to operate from either vac uum or electrical power i...

Page 51: ...ntactor 2 4 Beacon Flashing 2 5 Bearing Indicator 1 4 Before Entering the Airplane 1 1 Befor e Landing 1 3 Befor e Starting the Engine 1 1 Before Take Off 1 2 2 8 magneto check 2 8 warm up 2 8 Brake M...

Page 52: ...it br eaker s 2 3 2 4 ignition switch 1 4 2 4 Index 2 magnetos 2 4 mas ter switch 1 4 2 4 r egulator 2 4 schematic 2 4 star ter 2 4 star ter switch 1 4 2 4 switches 1 4 Elevator Trim Control Wheel 1 4...

Page 53: ...gr am Exterior iv Inspection Service and Inspection Periods 4 4 Instrument Markings Engine 3 3 Interior Care 4 4 L Landing inside cover 2 11 alter 1 3 before 1 3 crosswind 2 12 distance table 5 3 norm...

Page 54: ...de cover Primer Engine 1 4 2 2 Principal Dimensions ii Propeller inside cover care 4 3 Publications 4 9 Index 4 Q Quantity Data Fuel 2 1 Quantity Indicators Fuel 1 4 3 3 Quick Drain Valve Kit Fuel 6 2...

Page 55: ...rmal 1 2 per formance charts 2 9 power checks 2 8 Taxiing 2 7 diagram 2 6 Throttle 1 4 2 2 Tire Pressure ins ide back cover Trim Control Wheel Elevator 1 4 T rue Airspeed Indicator 6 3 Turn Coordinato...

Page 56: ...stablished for replacements Replacements are warranted for the remainder of the applicable six 6 or twelve 12 months original warranty period The repair or replacement of defec tive parts under this w...

Page 57: ...F ICATION MHS 24A MUST BE USE D CAPAC ITY OF E C INE SUMP 6 QUARTS DO NOT OPERATE 0 LESS THAN 4 Q UARTS TO MINIMIZE LOSS OF OIL THROUG H BREAT HER FILL TO 5 QUART LEVEL FOR ORMAL FLIGHTS OF LESS THA 3...

Page 58: ...Cessna TAKE YOUR CESSNA HOME FOR SERVICE AT THE SIGN OF THE CESSNA SH IELD CESSNA AIRCRAFT COMP AN Y WI C HITA KAN S AS lllllllllllllllllllllllllllllllllllllllllllll D624 13...

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Summary of Contents for 150 1969

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Cessna 150 1969, Owner'S Manual

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