Cessna 150 1968 Скачать руководство пользователя

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to ramp tie-down.

(4)

Install a surface control lock over the fin and rudder.

(5)

Install a pitot tube cover.

(6) Tie a rope to an exposed portion of the engine mount and secure

the opposite end to a ramp tie-down.

WINDSHIELD-WIND

W S.

The plastic windshield and windows should be cleaned with an aircraft

windshield cleaner. Apply the cleaner sparingly with soft cloths, and rub

with moderate pressure until all dirt, oil scum and bug stains are re

moved. Allow the cleaner to dry, then wipe it off with soft flannel cloths.

a windshield cleaner is not available, the plastic can be cleaned

with soft cloths moistened with Stoddard solvent to remove oil and grease.

NOTE

Never use gasoline, benzine, alcohol, acetone, carbon

t-etrachloride, fire extinguisher or anti-ice fluid, lacquer

•thinner or glass cleaner to clean the plastic. These ma

terials will attack the plastic 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 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 scratches and help prevent further scratching.

Do not use a canvas cover on the windshield unless freezing rain or

sleet is anticipated since the cover may scratch the plastic surface.

PAINTED SURFACES.

The painted exterior surfaces of your new Cessna have a durable,

long lasting finish and, under normal conditions, require no polishing or

buffing. Approximately

days are required for the paint to cure com

pletely; in most cases, the curing period will have been completed prior

to delivery of the airplane. In the event that polishing or buffing is re -

quired within the curing period, it is recommended that the work be done

4-2

Содержание 150 1968

Страница 1: ...1 RE A E MO R CES A i FLYING T A N AN fHi _ ___ _ I IDITCO JIDJEIT Jl CQ I 1968 I OWNER S MANllAL...

Страница 2: ...7 mph 475 mi 4 l hrs 117 mph 725 mi 6 2 hrs 117 mph 565 mi 6 1 hrs 93 mph 880 mi 9 4 hrs 93 mph 670 pm 12 650 ft 735 ft 1385 ft 445 It 1075 ft Standard Trainer 980 lbs 1010 lbs 985 lbs 1015 lbs 120 lb...

Страница 3: ...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...

Страница 4: ...gear depressed and an optional flashing beacon installed Overall length or airplane with optional bullet shaped propeller spinner When standard propeller spinner is installed length is 23 8 7Y MAX 3...

Страница 5: ...LLOW UP SYSTEM 4 8 SECTION V OPERATIONAL DATA 5 1 SECTION VI OPTIONAL SYSTEMS 6 1 ALPHABETICAL INDEX lndex 1 This manual describes the operation and performance of the Standard Model 150 the Trainer a...

Страница 6: ...urlng walk around inspection tr nlghl flight Is planned check operalJon of all lights and make sure a flashlight Is avaJlable c Check carburetor 3 lr Hiter for restr ictlons by dust or other foreign m...

Страница 7: ...but it does cover briefly all of the points that you should know for a typical flight The flight and operational characteristics of your airplane are normal in all respects There are no unconventiona...

Страница 8: ...E OFF setting 8 Cabin Doors Latched 9 Flight Instruments and Radios Set 10 Optional Wing Leveler OFF V 1 Aw TAKE OFF NORMAL TAKE OFF 1 Wing Flaps Up 2 Carburetor Heat Cold 3 Throttle Full OPEN 4 Eleva...

Страница 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...

Страница 10: ...pt 18 Suction Gage Opl 30 Carburetor Heat Control Knob Gyro Horizon Opt 19 Opllonal Instrument Space 31 Vertical Speed Indicator Opt Aircraft Registration Number 20 Map Compartment 32 Parking Brake Co...

Страница 11: ...ne from two tanks one in each 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 se...

Страница 12: ...FUEL SHUTOFF 22 s GAlS VALVE o c J RIGHT FUEL TANK CODE _ _ o o FUEL SUPPLY ENGINE PRIMER FUEL SYSTEM SCHEMATIC CARBURETOR TO ENGINE CYLINDERS Figure 2 3 c J VENT MECHANICAL LINKAGE THROTTLE MIXTURE...

Страница 13: ...t panel protect the majority of electrical circuits in the airplane Labeling above each fuse retainer indicates the circuits protected by the fuses Fuse capacity is shown on each fuse retainer cap Fus...

Страница 14: ...LINE DIODE H CAPACITOR MECHANICAL CONNECTION IGNITION SWITCH MAGNETOS Figure 2 4 SCHEMATIC _ 1 10 TO LANDING TAXI LIGHTS OPT TO FLASHING BEACON OPT TO PITOT HEAT SYSTEM OPn TO DOME LIGHT TO NAVIGATION...

Страница 15: ...volume of airflow into the cabin can be regulated to any degree desired by manipulation of the push pull CABIN HEAT and CABIN AIR knobs Heated fresh air and outside air are blended in a cabin manifold...

Страница 16: ...CTION DIAGRAM USE UP AILERON ON RIGHT WING AND NEUTRAL ELEVATOR USE DOWN AILERON ON RIGHT WING AND DOWN ELEVATOR Strong quartering tatlwlnda require caution Avoid sudden bursts or the throtlle and sha...

Страница 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 very cold weather stop engine and investigate Lack of...

Страница 18: ...exists 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 spec...

Страница 19: ...m in the 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 recomme...

Страница 20: ...GO AROUND CLIMB In a balked landing go around climb the wing flap setting should be reduced to 20 immediately after full power is applied Upon reach ing a safe airspeed the flaps should be slowly ret...

Страница 21: ...ending upon the turbulence of the air SHORT FIELD LANDINGS For a short field landing make a power off approach at 58 MPH with flaps 40 and land on the main wheels first Immediately after touchdown low...

Страница 22: ...er priming push primer all the way in and turn to locked position to avoid possibility of engine drawing fuel through the primer 2 Clear propeller 3 Pull master switch ON 4 Turn ignition switch to BOT...

Страница 23: ...or 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 suitable w...

Страница 24: ......

Страница 25: ...n 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 aerobatic flight However in the acqu...

Страница 26: ...an in aerodynamic design and will build up speed quickly with the nose doWQ Proper speed control is an essentia l requirement for execution of any maneuver and care should always be exercised to avoid...

Страница 27: ...n arc 2750 red line The following information will enable you to operate your Cessna within the prescribed weight and center of gravity limitations To figure the weight and balance for your particular...

Страница 28: ...1 BAGGAGE LOADING AND TIE DOWN LOADS 120 POUNDS _ e 1 _ I TIE DOWN NET ATTACH POINTS 3 4 A cargo tie down net Is provided lo secure baggage In the baggage area The net attaches to slx lie down rings T...

Страница 29: ...LOT AND PASSENGER AND fUEL LONG RANGE TANKS 35 GAL MAX 6 GAL FUEL STANDARD TANKS 22 5 GAL MAX 6 GAL BAGGAGE IN AREA CD OR PASSENGER ON CHILD S SEAT 120 MAX BAGGAGE IN AREA 40 MAX 35 MAX o 20 22 5 MAX...

Страница 30: ...500 J g 1450 E tI g 1400 w 1350 0 1300 e i A 1250 w 3 1200 1150 1100 I A I I A lf ir I f 1 1 r l 1 1 CENTER OF GRAVITY MOMENT ENVELOPE NORMAL CATEGORY _ u rii ITY CA TEGORY 35 40 45 l J i lil P 50 55...

Страница 31: ...hanges are necessary and about other seasonal and periodic services GROUND HANDLING The airplane is most easily and safely maneuvered by hand with a tow bar attached to the nose wheel NOTE When using...

Страница 32: ...tack the plastic 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...

Страница 33: ...d with water to remove dirt oil and grease may be removed with gasoline naphtha car bon tetrachloride or other non alkaline solvents Dulled aluminum sur faces may be cleaned effectively with an aircra...

Страница 34: ...sene Volatile solvents such as mentioned in paragraphs on care of the windshield must never be used since they soften and craze the plastic INSPECTION SERVICE AND INSPECTION PERIODS With your airplane...

Страница 35: ...all data requirements are met A To be displayed in the aircraft at all times 1 Aircraft Airworthiness Certificate Form FAA 1362B 2 Aircraft Registration Certificate Form FAA 500A 3 Aircraft Radio Stat...

Страница 36: ...plug should be removed 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 M...

Страница 37: ...y maintenance of the filter is recommended NOSE GEAR TORQUE LINKS Lubricate When operating under dusty conditions more frequent lubrication is recommended EACH 100 HOURS BRAKE MASTER CYLINDERS Check a...

Страница 38: ...icient low cost service PUBLICATIONS Included in your aircraft file are various manuals which describe the operation of the equipment in your aircraft These manuals plus many other supplies that are a...

Страница 39: ...lean 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 gross weight and standard atmosphe...

Страница 40: ...5 73 82 91 100 109 118 127 136 Flaps Down IAS 40 50 60 70 80 90 100 CAS 49 55 63 72 81 89 98 Figure 5 1 I Power Off STALLING SPEEDS MPH CAS I Gross Weig I ANGLE OF BANK I 1600 lbs ffe I l o IAu I ICON...

Страница 41: ...RATE OF I FUEL CLIMB FT MIN S L GAL 69 I 440 I 1 6 AT 10000 FT 23 F CLIMB 5 AS MPHrATE OF I FUEL FT MIN S L GAL 65 I 220 I 3 0 Flaps retracted full throttle mixture leaned to smooth operation above 50...

Страница 42: ...___ 2300 49 93 3 8 5 9 9 2 550 860 2200 43 84 3 4 6 6 10 3 560 870 I I _ 1 f 2100 37 71 3 0 7 5 11 7 540 835 7500 2700 74 117 5 5 4 1 6 3 480 745 2600 66 Ill 4 9 4 6 7 1 505 790 2500 58 105 4 4 5 1 7...

Страница 43: ...i w w z w I w 0 CD I J 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...

Страница 44: ......

Страница 45: ...g range fuel tanks are available to replace the standard wings and 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 f...

Страница 46: ...r transmitter and the down position selects the lower transmitter TRU E A IRSPEED INDICATOR A true airspeed indicator is available to replace the standard airspeed indicator in your airplane The true...

Страница 47: ...iations The rudder action effectively cor rects adverse yaw induced by the ailerons The wing leveler system has manual roll trim capabilities which may be used to compensate for asymmetrical loading o...

Страница 48: ...m can be easily overpowered servo forces C lUld significantly alter the manual feel of the aileron control especially should a malfuriction occur FUEL TANK QUICK DRAIN VALVE KIT Two fuel tank quick dr...

Страница 49: ...Take Off 1 2 2 8 magneto check 2 8 warm up 2 8 Brake Master Cylinders 4 7 Brake System Parking 2 5 c Cabin Air and Heat Controls 1 4 Cabin Heating and Ventilating System 2 5 Capacity baggage inside c...

Страница 50: ...eight inside cover Engine inside cover before starting 1 1 Index 2 instrument markings 3 3 oil dipstick 4 6 oil filler 4 6 op ration limitations 3 2 primer 2 2 starting 1 1 2 7 Equipment Cold Weather...

Страница 51: ...ht Landing 2 5 Limitations airspeed 3 2 engine operation 3 2 Loading Power inside cover Loading Graph 3 5 Loading Problem Sample 3 4 Long Range Fuel Tanks 6 1 Lubrication and Servicing Procedures 4 6...

Страница 52: ...Switch 6 2 Range inside cover Registration Number Aircraft 1 4 Regulator Voltage 2 4 s Sample Loading Problem 3 4 Secure Aircraft 1 3 Service Ceiling inside cover Servicing and Lubrication 4 6 Servici...

Страница 53: ...l Wheel Elevator 1 4 True Airspeed Indicator 6 2 Turn Coordinator 1 4 u Utility Category Maneuvers 3 1 v Vacuum System Air Filter 4 7 Vacuum System Oil Separator 4 7 Vertical Speed Indicator 1 4 w Wei...

Страница 54: ...is not established 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 und...

Страница 55: ...MOTORS SPECIFICATION MHS 24A MUST BE USED CAPACITY OF ENGINE SUMP 6 QUARTS DO NOT OPERATE ON LESS THAN 4 QUARTS TO MINIMIZE LOSS OF OIL THROUGH BREATHER FILL TO 5 QUART LEVEL FOR NORMAL FLIGHTS OF LES...

Страница 56: ...C essna TAKE Y O U R C F SS N A H O M 1 0 SERVICE A f T H E S I G O F 1 H i C E S S N A S H I ELD CESSNA A I R CRAFT C O M P A N Y W I C HITA K A N S A S I I 1 f f...

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