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Cessna 150 STANDARD User manual

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Copyright 2025 Manuals.Online. All Rights Reserved.

ESSNA
MORE PEOPLE BUY AND
FLY CESSNA AIRPLANES
THAN ANY OTHER MAKE
1967
WORLD'S LARGEST PRO- OWNER'S
,o¶ 4G NC RA, MANUAL
SINCE 1956
Intentional Spins and
other Aerobatic
Maneuvers prohibited per
AD 2009-10-09 R2.
NOTE: This does not
prohibit intentional stalls.
PERFORMANCE -SPECIFICATIONS SERVICING REQUIREMENTS
STANDARD
AND TRAINER COMMUTER FUEL:
AVIATION GRADE -- 80/87 MINIMUM GRADE
CAPACITY EACH STANDARD TANK -- 13 GALLONS
GREESS WEIGHT . . .. . . . . . . . . .... . 1600 lbs 1600 lbs CAPACITY EACH LONG RANGE TANK -- 19 GALLONS
Top Speed At Sea Level . . . . . . . . . . . . 123 mph 125 mph
Cruise, 75% Power at 7500 ft . . . . . . . . . 120 mph 122 mph
RANGE:
Cruise, 75% Power at 7500 ft ..... . ...480 mi 490 mi ENGINE OIL:
22.5 Gallons, No Reserve 4.0 hrs 4.0 hrs AVIATION GRADE -- SAE 40 ABOVE 40° F.
120 mph 122 mph SAE 10W30 OR SAE 20 BELOW 40° F.
CrL ge, 75%e VoweLan,
7355000
Gallons 2h-s 2s(lVIULTI-VISCOSITY OIL WITH ARANGE OF SAE 10W30
120 mph 122 mph IS RECOMMENDED FOR IMPROVED STARTING IN COLD
Optimum Range at 10, 000 ft ... . ... . .560 mi 565 mi WEATHER. DETERGENT OR DISPERSANT OIL, CON-
22.5 Gallons, No Reserve 5.7 hrs 5.7 hrs FORMING TO CONTINENTAL MOTORS SPECIFICATION
98 mph 99 mph MHS-24, MUST BE USED.
Optimum Range at 10, 000 ft . . . . . . . . . 870 mi 885 mi CAPACITY OF ENGINE SUMP -- 6QUARTS
Long Range Version, 35.0 Gallons 8.9 hrs 8.9 hrs
98 mph 99 mph (DO NOT OPERATE ON LESS THAN 4QUARTS. TO
RATE OF CLIMB AT SEA LEVEL . . . . . . . . . 670 fpm 670 fpm MINIMIZE LOSS OF OIL THROUGH BREATHER, FILL
SERVICE CEILING ............ . .. . 12, 650 ft 12, 650 ft TO 5QUART LEVEL FOR NORMAL FLIGHTS OF LESS
TAKE-OFF: THAN 3HOURS. FOR EXTENDED FLIGHT, FILL TO
Ground Run .... . . . . . . . . . . . . . 735 ft 735 ft 6 QUARTS. IF OPTIONAL OIL FILTER IS INSTALLED,
Total Distance Over 50-ft Obstacle ... . . ..1385 ft 1385 ft ONE ADDITIONAL QUART IS REQUIRED WHEN THE
LANDING: FILTER ELEMENT IS CHANGED.
Landing Roll . . . . . . .... . . . .. . . . 445 ft 445 ft
Total Distance Over 50-ft Obstacle ... . ...1075 ft 1075 ft
EMPTY WEIGHT: (Approximate) Standard Trainer
With Standard Fuel Tanks . . . ... . . 975 lbs 1005 lbs 1060 lbs
With Long Range Fuel Tanks . . . . ...980 lbs 1010 lbs 1065 lbs HYDRAULIC FLUID:
BAGGAGE ..... . .. ... . . . . . . . . 120 lbs 120 lbs MIL-H-5606 HYDRAULIC FLUID
WING LOADING: Pounds/Sq Foot .. . .. . ...10. 2 10. 2
POWER LOADING: Pounds/HP . . . . . ... . .16. 016. O
FUEL CAPACITY:
Total (Standard Tanks) . . . . ... . . . . 26 gal. 26 gal· TIRE PRESSURE:
Total (Long Range Tanks) . . . . . . . . . . . 38 gal. 38 gal.
OIL CAPACITY: Total . . . . ... . ... . ..6qts 6 qts NOSE WHEEL --- 30 PSI ON 5:00 ×5TIRE
PROPELLER: Fixed Pitch (Diameter) ... . . . . 69 inches 69 inches MAIN WHEELS -- 21 PSI ON 6:00 ×6TIRES
ENGINE: Continental Engine ....... . .. . O-200-A* O-200-A*
100 rated HP at 2750 RPM
*The Model F150, which is manufactured by Reims Aviation S. A. ,Reims (Marne) France, is NOS E GEARSHOCKSTRU T:
identical to the 150 except that it is powered by an O-200-A engine manufactured under license KEEP FILLED WITH FLUID AND INFLATED TO 20 PSI
by Rolls Royce, Crewe, England. All 150 information in this manual pertains to the F150 as well. •
DO NOT OVER-INFLATE.
D397-13-RAND-1000-9/77
CONGRATULATIONS . . . . .
Welcome to the ranks of Cessna owners! Your Cessna has been designed
and constructed to give you the most in performance, economy, and com-
fort. It is our desire that you will find flying it, either for business or
pleasure, apleasant and profitable experience.
This Owner's Manual has been prepared as aguide to help you get the
most pleasure and utility from your Model 150. It contains information
about your Cessna's equipment, operating procpdures, and performance;
and suggestions for its servicing and care. We urge you to read it from
cover to cover, and to refer to it frequently.
Our interest in your flying pleasure has not ceased with your purchase of
aCessna. World-wide, the Cessna Dealer Organization backed by the
Cessna 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 EQUIPMENT to provide you
with the most efficient and accurate workmanship possible.
ASTOCK OF GENUINE CESSNA SERVICE PARTS on hand
when you need them.
THE LATEST AUTHORITATIVE INFORMATION FOR SERV-
ICING CESSNA AIRPLANES, since Cessna Dealers have all
of the Service Manuals and Parts Catalogs, kept current by
Service Letters and Service News Letters, published by Cessna
Aircraft Company.
We urge all Cessna owners to use the Cessna Daaler Organization to the
fullest.
A current Cessna Dealer Directory accompanies your new airplane. The
Directory is revised frequently, and a current copy can be obtained from
your Cessna Dealer. Make your Directory one of your cross-country
flight planning aids; a warm welcome awaits you at every Cessna Dealer.
i
*Maximum height of airplane with nose gear depressed and
an optional flashing beacon installed.
** Overal11ength of airplane with optional bullet -shaped
propeller spinner. When standard propeller spinner
is installed, length is 23'.
8'-7½" MAX.
**23 -9"
10 -D"
PRINCIPAL
DIMENSIONS
ii
+- 7-0
6-6½"
ii
TABLE OF CONTENTS
SECTION I-OPERATING CHECK LIST.............. 1-1
SECTION 11 -DESCRIPTION AND
OPERATING DETAILS ...................... 2-1
SECTION lli -OPERATING LIMITATIONS............. 3-1
SECTION IV -CARE OF TH E AIRPLANE ............ 4-1
OWNER FOLLOW-UP SYSTEM ........................... 4-8
SECTION V -OPERATIONAL DATA ...................... 5-1
SECTION VI -OPTIONAL SYSTEMS...................... 6-1
A LPH A BET IC A LINDEX ........................................ Index -1
This manual describes the operation and performance of
the Standard Model 150, the Trainer and the Commuter. Equip-
ment described as "Optional" denotes that the subject equipment
is optional on the Standard airplane. Much of this equipment is
standard on the Trainer and Commuter.
iii
distance table, 5-3
flap settings, 2-8
maximum performance, 1-2 Vacuum System Air Filter, 4-7
normal, 1-2 Vacuum System Oil Separator, 4-7
performance charts, 2-9 Vertical Speed Indicator, 1-4
power checks, 2-8
6 4 TRXiing, 2-7
diagram, 2-6 W
IThrottle, 1-4, 2-2
Tire Pressure, inside back cover Weight,
Trim Tab Control Wheel, Elevator, empty, inside cover
831-4 gross, inside cover, 3-1
N0TE True Airspeed Indicator, 6-2 Weight and Balance, 3-3
Turn-and-Bank Indicator, 1-4 center of gravity envelope, 3-6
n's"p"eion ic neianiiierne" loading graph, 3-5
aircraft condition during walk- Sample loading problem, 3-4
around inspection. If night
EXTERIOR flight is planned, check operation Wheel Bearings, 4-7
of all lights, and make sure aWindshield -Windows, 4-2
INSPE CTION flashlight is available. UWing Flap Switch, 1-4
Wing Loading, inside cover
Utility Category, Maneuvers, 3-1 Winterization Kit, 6-1
2
(a) Turn on master switch and check fuel quantity (c) Check carburetor air filter for restrictions by
indicators, then turn master switch off, dust or other foreign matter.
(b) Check ignition switch "OFF." (d) On first flight of day and after each refueling,
(c) Check fuel valve handle "ON." pull strainer drain knob and drain a two-
(d) Remove control wheel lock, ounce quantity of fuel trom the fuel strainer
to check for presence of water and sediment.
(e) Check nosewheel strut and tire for proper
inflation.
(a) Remove rudder gust lock, if installed. (f) Disconnect nose lie-down.
(b) Disconnect tail tie-down.
(a) Remove gust lock, if installed. Same as
4(a) Check main wheel tire for proper inflation.
(b) Inspect airspeed static source hole on side of
fuselage for stoppage (left side only). (a) Remove pitot tube cover, if installed, and
(c) Disconnect wing tie-down. check pitot tube opening for stoppage.
(b) Check fuel tank vent opening for stoppage.
(c) Check stall warning vent opening for stoppage.
5(a) Check all level. Do not operate with less than
4 quarts. Fill for extended flights.
(b) Check propeller and spinner for nicks and
security. Same as
Figure 1-1.
iv Index-5
filter, 4-7 S•
temperature gage, 1-4, 3-3
pressure gage, 1-4, 3-3 Sample Loading Problem, 3-4
Operation, Cold Weather, 2-11 Secure Aircraft, 1-3
Operation Limitations, Engine, 3-2 Service Ceiling, inside cover
Operations Authorized, 3-1 Servicing and Lubrication, 4-6 OPERATING CHECK LIST
Optimum Cruise Performance, 2-10 Servicing Intervals Check List, 4-7
Optional Instrument Space, 1-4 Servicing Requirements Table,
Owner Follow-Up System, 4-8 inside back cover
Shimmy Dampener 4-7 One of the first steps in obtaining the utmost performance, service,
Short Field Landing, 2-11 and flying enjoyment from your Cessna is to familiarize yourself with your
PShut-Off Valve Fuel, 2-2 airplane's equipment, systems, and controls. This can best be done by
Specifications -Performance, reviewing this equipment while sitting in the airplane. Those items whose
. . function and operation are not obvious are covered in Section II.
Painted Surfaces, 4-2 inside cover
Parking Brake Control, 1-4 eeeedd,S inC11dnebco2 Section Ilists, in Pilot's Check List form, the steps necessary to
Parking Brake System, 2-5 Stalls 2-10 operate your airplane efficiently and safely. It is not acheck list in its
Performance -Specifications' speed chart, 5-2 true form as it is considerably longer, but it does cover briefly all of the
inside cover Starter, 2-4 points that you should know for atypical flight.
Power, inside cover
..Starter Handle, 1-4, 2-4
Power Loading, inside cover Starting Engine 1-1, 2-5 The flight and operational characteristics of your airplane are normal
Primer, Engine, 1-4, 2-2 before, 1-1 in all respects. There are no unconventional characteristics or operations
Principal Dimensions, ii Strainer, Fuel, 2-1, 2-2, 4-6, 4-7 that need to be mastered. All controls respond in the normal way within
Propeller, inside cover Suction Relief Valve Inlet Screen, the entire range of operation. All airspeeds mentioned in Sections I and
care, 4-3 4-7 II are indicated airspeeds. Corresponding calibrated airspeeds may
Publications, 4-8 Surfaces, be obtained from the Airspeed Correction Table in Section V.
aluminum, 4-3
painted, 4-2
Sy stec in heating and ventilating, BEFOREENTER INGTHE AIRPLANE.
Quantity Data, Fuel, 2-1 2-5
Quantity Indicators, Fuel, 1-4, 3-3 electrical, 2-3 (1) Make an exterior inspection in accordance with figure 1-1.
fuel, 2-1
owner follow-up, 4-8
Rparking brake, 2-5 BEFORE STARTING THE ENGINE.
(1) Seats and Seat Belts -- Adjust and lock.
Radio, 1-4 T(2) Brakes -- Test and set.
Radio Transmitter Selector I(3) Master Switch -- "ON. "
Switch, 6-2 (4) Fuel Valve Handle -- "ON "
Range, inside cover Table of Contents, iii
Rate of Climb, inside cover Tachometer, 1-4, 3-3
Rate-of-ClimbDataTable, 5-3 Take-Off, inside cover, 1-2, 2-8 STARTING THE ENGINE
Registration Number, Aircraft, 1-4 before take-off, 1-2, 2-7
Regulator, Voltage, 2-4 crosswind, 2-9 (1) Carburetor gat -- Cold.
Index-4 1-1
(2) Mixture -- Rich. Gross Weight, inside cover, 3-1 Loading Graph, 3-5
(3) Primer -- As required. Ground Handling, 4-1 Loading Problem, Sample, 3-4
(4) Ignition Switch -- "BOTH. "Gyro, Directional, 1-4 Long Range Fuel Tanks, 6-1
(5) Throttle -- Open 1/4". Gyro Horizon, 1-4 Lubrication and Servicing
(6) Propeller Area -- Clear. Procedures, 4-6
(7) Starter Handle -- Pull. HM
BEFORE TAKE-OFF. Handling Airplane on Ground, 4-1
Heating and Ventilating System, Magnetic Compass, 1-4
(1) Throttle Setting -- 1700 RPM. Cabin, 2-5 Magnetos, 2-4
(2) Engine Instruments -- Within green arc. Hydraulic Fluid, inside back cover Maneuvers -Utility Category, 3-1
(3) Magnetos -- Check (75 RPM maximum differential between magneto Map Compartment, 1-4
(4) Carburetor Heat -- Check operation. Markings, Instrument, 3-3
(5) Suction Gage -- Check (4. 6 to 5. 4 inches of mercury). Master Cylinders, Brake, 4-7
(6) Flight Controls -- Check. Master Switch, 1-4, 2-4
(7) Trim Tab -- "TAKE-OFF" setting. Indicator, Maximum Glide, 5-5
(8) Cabin Doors -- Latched. airspeed, 1-4, 6-2 Maximum Performance Climb, 1-3
(9) Flight Instruments and Radios -- Set. turn-and-bank, 4-4 Maximum Performance Take-Off,
vertical speed, 1-4 1-2
Indicators, Fuel Quantity, 1-4, 3-3 Maximum Rate-of-Climb Data, 5-3
TAKE-OFF. Ignition Switch, 1-4, 2-4 Mixture Control Knob, 1-4, 2-2
Inspection Diagram, Exterior, iv Moment Envelope, Center of
NORMAL TAKE-OFF. Inspection Service and Inspection Gravity, 3-6
(1) Wing Flaps -- Up. Periods, 4-4 Mooring Your Airplane, 4-1
(2) Carburetor Heat -- Cold. Instrument Markings, Engine, 3-3
(3) Throttle -- Full "OPEN. "Interior Care, 4-3
(4) Elevator Control -- Lift nose wheel at 50 MPH. N
(5) Climb Speed -- 72 MPH until all obstacles are cleared, then set
up climb speed as shown in "NORMAL CLIMB" paragraph- LNormal Climb, 1-2
Normal Landing, 1-3
MAXIMUM PERFORMANCE TAKE-OFF- Landing, inside cover, 2-11 Normal Take-Off, 1-2
(1) Wing Flaps -- UP. after, 1-3 Nose Gear Shock Strut, 4-7
(2) Carburetor Heat -- Cold. before, 1-3 Nose Gear Torque Links, 4-7
(3) Brakes -- Hold. crosswind, 2-11
(4) Throttle -- Full "OPEN. "distance table, 5-3
(5) Brakes -- Release. lights, 2-3
(6) Elevator Control -- Slightly tail low. normal, 1-3
(7) Climb Speed -- 52 MPH (with obstacles ahead). short field, 2-11 Oil System,
Light, Landing, 2-3 capacity, inside cover s
Limitations, dipstick, 4-6
CL1MB-air speed, 3-2 engine oil, 4-7, inside back
NORMAL CLIMB. engine operation, 3-2 cover
(1) Air Speed -- 75 to 80 MPH. Loading, Power, inside cover filler, 4-6
1-2 Index-3
Cruise Performance Table, 5-4 Elevator Trim Control Wheel, 1-4 (2) Power -- Full throttle.
Cruising, 1-3, 2-10 Empty Weight, inside cover (3) Mixture -- Rich (unless engine is rough).
Engine, inside cover
before starting, 1-1 MAXIMUM PERFORMANCE CLIMB.
Dinstrument markings, 3-3 (1) Air Speed -- 72 MPH.
oil dipstick, 4-6 (2) Power -- Full throttle.
oil filler, 4-6 (3) Mixture -- Rich (unless engine is rough).
Diagb gage loading/tie-down, 3-4 operation limitations, 3-2
electrical, 2-4 21--21, 2-5 CRUISING.
exterior inspection, iv
fuel 2-2 Equipment, Cold Weather, 6-1
'Exterior Care 4-2, 4-3 (1) Power -- 2000 to 2750 RPM.
maximum glide, 5-5 Exterior Inspe'ction Diagram, iv (2) Elevator Trim -- Adjust.
principal dimensions, ii (3) Mixture -- Lean to maximum RPM.
taxiing, 2-6
Dimensions, Principal, ii F
Dipstick, Oil, 4-6 BEFORE LANDING.
Directional Gyro, 1-4 File, Aircraft, 4-5
Distance Table' Filler, Oil, 4-6 (1) Mixture -- Rich.
landing, 5-3 Filter, Carburetor Air, 4-7 (2) Carburetor Heat -- Apply full heat before closing throttle.
take-off, 5-3 Filter, Oil, 4-7 (3) Airspeed -- 65 to 75 MPH.
Flashing Beacon, 2-3 (4) Wing Flaps -- As desired below 100 MPH.
Fuel System, 2-1 (5) Airspeed -- 60 to 70 MPH (flaps extended).
Ecapacity, inside covers
carburetor, 2-2
Electrical System, 2-3 fuel line drain plug, 4-7 NORM ALL ANDING.
alternator, 2-4 fuel tanks, 2-2
ammeter, 1-4, 2-3, 2-4 fuel tank fillers, 4-6 (1) Touch Down -- Main wheels first.
hattery, 2-4, 4-7 fuel tank sump drains, 4-7 (2) Landing Roll -- Lower nose wheel gently.
battery contactor, 2-4 long range fuel tanks, 6-1 (3) Braking -- Minimum required.
cigar lighter, 1-4, 2-4 mixture control knob, 1-4, 2-2
clock, 1-4, 2-4 primer, 1-4, 2-2
flashing beacon, 2-3 quantity data, 2-1 AFTER LAND ING.
fuses and circuit breakers, quantity indicators, 1-4, 3-3
2-3, 2-4 schematic, 2-2 (1) Wing Flaps -- Up.
ignition switch, 1-4, 2-4 shut-off valve, 2-2 (2) Carburetor Heat -- Cold.
landing lights, 2-3 strainer, 2-1, 2-2, 4-6, 4-7
magnetos, 2-4 Fuse/Circuit Breaker Panel, 1-4
master switch, 1-4, 2-4 Fuses and Circuit Breakers, 2-3, 2-4 SECURE AIRCR A FT.
regulator, 2-4
schematic, 2-4 (1) Mixture -- Idle cut-off.
starter, 2-4 (2) All Switches -- Off.
starter handle, 1-4, 2-4 (3) Parking Brake -- Set.
switches, 1-4 Go-Around Climb, 2-10 (4) Control Lock -- Insta11ed.
Index-2 1-3
INSTRUMENT PANEL ALPHABETICAL INDEX
234567810 11 12 3 14 516 17 19
AC
After Landing, 1-3 Cabin Air and Heat Controls, 1-4
Air and Heat Controls, Cabin, 1-4 Cabin Heating and Ventilating
Air Filter, Carburetor, 4-7 System, 2-5
Air Filter, Vacuum System, 4-7 Capacity,
Aircraft Registration Number, 1-4 baggage, inside cover
Airplane, fuel, inside covers
before entering, 1-1 oil, inside covers
file, 4-5 Carburetor, 2-2
ground handling, 4-1 air filter, 4-7
mooring, 4-1 air heat control, 1-4
secure, 1-3 Care,
Airspeed Correction Table, 5-2 exterior, 4-2, 4-3
Airspeed Indicator, 1-4 interior, 4-3
Airspeed Limitations, 3-2 propeller, 4-3
Alternator, 2-4 Center of Gravity Moment
Altimeter, 1-4 Envelope, 3-6
Aluminum Surfaces, 4-3 Check List, Servicing Intervals, 4-7
Ammeter, 1-4, 2-3, 2-4 Cigar Lighter, 1-4, 2-4
Authorized Operations, 3-1 Climb, 1-2, 2-9
climb data, 2-9
climb speeds, 2-9
36 35 14 33 :2 31 30 29 28 27 26 25 24 23 22 21 20 8go-around clinib, 2-10
maximum performance, 1-3
1. Altimeter 13. Oil Pressure Gage 25. Mixture Control Knob Baggage, Capacity, inside cover maximum rate-of-climb data,
2. AirspeedIndicator 14. OilTemperatureGage 26. Throttle Baggage Loading/Tie-Down, 324 5-3
r'e"etÌnd-B
yr ncator(Opt.) AFume ue tityIndicator(Right) Ehnr craTrimeChonStro1Wheel Battery, 2-4, 4-7 ROrmal, 1-2
5. Vertical Speed Indicator (Opt.) 17. Optional Instrument Space 29. Carburetor Air Heat Control Battery Contactor, 2-4 Clock, 1-4, 2-4
m°piss ŠreoenCard SOp nnalGans ru nt Space Omni Course Indicator (Opt.) BORCOn, Flashing, 2-3 Cold Weather Equipment, 6-1
8. Optional Radio 20. Map Compartment 32. Clock BOÎOre Entering the Airplane, 1-1 winterization kit, 6-1
1e"1"Ûnty na cator (Left) 21 CF ser/CLircuit Breaker Panel 3Stern tBOÎOre Landing, 1-3 Cold Weather Operation, 2-11
11. Aircraft Registration Number 23. Cabin Air and Heat Controls 35. Primer BOÎOre Starting the Engine, 1-1 Compass Correction Card, 1-4
12. Tachometer 24. Wing Flap Switch 36. Master Switch BOÎOre Take-Off, 1-2, 2-7 Compass, Magnetic, 1-4
magneto check, 2-7 Correction Table, Airspeed, 5-2
warm-up, 2-7 Crosswind Landing, 2-11
Figure 2-1. Brake Master Cylinders, 4-7 Crosswind Take-Off, 2-9
Brake System, Parking, 2-5 Cruise Performance, Optimum, 2-10
1-4 Index-1