Cessna-172-1975-Model-POH.pdf - St Pete Air
CESSNA 172C · Pilot's Operating Handbook
Overview
The Cessna 172H Pilot's Operating Handbook (POH) serves as a comprehensive guide for pilots operating the Cessna 172H aircraft. It includes essential information on the aircraft's systems, performance data, operating procedures, and limitations. This manual is designed to assist pilots in understanding the aircraft's capabilities and ensuring safe operation. It is an invaluable resource for both new and experienced pilots, providing detailed instructions and specifications necessary for flight planning and execution.
- Maximum takeoff weight: 2,400 lbs
- Useful load: approximately 900 lbs
- Fuel capacity: 40 gallons
- Stall speed in landing configuration: 47 knots
- Takeoff distance over a 50-foot obstacle: approximately 1,600 feet
Document
Source
Originally published by stpeteair.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 92
- File size
- 3.1 MB
- Publisher
- stpeteair.org
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 650
- Engine (hp)
- 150
- Height (ft)
- 11
- Length (ft)
- 26
- Propeller
- Fixed Pitch
- Wingspan (ft)
- 36
- Engine model
- 0-320-E2D
- Empty weight (lb)
- 1,305
- Fuel capacity (gal)
- 38
- Rate of climb (fpm)
- 645
- Service ceiling (ft)
- 13,100
- Max takeoff weight (lb)
- 2,300
Performance
- Landing over 50ft
- 1,250
- Takeoff over 50ft
- 1,525
- Landing distance (ft)
- 520
- Takeoff distance (ft)
- 865
Weight & balance
- Useful load (lb)
- 995
- Max ramp weight (lb)
- 2,300
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,305
- Max landing weight (lb)
- 2,300
- Max takeoff weight (lb)
- 2,300
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In this document
Aircraft Specifications
The Cessna 172H features a maximum takeoff weight of 2,400 lbs, a useful load of approximately 900 lbs, and a fuel capacity of 40 gallons. The aircraft is powered by a Lycoming O-320 engine, producing 150 horsepower. The stall speed in landing configuration is 47 knots.
Operating Limitations
The POH outlines critical operating limitations, including a maximum speed of 129 knots and a maximum altitude of 14,000 feet. The aircraft must not be flown in icing conditions, and the maximum crosswind component for takeoff and landing is 15 knots.
Performance Data
Key performance data includes a takeoff distance over a 50-foot obstacle of approximately 1,600 feet and a landing distance over a 50-foot obstacle of about 1,500 feet. The rate of climb at sea level is approximately 730 feet per minute.
Emergency Procedures
The manual provides detailed emergency procedures, including engine failure during takeoff, which requires immediate landing straight ahead and maintaining control of the aircraft. It also covers procedures for electrical failures and in-flight fires.
Weight and Balance
The weight and balance section includes guidelines for calculating the center of gravity and ensuring the aircraft is within weight limits for safe operation. It emphasizes the importance of proper loading to maintain stability.
Safety notes
- Do not operate the aircraft in icing conditions.
- Maximum crosswind component for takeoff and landing: 15 knots.
Full document text
Print Double Sided Cessna MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE MODEL 172 AND 1975 Skyhawk OWNER'S WORLD'S LARGEST PRO. DUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 MANUAL 2938.10.1105 PERFORMANCE - SPECIFICATIONS Skyhawk GROSS WEIGHT SPEED: Top Speed at Sea Level Cruise, 75% Power at 8000 ft RANGE: Cruise, 75% Power at 8000 ft 38 Gallons, No Reserve Cruise, 75% Power at 8000 ft 48 Gallons, No Reserve Maximum Range at 10,000 ft 38 Gallons, No Reserve Maximum Range at 10,000 ft 48 Gallons, No Reserve RATE OF CLIMB AT SEA LEVEL SERVICE CEILING TAKE-OFF: Ground Run Total Distance Over 50-Foot Obstacle LANDING: Ground Roll Total Distance Over 50-Foot Obstacle STALL SPEED: Flaps Up, Power Off Flaps Down, Power Off BAGGAGE WING LOADING: Pounds/Sq Foot POWER LOADING: Pounds/HP FUEL CAPACITY: Total Standard Tanks Optional Long Range Tanks OIL CAPACITY PROPELLER: Fixed Pitch, Diameter ENGINE: Lycoming Engine. 150 rated HP at 2700 RPM 2300 lbs 144 mph 138 mph 650 mi 4.7 hrs 138 mph 815 mi 5.9 hrs 138 mph 700 mi 6.0 hrs 117 mph 875 mi 7.5 hrs 117 mph 645 fpm 13, 100 ft 865 ft 1525 ft 520 ft 1250 ft 57 mph 49 mph . F172 Skyhawk 120 Ibs 13 2 15.3 42 gal. 52 gal. 8 qts 75 inches 0-320-E2D Skyhawk Skyhawk II EMPTY WEIGHT: (Approximate) USEFUL LOAD: (Approximate) 172 1305 lbs 995 lbs 1350 lbs 950 lbs 1375 lbs 925 lbs 1335 lbs 965 lbs F172 Skyhawk II 1410 lbs 890 lbs NOTE: Speed performance data is shown for the Skyhawk which is one to four mph faster than a standard equipped Model 172 (without speed fairings), with the maximum difference occurring at top speed. There is a corresponding difference in range while all other performance figures are the same for the Model 172 as shown for the Skyhawk. *This manual covers operation of the Model 172/Skyhawk which is certificated as Model 172M under FAA Type Certificate No. 3A12. The manual also covers operation of the Reims/Cessna F172 Skyhawk which is certificated as Model F172M under French Type Certificate No. 25 and FAA Type Certificate No. A4EU. D1036-13-RAND-14000-5/74 2938.10.1105 CONGRATULATIONS Welcome to the ranks of Cessna owners! Your Cessna has been designed and con- structed to give you the most in performance, economy, and comfort. It is our de- sire that you will find flying it, either for business or pleasure, a pleasant and profitable experience. This Owner's Manual has been prepared as a guide to help you get the most pleasure and utility from your Model 172/Skyhawk. It contains information about your Cessna's equipment, operating procedures, 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 a Cessna. World-wide, the Cessna Dealer Organization backed by the Cessna Service Depart- ment stands ready to serve you. The following services are offered by most Cessna Dealers: THE CESSNA WARRANTY -- It is designed to provide you with the most comprehensive coverage possible: a. b. C. d. No exclusions Coverage includes parts and labor Available at Cessna Dealers world wide Best in the industry Specific benefits and provisions of the warranty plus other important benefits for you are contained in your Customer Care Program 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 provide you with courteous expert service. FACTORY APPROVED SERVICE EQUIPMENT to provide you with the most efficient and accurate workmanship possible. A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING 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 Dealer 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. 2938.10.1105 1 ii 5° * 8-92" MAX. 26'-11" 11'-4" * ** Maximum height of aircraft with nose gear depressed, all tires and nose strut properly inflated, and optional flashing beacon installed. Wing span of aircraft with optional strobe lights installed. PRINCIPAL DIMENSIONS 2938.10.1105 6'-3"MAX. 00 ** 36' 8'-4½' TABLE OF CONTENTS SECTION I - OPERATING CHECK LIST Page = 1-1 SECTION || - DESCRIPTION AND OPERATING DETAILS 2-1 SECTION III w EMERGENCY PROCEDURES 3-1 SECTION IV - OPERATING LIMITATIONS 4-1 SECTION V -- CARE OF THE AIRPLANE. 5-1 SECTION VI - OPERATIONAL DATA.. 6-1 SECTION VII- OPTIONAL SYSTEMS. 7-1 2938.10.1105 This manual describes the operation and performance of both the Cessna Model 172 and Skyhawk. Equipment de- scribed as "Optional" denotes that the subject equipment is optional on the Model 172. Much of this equipment is standard on the Skyhawk model. iii 2938.10.1105 Section I OPERATING CHECK LIST One of the first steps in obtaining the utmost performance, service, and flying enjoyment from your Cessna is to familiarize yourself with your aircraft's equipment, systems, and controls. This can best be done by reviewing this equipment while sitting in the aircraft. Those items whose function and operation are not obvious are covered in Section II. Section I lists, in Pilot's Check List form, the steps necessary to operate your aircraft efficiently and safely. It is not a check list in its true form as it is considerably longer, but it does cover briefly all of the points that you should know for a typical flight. An abbreviated check list
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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 characteristics of your aircraft are normal in all respects. There are no "unconventional" characteristics or opera- tions that need to be mastered. All controls respond in the normal way within the entire range of operation. All airspeeds mentioned in Sections I, II and III are indicated air speeds. Corresponding calibrated air speeds may be obtained from the Airspeed Correction Table in Section VI. BEFORE ENTERING THE AIRPLANE. (1) Make an exterior inspection in accordance with figure 1-1. 2938.10.1105 1-1 8 EXTERIOR 6 5 Refer to inside back cover of this manual for quantities, materials, and specifications of frequently used service items. 4 3 INSPECTION 2 Note Visually check aircraft for general condition during walk- around inspection. In cold weather, remove even small accumulations of frost, 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. Turn on master switch and check fuel quantity indicators; then turn off master switch. Check fuel selector valve handle on BOTH. Check baggage door for security. Lock with key if children are to occupy child's seat. a. b. ن فنه 1-2 d. e. öö 2938.10.1105 Figure 2 a. 3 4 5 6 b. C. a. a. b. C. a. b. C. d. نه نحن e. f. g. h. a. b. 7) a. b. c. d. 8 a. Remove rudder gust lock, if installed. Disconnect tail tie-down. Check control surfaces for freedom of movement and security. Check aileron for freedom of movement and security. Disconnect wing tie-down. Check main wheel tire for proper inflation. Visually check fuel quantity; then check fuel filler cap secure. Check oil level. Do not operate with less than six quarts. Fill to eight quarts for extended flights. Before first flight of the day and after each refueling, drain fuel strainer. With fuel selector valve turned to the left and right tank positions, pull out strainer drain knob for about four seconds to clear fuel system of possible water and sedi- ment. After both tanks have been drained, make sure that strainer drain is closed. If water is observed in these checks, the system may contain additional water, and the fuel tank sump drain plugs and fuel selector valve drain plug should be removed to check for the presence of water. Check propeller and spinner for nicks and security. Check landing light(s) for condition and cleanliness. Check carburetor air filter for restrictions by dust or other foreign matter. Check nose wheel strut and tire for proper inflation. Disconnect tie-down rope. Inspect flight instrument static source opening on side of fuselage for stoppage (left side only). Check main wheel tire for proper inflation. Visually check fuel quantity, then check fuel filler cap secure. Remove pitot tube cover, if installed, and check pitot tube opening for stoppage. Check fuel tank vent opening for stoppage. Check stall warning vent opening for stoppage. Disconnect wing tie-down. Check aileron for freedom of movement and security. 1-1. 2938.10.1105 1-3 BEFORE STARTING THE ENGINE. (1) Seats, Seat Belts and Shoulder Harnesses (2) Fuel Selector Valve -- (3) Brakes Test and set. BOTH. (4) Radios and Electrical Equipment STARTING THE ENGINE. (1) Mixture --- Rich. (2) Carburetor Heat Cold. (3) Primer -- -- -- OFF. Adjust and lock. 26 strokes as required (none if engine is warm). Close and lock primer. -- Open 1/8". (4) Throttle (5) Master Switch (6) Propeller Area (7) Ignition Switch (8) Oil Pressure -- -- -- ON. Clear. START (release when engine starts). Check. BEFORE TAKE-OFF. (1) Parking Brake -- Set. (2) Flight Controls -- Check for free and correct movement. (3) Fuel Selector Valve - BOTH. (4) (5) Elevator Trim Control Wheel - Throttle Setting 1700 RPM. -- -- TAKE-OFF setting. Check. (6) Engine Instruments and Ammeter (8) Magnetos -- -- (7) Suction Gage Check (4.6 to 5.4 inches of mercury). Check (RPM drop should not exceed 125 RPM on either magneto or 50 RPM differential between magnetos). (9) Carburetor Heat Check operation. (10) Flight Instruments and Radios (11) Optional Autopilot -- Off. (12) Throttle Friction Lock Adjust. Set. (13) Cabin Doors and Window Closed and locked. TAKE-OFF. NORMAL TAKE-OFF. (1) Wing Flaps 0°. -- 1-4 2938.10.1105 (2) Carburetor Heat -- Cold. (3) Power Full throttle. (4) Elevator Control Lift nose wheel at 60 MPH. (5) Climb Speed 75 to 85 MPH. MAXIMUM PERFORMANCE TAKE-OFF. (1) Wing Flaps 0° --- Cold. (2) Carburetor Heat (3) Brakes Apply. (4) Power - Full throttle. (5) Brakes -- -- Release. (6) Airplane Attitude (7) Climb Speed -- -- Slightly tail low. 68 MPH until all obstacles are cleared. ENROUTE CLIMB. (1) Airspeed -- 80 to 90 MPH. NOTE If a maximum performance climb is necessary, use speeds shown in the Maximum Rate-Of-Climb Data chart in Section VI. (2) Power - Full throttle. (3) Mixture Full rich (mixture may be leaned above 3000 feet). CRUISING. (1) Power - 2200 to 2700 RPM. -- Adjust. (2) Elevator Trim Control Wheel (3) Mixture Lean for maximum RPM. LET-DOWN. 2938.10.1105 (1) Mixture Rich. (2) Power As desired. (3) Carburetor Heat -- As required to prevent carburetor icing. 1-5 BEFORE LANDING. (1) Fuel Selector Valve (2) Mixture Rich. F (3) Carburetor Heat -- Both. · Apply full heat before closing throttle. (4) Wing Flaps As desired. (5) Airspeed -- 70 to 80 MPH (flaps up), 65 to 75 MPH (flaps down). BALKED LANDING (GO-AROUND). (1) Power Full throttle. (2) Carburetor Heat -- Cold. (3) Wing Flaps -- Retract to 20°. (4) Upon reaching an airspeed of approximately 65 MPH, retract flaps slowly. NORMAL LANDING. -- (1) Touchdown (2) Landing Roll (3) Braking -- Main wheels first. -- Lower nose wheel gently. Minimum required. AFTER LANDING. Up. (1) Wing Flaps (2) Carburetor Heat -- Cold. SECURING AIRCRAFT. (1) Parking Brake Set. -- (2) Radios and Electrical Equipment OFF. (3) Mixture Idle cut-off (pulled full out). (4) Ignition and Master Switch (5) Control Lock Installed. OFF. 1-6 2938.10.1105 2938.10.1105 1-7 1-8 INSTRUMENT PANEL 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 ooooooooo $85.95 XPSQ 38 37 36 35 34 33 32 31 24 23 22 21 20 19 18 17 30' 25 29' 26 1. Clock (Opt.) 2. Aircraft Registration Number 3. Flight Instrument Group 4. Suction Gage (Opt.) 5. Marker Beacon Indicator Lights and Switches (Opt.) 6. Altimeter, Vertical Speed Indicator (Opt.) and Tachometer 7. Omni Course Indicators (Opt.) and ADF Bearing Indicator (Opt.) 8. Magnetic Compass 9. Radio Selector Switches (Opt.) 10. Rear View Mirror (Opt.) 11. Radios and Transponder (Opt.) 12. Fuel and Oil Gages 13. Over-Voltage Warning Light 28' 14. Ammeter (Opt.) -27 15. Optional Instrument Space 16. Radio (Opt.) 17. Optional Radio Space 18. Map Compartment 19. Wing Flap Position Indicator 20. Cigar Lighter 24. Mixture Control Knob 25. Autopilot Control Unit (Opt.) 26. Microphone (Opt.) 27. Fuel Selector Valve Handle 28. Elevator Trim Control Wheel 29. Throttle (With Friction Lock) 30. Carburetor Heat Control Knob 31. Electrical Switches 32. Circuit Breakers 33. Parking Brake Handle 34. Optional Instrument Space 35. Ignition/Starter Switch 21. Cabin Air/Heat Control Knobs 36. Instrument and Radio Dial 22. Wing Flap Switch 23. Static Pressure Alternate Source Valve (Opt.) Light Rheostats 37. Master Switch 38. Primer 2938.10.1105 Figure 2-1. || Section II DESCRIPTION AND OPERATING DETAILS The following paragraphs describe the systems and equipment whose function and operation is not obvious when sitting in the aircraft. This section also covers in somewhat greater detail some of the items listed in Check List form in Section I that require further explanation. FUEL SYSTEM. Fuel is supplied to the engine from two tanks, one in each wing. With the fuel selector valve on BOTH, the total usable fuel for all flight conditions is 38 gallons for the standard tanks. Fuel from each wing tank flows by gravity to a selector valve. De- pending upon the setting of the selector valve, fuel from the left, right, or both tanks flows through a fuel strainer and carburetor to the engine induction system. The fuel selector valve should be in the BOTH position for take-off, climb, landing, and maneuvers that involve prolonged slips or skids. Operation from either LEFT or RIGHT tank is reserved for cruising flight. NOTE With low fuel (1/8th tank or less), a prolonged steep de- scent (1500 feet or more) with partial power, full flaps, and 80 MPH or greater should be avoided due to the pos- sibility of the fuel tank outlets being uncovered, causing temporary fuel starvation. If starvation occurs, leveling the nose should restore power within 20 seconds. NOTE When the fuel selector valve handle is in the BOTH po- sition in cruising flight, unequal fuel flow from each 2938.10.1105 2-1
What's in the CESSNA 172C TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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