Airplane Flight Manual for Cessna 172M Skyhawk
CESSNA 172M SKYHAWK · Flight Manual
Overview
This Airplane Flight Manual (AFM) provides essential information for the operation of the Cessna 172M Skyhawk. It is designed for pilots and aviation enthusiasts, offering detailed specifications, performance data, and operational procedures. The manual covers various aspects of flight, including preflight checks, emergency procedures, and performance limitations. It serves as a comprehensive guide to ensure safe and efficient operation of the aircraft.
- Maximum takeoff weight: 2,400 lbs (1,088 kg)
- Stall speed in landing configuration: 47 knots
- Maximum cruise speed: 122 knots
- Range: approximately 640 nautical miles
- Engine type: Lycoming O-320, 150 horsepower
Document
Source
Originally published by flyefi.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 88
- File size
- 6.5 MB
- Publisher
- flyefi.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 875
- Engine (hp)
- 150
- Height (ft)
- 8.5
- Length (ft)
- 26.92
- Propeller
- Fixed Pitch
- Wingspan (ft)
- 36
- Engine model
- 0-320-E2D
- Empty weight (lb)
- 1,335
- Fuel capacity (gal)
- 42
- Rate of climb (fpm)
- 645
- Service ceiling (ft)
- 13,100
- Max takeoff weight (lb)
- 2,300
Performance
- Landing over 50ft
- 520
- Takeoff over 50ft
- 1,250
- Landing distance (ft)
- 885
- Takeoff distance (ft)
- 1,525
Weight & balance
- Useful load (lb)
- 995
- Max ramp weight (lb)
- 1,410
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,305
- Max landing weight (lb)
- 2,300
- Max takeoff weight (lb)
- 2,300
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172M SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
General Information
The Cessna 172M Skyhawk is a single-engine, four-seat aircraft known for its reliability and ease of handling. It features a high-wing design and is equipped with a Lycoming O-320 engine, providing a maximum power output of 150 horsepower.
Performance Data
The maximum takeoff weight for the Cessna 172M is 2,400 lbs (1,088 kg). The stall speed in landing configuration is approximately 47 knots, while the maximum cruise speed is around 122 knots. The aircraft has a range of about 640 nautical miles with standard fuel capacity.
Operating Procedures
Pilots must conduct a thorough preflight inspection, which includes checking fuel levels, oil quantity, and control surfaces. The manual outlines specific procedures for engine start, taxiing, takeoff, and landing, ensuring pilots follow best practices for safety.
Emergency Procedures
In case of engine failure during flight, pilots should follow the glide procedure to maintain control and find a suitable landing area. The manual details emergency checklists for various scenarios, including electrical failures and cabin fires.
Weight and Balance
Proper weight and balance calculations are crucial for safe flight operations. The manual provides charts and formulas to determine the center of gravity and ensure the aircraft is loaded within its limits.
Safety notes
- Always perform a thorough preflight inspection before flight.
- Follow emergency procedures as outlined in the manual to ensure safety.
- Ensure weight and balance calculations are accurate before takeoff.
Full document text
Cessna. MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE MODEL 172 AND 1975 Skyhawk WORLD'S LARGEST PRO- UCER OF GENERAL VIATION AIRCRAFT SINCE 1956 OWNER'S MANUAL 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 885 ft 1525 ft 520 ft 1250 ft 57 mph 49 mph EMPTY WEIGHT: (Approximate) USEFUL LOAD: (Approximate) Skyhawk II 172 1305 lbs 995 lbs Skyhawk 1350 lbs 950 lbs 1375 lbs 925 lbs F172 Skyhaw 1335 lbs 965 lbs 120 lbs 13 2 15.3 42 gal. 52 gal. 8 qts 75 inches 0-320-E2D 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 cove operation of the Reims/Cessna F172 Skyhawk which is certificated as Model F172M under French Type Certificate No. 25 and FAA Type Certificate No. X4E D1036-13-RGI-1000-6/94 Cessna Aircraft Compan Wichita, Kansas USA 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: It is designed to provide you with the most THE CESSNA WARRANTY 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. i ii 02 8'-91/2" MAX. 26'-11" ** 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 6'-3"MAX. 01 00 10 ** 36' 8'-4½" TABLE OF CONTENTS Page = SECTION I SECTION II - OPERATING CHECKLIST ……………………… 1-1 - DESCRIPTION AND OPERATING DETAILS SECTION III SECTION IV SECTION V - EMERGENCY PROCEDURES 2-1 3-1 - OPERATING LIMITATIONS ….. 4-1 -------- - CARE OF THE AIRPLANE SECTION VI - OPERATIONAL DATA____________ SECTION VII- OPTIONAL SYSTEMS…….. ALPHABETICAL INDEX.…….. 5-1 6-1 7-1 Index-1 This manual describes the operation and performance of the Model 172, the Skyhawk, and the Skyhawk II. Equip- ment described as "Optional" denotes that the subject equipment is optional on the Model 172. Much of this equipment is standard on the Skyhawk and Skyhawk II. iii Section I OPERATING CHECKLIST 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 Checklist form, the steps necessary to op- erate your aircraft efficiently and safely. It is not a checklist 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. A more convenient plastic
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enclosed checklist, stowed in the map compartment, is available for quickly checking that all important procedures have been performed. Since vigilance for other traffic is so important in crowded terminal areas, it is important that preoccupation with checklists be avoided in flight. Procedures should be carefully memorized and performed from memory. Then the checklist should be quickly scanned to ensure that nothing has been missed. 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 airspeeds. Corresponding calibrated airspeed may be obtained from the Airspeed Correction Table in Section VI. 1-1 EXTERIOR 1-2 Refer to inside beck cover of this manual for quantities, materials, and specifications of frequently used service items. 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. a. Remove control wheel lock. b. Check ignition switch OFF. c. Turn on master switch and check fuel quantity indicators; then turn off master switch. d. Check fuel selector valve handle on BOTH. e. Check baggage door for security. Lock with key if children are to occupy child's seat. Figure 3 a. b. c. રે a. 4 a. b. C. d. a. b. C. d. نه نان 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. Before first flight of the day and after each refueling, use sampler cup and drain small quantity of fuel from fuel tank sump quick-drain valve to check for water, sediment, and proper fuel grade. 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, pull out strainer drain knob for about four seconds to clear fuel strainer of possible water and sediment. Check strainer drain closed. If water is observed, the fuel system may contain additional water, and further draining of the system at the strainer, fuel tank sumps, and fuel selector valve drain plug will be necessary. 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. e. f. g. Check nose wheel strut and tire for proper inflation. Disconnect tie-down rope. h. Inspect flight instrument static source opening on side of fuselage for stoppage (left side only). a. Check main wheel tire for proper inflation. b. Before first flight of the day and after each refueling, use sampler cup and drain small quantity of fuel from fuel tank sump quick-drain valve to check for water, sediment, and proper fuel grade. Visually check fuel quantity, then check fuel filler cap secure. Remove pitot tube cover, if installed, and check pitot tube opening for stoppage. C. ⑦ a. b. نف Check fuel tank vent opening for stoppage. c. Check stall warning vent opening for stoppage. 1-1. d. a. Disconnect wing tie-down. Check aileron for freedom of movement and security. 1-3 BEFORE STARTING ENGINE. ADJUST and LOCK. (2) (3) (1) Exterior Preflight COMPLETE. Seats, Belts, Shoulder Harnesses Fuel Selector Valve BOTH. -- -- -- (4) Radios, Autopilot, Electrical Equipment (5) Brakes TEST and SET. -- OFF. STARTING ENGINE. (1) Mixture -- RICH. (2) Carburetor Heat COLD. -- (3) Master Switch -- ON. (4) Prime -- AS REQUIRED (2 to 6 strokes; none if engine is warm). (5) Throttle -- OPEN 1/8 INCH. (6) Propeller Area (7) Ignition Switch (8) Oil Pressure -- -- -- CLEAR. START (release when engine starts). CHECK. BEFORE TAKE-OFF. 1-4 (1) Parking Brake -- SET. (2) Cabin Doors and Window -- CLOSED and LOCKED. (3) Flight Controls FREE and CORRECT. (4) -- TAKE-OFF. -- Elevator Trim (5) Fuel Selector Valve (6) Mixture -- BOTH. RICH (below 3000 ft.). (7) Throttle 1700 RPM. a. b. C. d. -- Magnetos -- CHECK (RPM drop should not exceed 125 RPM on either magneto or 50 RPM differential between magnetos). Carburetor Heat CHECK (for RPM drop). -- -- Engine Instruments and Ammeter CHECK. Suction Gage -- CHECK. (8) Flight Instruments and Radios -- SET. -- OFF. -- ADJUST. (9) Optional Autopilot (10) Throttle Friction Lock (11) Wing Flaps UP. TAKE-OFF. NORMAL TAKE-OFF. (1) Wing Flaps UP. Carburetor Heat -- COLD. (2) (3) Throttle (4) -- FULL. Elevator Control (5) Climb Speed -- -- LIFT NOSE WHEEL (at 60 MPH). 75 to 85 MPH. MAXIMUM PERFORMANCE TAKE-OFF. (1) Wing Flaps (2) -- UP. Carburetor Heat (3) Brakes -- -- COLD. · APPLY. (4) Throttle FULL. (5) Brakes -- RELEASE. (6) Airplane Attitude SLIGHTLY TAIL LOW. (7) Climb Speed -- 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) Throttle (3) Mixture -- FULL. FULL RICH (mixture may be leaned above 3000 feet). CRUISE. (1) Power (2) -- 2200 to 2700 RPM (no more than 75%). Elevator Trim ADJUST. (3) Mixture -- LEAN. 1-5 LET-DOWN. (1) Mixture -- RICH. -- (2) Power AS DESIRED. (3) Carburetor Heat -- AS REQUIRED (to prevent carburetor icing). BEFORE LANDING. (1) Fuel Selector Valve (2) Mixture -- RICH. (3) Carburetor Heat -- BOTH. ON (apply full heat before closing throttle). (4) Airspeed 70-80 MPH (flaps UP). (5) Wing Flaps (6) Airspeed. -- -- AS DESIRED. 65 - 75 MPH (flaps DOWN). BALKED LANDING. (1) Throttle FULL. (2) Carburetor Heat -- COLD. (3) Wing Flaps 20°. (4) Airspeed -- 65 MPH. (5) Wing Flaps - RETRACT (slowly). NORMAL LANDING. (1) Touchdown -- MAIN WHEELS FIRST. (2) Landing Roll -- LOWER NOSE WHEEL GENTLY. (3) Braking MINIMUM REQUIRED. -- AFTER LANDING. -- UP. -- COLD. (1) Wing Flaps (2) Carburetor Heat 1-6 SECURING AIRCRAFT. (1) Parking Brake -- SET. -- OFF. (2) Radios, Electrical Equipment, Autopilot · (3) Mixture IDLE CUT-OFF (pulled full out). (4) Ignition Switch -- -- OFF. (5) Master Switch OFF. (6) Control Lock -- INSTALL. 1-7 1-8 INSTRUMENT PANEL 10 11 12 13 14 15 16 17 18 19 20 42 41 40 39 38 37 36 35 34 33 29 28 27 26 25 24 23 22 21 30 32 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. No. 2 LOC Reversed Indicator Light (Opt.) 8. No. 1 LOC Reversed Indicator Light (Opt.) 9. Omni Course Indicators (Opt.) 10. ADF Bearing Indicator (Opt.) 11. Magnetic Compass 12. Radio Selector Switches (Opt.) 13. Rear View Mirror (Opt.) 14. Radios and Transponder (Opt.) 15. Autopilot Control Unit (Opt.) 16. Fuel and Oil Gages .31 17. Over-Voltage Warning Light 18. Ammeter 19. Optional Instrument Space 20. ADF (Opt.) 21. Optional Radio Space 32. Map Compartment 23. Wing Flap Position Indicator 24. Cigar Lighter 25. Cabin Air/Heat Control Knobs 26. Wing Flap Switch 27. Static Pressure Alternate Source Valve (Opt.) 28. Mixture Control Knob 29. Throttle 30. Microphone (Opt.) 31. Fuel Selector Valve Handle 33. Elevator Trim Control Wheel 33. Carburetor Heat Control Knob 34. Electrical Switches 35. Circuit Breakers 38. Parking Brake Handle 37. Optional Instrument Space 38. Ignition Switch 39. Instrument and Radio Dial Light Rheostats 40. Master Switch 41. Auxiliary Mike and Phone Jacks (Opt.) 42. Primer 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 Checklist 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 2-1
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