Pilot's Operating Handbook Cessna 172P Skyhawk
CESSNA 172P SKYHAWK · Pilot's Operating Handbook
Overview
This Pilot's Operating Handbook (POH) is specifically designed for the Cessna 172P Skyhawk, providing essential information for pilots operating this aircraft. It includes detailed sections on aircraft specifications, performance data, operating procedures, and safety information. The handbook serves as a comprehensive guide for both new and experienced pilots, ensuring they have access to critical information for safe flight operations. The content is structured to facilitate quick reference during preflight checks, in-flight operations, and emergency procedures, making it an invaluable resource for effective aircraft management.
- Wingspan: 36 ft 1 in
- Max Takeoff Weight: 2,400 lbs
- Cruise Speed: 120 knots
- Stall Speed (Clean): 54 knots
- Fuel Capacity: 40 gallons
Document
Source
Originally published by www.mattbeyer.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 388
- File size
- 14 MB
- Publisher
- www.mattbeyer.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 440
- Engine (hp)
- 160
- Propeller
- Fixed Pitch
- Engine model
- O-320-D2J
- Max speed (kt)
- 123
- Cruise speed (kt)
- 120
- Empty weight (lb)
- 1,438
- Fuel capacity (gal)
- 40
- Rate of climb (fpm)
- 700
- Service ceiling (ft)
- 13,000
- Max takeoff weight (lb)
- 2,400
Performance
- Landing over 50ft
- 1,280
- Takeoff over 50ft
- 1,625
- Landing distance (ft)
- 540
- Takeoff distance (ft)
- 890
- Stall speed clean (kt)
- 51
- Stall speed landing (kt)
- 46
V-speeds
- VS1
- 51
- VSO
- 46
Weight & balance
- Useful load (lb)
- 969
- Max ramp weight (lb)
- 2,407
- Baggage allowance (lb)
- 120
- Basic empty weight (lb)
- 1,438
- Max landing weight (lb)
- 2,400
- Max takeoff weight (lb)
- 2,400
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172P SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 172P Skyhawk to your watchlist and track it in one place.
More CESSNA 172P SKYHAWKmanuals & documents
- Regal Air Instrument Pilot HandbookTraining Manual
- EMERGENCY PROCEDURESEmergency Procedures
- Airworthiness Directives (ADs) – Current Only – Search Results for "Cessna" filtered by "Cessna 172P"Airworthiness Directives
- CESSNA 172 Aircraft Rev-022 SK4172-42A.DOCService Bulletins
- AAIB Bulletin No: 11/2003Service Bulletins
- PERFORMANCE SPECIFICATIONS CESSNA MODEL 172PPerformance Data
- PILOT'S OPERATING HANDBOOK and FAA APPROVED AIRPLANE FLIGHT MANUALPilot's Operating Handbook
- CESSNA 172P PERFORMANCE CHARTSPerformance
- Chapter 3: Aircraft Construction - Federal Aviation AdministrationType Certificate
- Cessna 172P Skyhawk Pilot's Operating HandbookPilot's Operating Handbook
- Pilot's Operating HandbookPilot's Operating Handbook
If you fly the CESSNA 172P SKYHAWK, you may also be researching these.
In this document
Aircraft Specifications
The Cessna 172P Skyhawk features a wingspan of 36 feet, 1 inch, a length of 27 feet, 2 inches, and a height of 8 feet, 11 inches. The empty weight is approximately 1,600 pounds, while the maximum takeoff weight is 2,400 pounds. The fuel capacity is 40 gallons, providing ample range for various flight operations.
Performance Data
The performance section outlines critical flight metrics, including a takeoff distance of approximately 1,600 feet and a landing distance of about 1,500 feet. The stall speed in a clean configuration is 54 knots, while the landing stall speed is 61 knots. The aircraft has a maximum cruise speed of 120 knots and a service ceiling of 14,000 feet.
Operating Procedures
This section details standard operating procedures for the Cessna 172P, including preflight checks, engine start procedures, and emergency protocols. Pilots are advised to follow the outlined steps to ensure safety and compliance with aviation regulations.
Weight and Balance
Weight and balance considerations are crucial for safe flight operations. The basic empty weight of the Cessna 172P is 1,600 pounds, with a maximum ramp weight of 2,400 pounds. The useful load is 800 pounds, allowing for passengers and cargo within specified limits.
Safety Information
Safety notes emphasize the importance of adhering to operational limits, including maximum crosswind components and proper weight distribution. Pilots are reminded to conduct thorough preflight inspections and to be aware of environmental factors that may affect flight safety.
Safety notes
- Always perform a thorough preflight inspection before flight.
- Adhere to weight and balance limits to ensure safe operations.
- Be aware of maximum crosswind limits during takeoff and landing.
Full document text
Pilot's Operating Handbook and FAA Approved Airplane Flight Manual 0- Cessna Cessna Aircraft Company THIS DOCUMENT MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES. 1984 Model 172P Serial No. 17276232 Registration No. N97811 THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR PART 3 AND CONSTI- TUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. Member of GAMA COPYRIGHT © 1983 Cessna Aircraft Company Wichita, Kansas USA Original Issue - 21 July 1983 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON 08-30-84 SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY IN- SERTED. R Rogus Cessna Aircraft Company, Pawnee Aircraft Division о CESSNA MODEL 172P CONGRATULATIONS CONGRATULATIONS .... Welcome to the ranks of Cessna owners! Your Cessna has been designed and constructed to give you the most in performance, economy, and comfort. It is our desire that you will find flying it, either for business or pleasure, a pleasant and profitable experience. This Pilot's Operating Handbook has been prepared as a guide to help you get the most pleasure and utility from your airplane. 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. Worldwide, the Cessna Dealer Organization backed by the Cessna Customer Services Department stands ready to serve you. The following services are offered by most Cessna Dealers: THE CESSNA WARRANTY, which provides coverage for parts and labor, is available at Cessna Dealers worldwide. Specific benefits and provisions of warranty, plus other important benefits for you, are contained in your Customer Care Program book, supplied with your airplane. Warranty service is available to you at authorized Cessna Dealers 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 efficient and accurate workmanship. A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNA AIR- PLANES, since Cessna Dealers have all of the Service Manuals and Parts Catalogs, kept current by Customer Care Service Information Letters and Customer Care News Letters, published by Cessna Aircraft Company. We urge all Cessna owners to use the Cessna Dealer Organization to the fullest. A current Worldwide Customer Care 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. Original Issue PERFORMANCE- SPECIFICATIONS CESSNA MODEL 172P PERFORMANCE - SPECIFICATIONS *SPEED: Maximum at Sea Level Cruise, 75% Power at 8000 Ft CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. 75% Power at 8000 Ft 40 Gallons Usable Fuel 75% Power at 8000 Ft 50 Gallons Usable Fuel 75% Power at 8000 Ft 62 Gallons Usable Fuel Maximum Range at 10,000 Ft 40 Gallons Usable Fuel Maximum Range at 10.000 Ft 50 Gallons Usable Fuel Maximum Range at 10,000 Ft 62 Gallons Usable Fuel RATE OF CLIMB AT SEA LEVEL SERVICE CEILING TAKEOFF PERFORMANCE: Ground Roll Total Distance Over 50-Ft Obstacle LANDING PERFORMANCE: Ground Roll Total Distance Over 50-Ft Obstacle STALL SPEED (KCAS): Flaps Up, Power Off Flaps Down, Power Off MAXIMUM WEIGHT: Ramp .. Takeoff or Landing STANDARD EMPTY WEIGHT: Skyhawk Skyhawk II MAXIMUM USEFUL LOAD: Skyhawk Skyhawk II BAGGAGE ALLOWANCE WING LOADING: Pounds/Sq Ft POWER LOADING: Pounds/HP FUEL CAPACITY: Total Standard Tanks Long Range Tanks Integral Tanks OIL CAPACITY ENGINE: Avco Lycoming 123 KNOTS 120 KNOTS .Range Time 440 NM 3.8 HRS .Range 585 NM Time 5.0 HRS .Range 755 NM Time 6.4 HRS .Range 520 NM Time .Range 5.6 HRS 680 NM Time .Range 7.4 HRS 875 NM 9.4 HRS Time 700 FPM 13,000 FT 890 FT 1625 FT 540 FT 1280 FT 51 KNOTS 46 KNOTS . 2407 LBS 2400 LBS 1438 LBS 1457 LBS • 969 LBS • 950 LBS 120 LBS 13.8 15.0 43 GAL. 54 GAL. 68 GAL. 8 QTS 160 BHP at 2700 RPM PROPELLER: Fixed Pitch, Diameter O-320-D2J 75 IN. *Speed performance is shown for an airplane equipped with optional speed fairings, which increase the speeds by approximately 2 knots. There is a corresponding differ- ence in range, while all other performance figures are unchanged when speed fair- ings are installed. The above performance figures are based on the indicated weights, standard atmos- pheric conditions, level hard-surface dry runways, and no wind. They are calculated values derived from flight tests conducted by the Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes and numer- ous factors affecting flight performance. ii Original Issue CESSNA MODEL 172P COVERAGE/REVISIONS/ LOG OF EFFECTIVE PAGES COVERAGE The Pilot's Operating Handbook in the airplane at the time of delivery from Cessna Aircraft Com- pany contains information applicable to the 1984 Model 172P airplane designated by the serial number and registration number shown on the Title Page of this handbook. This information is based on data available at the time of publication. REVISIONS Changes and/or additions to this handbook will be covered by revisions published by Cessna Air- craft Company. These revisions are distributed to owners of U. S. Registered aircraft according to FAA records at the time of revision issuance. Revisions should be examined immediately upon receipt and incorporated in this handbook, NOTE It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes.
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Owners should contact their Cessna Dealer whenever the revision status of their handbook is in question. A revision bar will extend the full length of new or revised text and/or illustrations added on new or presently existing pages. This bar will be located adjacent to the applicable revised area on the outer margin of the page. All revised pages will carry the revision number and date on the applicable page. The following Log of Effective Pages provides the dates of issue for original and revised pages, and a listing of all pages in the handbook. Pages affected by the current revision are indicated by an asterisk(*) preceding the pages listed. LOG OF EFFECTIVE PAGES Dates of issue for original and revised pages are: Original 21 July 1983 Page Date Page Date Title 21 July 1983 Assignment Record 21 July 1983 4-1 thru 4-25 4-26 Blank 21 July 1983 21 July 1983 i thru v 21 July 1983 5-1 21 July 1983 vi Blank 21 July 1983 5-2 Blank 21 July 1983 1-1 thru 1-9 21 July 1983 5-3 thru 5-7 21 July 1983 1-10 Blank 21 July 1983 5-8 Blank 21 July 1983 2-1 21 July 1983 5-9 thru 5-25 21 July 1983 2-2 Blank 21 July 1983 2-3 thru 2-13 21 July 1983 2-14 Blank 21 July 1983 5-26 Blank 6-1 6-2 Blank 21 July 1983 21 July 1983 (0) 3-1 thru 3-9 3-10 Blank 21 July 1983 21 July 1983 6-3 thru 6-30 21 July 1983 21 July 1983 7-1 thru 7-38 21 July 1983 3-11 thru 3-18 ............... 21 July 1983 8-1 21 July 1983 Original Issue D1251-13PH-RPC-375-9/83 iii LOG OF EFFECTIVE PAGES CESSNA MODEL 172P LOG OF EFFECTIVE PAGES (Continued) iv Page 8-2 Blank 8-3 thru 8-19 Date Page 21 July 1983 21 July 1983 8-20 Blank 21 July 1983 9-1 thru 9-3 21 July 1983 9-4 Blank 21 July 1983 tems. NOTE Date Refer to Section 9 Table of Contents for supplements applicable to optional sys- Original Issue CESSNA MODEL 172P TABLE OF CONTENTS TABLE OF CONTENTS GENERAL. LIMITATIONS.. EMERGENCY PROCEDURES.. NORMAL PROCEDURES... SECTION • 1 2 3 4 5 PERFORMANCE... WEIGHT & BALANCE/ EQUIPMENT LIST AIRPLANE & SYSTEMS DESCRIPTIONS AIRPLANE HANDLING, SERVICE & MAINTENANCE 6 7 8 SUPPLEMENTS (Optional Systems Description & Operating Procedures) 9 Original Issue v/(vi blank) C CESSNA MODEL 172P SECTION 1 GENERAL SECTION 1 GENERAL TABLE OF CONTENTS Specific Loadings Three View Introduction Descriptive Data Engine Propeller Fuel Oil Maximum Certificated Weights Standard Airplane Weights Cabin And Entry Dimensions Baggage Space And Entry Dimensions . Symbols, Abbreviations And Terminology Page 1-2 1-3 1-3 1-3 1-3 1-3 1-4 1-5 1-5 1-5 1-5 1-5 1-6 General Airspeed Terminology And Symbols 1-6 Meteorological Terminology 1-6 Engine Power Terminology 1-7 Airplane Performance And Flight Planning Terminology Weight And Balance Terminology 1-7 1-8 Original Issue 21 July 1983 - 1-1 SECTION 1 GENERAL 1-2 NOTES: 1. Wing span shown with strobe lights installed. 2. Maximum height shown with nose gear depressed, all tires and nose strut properly inflated, and flashing beacon installed, 3. Wheel base length is 65". 4. Propeller ground clearance is 11¼". 5. Wing area is 174 square feet, 6. Minimum turning radius (* pivot point to outboard wing tip) is 27'-5½". -26'-11"- -11-4" * PIVOT POINT 00 * PIVOT POINT 75" MAX. 36'-0" -8'-4 1/2"- Figure 1-1. Three View CESSNA MODEL 172P 8-9 1/2" MAX. Original Issue CESSNA MODEL 172P SECTION 1 GENERAL INTRODUCTION This handbook contains 9 sections, and includes the material required to be furnished to the pilot by CAR Part 3. It also contains supplemental data supplied by Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Avco Lycoming. Engine Model Number: O-320-D2J. Engine Type: Normally-aspirated, direct-drive, air-cooled, horizontally- opposed, carburetor equipped, four-cylinder engine with 319.8 cu. in. displacement. Horsepower Rating and Engine Speed: 160 rated BHP at 2700 RPM. PROPELLER Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: 1C160/DTM7557. Number of Blades: 2. * Propeller Diameter, Maximum: 75 inches. Minimum: 74 inches. Propeller Type: Fixed pitch. FUEL Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue). 100 (Formerly 100/130) Grade Aviation Fuel (Green). NOTE Isopropyl alcohol or ethylene glycol monomethyl ether may be added to the fuel supply. Additive concentrations shall not exceed 1% for isopropyl alcohol or .15% for ethylene glycol monomethyl ether. Refer to Section 8 for additional information. Original Issue 1-3 SECTION 1 GENERAL Fuel Capacity: Standard Tanks: Total Capacity: 43 gallons. Total Capacity Each Tank: 21.5 gallons. Total Usable: 40 gallons. Long Range Tanks: Total Capacity: 54 gallons. Total Capacity Each Tank: 27 gallons. Total Usable: 50 gallons. CESSNA MODEL 172P OIL Integral Tanks: Total Capacity: 68 gallons. Total Capacity Each Tank: 34 gallons. Total Usable: 62 gallons. NOTE To ensure maximum fuel capacity when refueling and minimize cross-feeding when parked on a sloping surface, place the fuel selector valve in either LEFT or RIGHT position. Oil Specification: MIL-L-6082 Aviation Grade Straight Mineral Oil: Used when the airplane was delivered from the factory and should be used to re- plenish the supply during the first 25 hours. This oil should be drained after the first 25 hours of operation. Refill the engine and con- tinue to use until a total of 50 hours has accumulated or oil consump- tion has stabilized. MIL-L-22851 Aviation Grade Ashless Dispersant Oil: Oil conforming to Avco Lycoming Service Instruction No. 1014, and all revisions and supplements thereto, must be used after first 50 hours or oil con- sumption has stabilized. Recommended Viscosity for Temperature Range: All temperatures, use multi-viscosity oil or Above 16° C (60° F), use SAE 50 -1° C (30° F) to 32° C (90° F), use SAE 40 -18° C (0° F) to 21° C (70° F), use SAE 30 NOTE When operating temperatures overlap, use the lighter grade of oil. Oil Capacity: Sump: 7 Quarts. Total: 8 Quarts. 1-4 Original Issue CESSNA MODEL 172P SECTION 1 GENERAL MAXIMUM CERTIFICATED WEIGHTS Ramp, Normal Category: 2407 lbs. Utility Category: 2107 lbs. Takeoff, Normal Category: 2400 lbs. Utility Category: 2100 lbs. Landing, Normal Category: 2400 lbs. Utility Category: 2100 lbs. Weight in Baggage Compartment, Normal Category: Baggage Area 1 (or passenger on child's seat) - Station 82 to 108; 120 lbs. See note below. Baggage Area 2 - Station 108 to 142: 50 lbs. See note below. NOTE The maximum combined weight capacity for baggage areas 1 and 2 is 120 lbs. Weight in Baggage Compartment, Utility Category: In this category, the baggage compartment and rear seat must not be occupied. STANDARD AIRPLANE WEIGHTS Standard Empty Weight, Skyhawk: 1438 lbs. Skyhawk II: 1457 lbs. Maximum Useful Load: Skyhawk: Skyhawk II: Normal Category 969 lbs. 950 lbs. Utility Category 669 lbs. 650 lbs. CABIN AND ENTRY DIMENSIONS Detailed dimensions of the cabin interior and entry door openings are illustrated in Section 6. BAGGAGE SPACE AND ENTRY DIMENSIONS Dimensions of the baggage area and baggage door opening are illustrated in detail in Section 6. SPECIFIC LOADINGS Wing Loading: 13.8 lbs./sq. ft. Power Loading: 15.0 lbs./hp. Original Issue 1-5 SECTION 1 GENERAL SYMBOLS, ABBREVIATIONS AND TERMINOLOGY CESSNA MODEL 172P GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS KCAS KIAS KTAS A VFE VNO VNE Vs ༠ VV Knots Calibrated Airspeed is indicated airspeed corrected for position and instrument error and expressed in knots. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level. Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots. Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature. Maneuvering Speed is the maximum speed at which full or abrupt control movements may be used. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, then only with caution. Never Exceed Speed is the speed limit that may not be exceeded at any time. Stalling Speed or the minimum steady flight speed at which the airplane is controllable. Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the landing configu- ration at the most forward center of gravity. Best Angle-of-Climb Speed is the speed which results in the greatest gain of altitude in a given horizontal distance. Best Rate-of-Climb Speed is the speed which results in the greatest gain in altitude in a given time. METEOROLOGICAL TERMINOLOGY OAT Outside Air Temperature is the free air static temperature. Original Issue 1-6 CESSNA MODEL 172P Standard Tempera- ture Pressure Altitude SECTION 1 GENERAL It is expressed in either degrees Celsius or degrees Fah- renheit. Standard Temperature is 15°C at sea level pressure alti- tude and decreases by 2°C for each 1000 feet of altitude. Pressure Altitude is the altitude read from an altimeter when the altimeter's barometric scale has been set to 29.92 inches of mercury (1013 mb). ENGINE POWER TERMINOLOGY BHP RPM Static RPM Brake Horsepower is the power developed by the engine. Revolutions Per Minute is engine speed. Static RPM is engine speed attained during a full-throttle engine runup when the airplane is on the ground and stationary. AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demon- strated Crosswind Velocity Usable Fuel Unusable Fuel GPH NMPG g Original Issue Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing was actually demon- strated during certification tests. The value shown is not considered to be limiting. Usable Fuel is the fuel available for flight planning. Unusable Fuel is the quantity of fuel that can not be safely used in flight. Gallons Per Hour is the amount of fuel consumed per hour. Nautical Miles Per Gallon is the distance which can be expected per gallon of fuel consumed at a specific engine power setting and/or flight configuration. g is acceleration due to gravity. 1-7