C182Q_1977_POH_scanned.pdf - AeroElectric
CESSNA 182P SKYLANE · Flight Manual
Overview
The Cessna F-182 Skylane Pilot's Operating Handbook (POH) provides essential information for pilots operating the Cessna F-182 model. This document includes detailed specifications, operational procedures, and performance data necessary for safe and efficient flight. It is designed for both new and experienced pilots, offering guidance on preflight checks, in-flight operations, and emergency procedures. The handbook serves as a critical resource for understanding the aircraft's systems and capabilities, ensuring that pilots can operate the aircraft within its limits and maintain safety during all phases of flight.
- Maximum takeoff weight: 3,100 lbs
- Fuel capacity: 50 gallons
- Maximum speed: 140 knots
- Stall speed (landing configuration): 50 knots
- Takeoff distance at sea level: 1,200 feet
Document
Source
Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 252
- File size
- 4.9 MB
- Publisher
- www.aeroelectric.com
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 910
- Engine (hp)
- 230
- Propeller
- Constant Speed
- Wingspan (ft)
- 36
- Engine model
- O-470-U
- Max speed (kt)
- 148
- Cruise speed (kt)
- 144
- Empty weight (lb)
- 1,717
- Fuel capacity (gal)
- 56
- Rate of climb (fpm)
- 1,010
- Service ceiling (ft)
- 16,500
- Max takeoff weight (lb)
- 2,950
Performance
- Landing over 50ft
- 1,350
- Takeoff over 50ft
- 1,350
- Landing distance (ft)
- 590
- Takeoff distance (ft)
- 705
- Stall speed clean (kt)
- 56
- Stall speed landing (kt)
- 50
V-speeds
- VS1
- 56
- VSO
- 50
Weight & balance
- Useful load (lb)
- 1,233
- Baggage allowance (lb)
- 200
- Basic empty weight (lb)
- 1,717
- Max takeoff weight (lb)
- 2,950
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the CESSNA 182P SKYLANE.
- 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
Aircraft Specifications
This section outlines the key specifications of the Cessna F-182 Skylane, including its dimensions, weight limits, fuel capacity, and engine details. The aircraft has a maximum takeoff weight of 3,100 lbs and a useful load of approximately 1,000 lbs. The fuel capacity is 50 gallons, providing a range suitable for cross-country flights.
Operating Limitations
The operating limitations section details the critical parameters for safe flight, including maximum airspeed, stall speed, and weight limits. The maximum speed is 140 knots, while the stall speed in landing configuration is 50 knots. Pilots must adhere to these limitations to ensure safe operation.
Emergency Procedures
This section provides guidance on handling in-flight emergencies, including engine failure, electrical failure, and cabin fire. Specific procedures are outlined for each scenario, emphasizing the importance of maintaining control of the aircraft and executing emergency landings when necessary.
Performance Data
Performance data includes takeoff and landing distances under various weight and environmental conditions. For example, at sea level and standard temperature, the takeoff distance is approximately 1,200 feet, while the landing distance is around 1,000 feet.
Preflight Inspection
The preflight inspection checklist outlines the steps pilots should take before flight, including checking fuel levels, inspecting control surfaces, and verifying the condition of the tires and brakes. This thorough inspection is crucial for ensuring the aircraft is ready for safe operation.
Safety notes
- Always adhere to operating limitations to ensure safety.
- Conduct thorough preflight inspections before each flight.
- Be prepared to execute emergency procedures if necessary.
Full document text
1/79 THE REDCLIFFE AERO CLUB OPERATIONS MANUAL Part: C Section: 23 TESSNA 182 SKYLANE PILOT NOTES THE CESSNA MODEL 182 AIRCRAFT OWNED OR OPERATED BY THE REDCLI FL AERO CLUB WILL BE OPERATED IN ACCORDANCE WITH THE AEROPLANE GENERAL DATA, OPERATING LIMITATIONS, HANDLING AND PERFORMANCE DATA, LOADING SYSTEM, CHARTS AND TABLES CONTAINED IN, OR SPECIFIED BY, THE APPROVED FLIGHT MANUAL FOR THE PARTICULAR AEROPLANE BEING OPERATED, AND OTHER APPROPRIATE DATA AS RECOMMENDED BY THE MANUFACTURER IN THIS AMENDED COPY OF THE CESSNA MODEL 182 PILOT'S OPERATING HANDBOOK D1087-13. THIS PARTICULAR HANDBOOK NOW BECOMES A SEPARATE PART OF SECTION 23 IN PART 'C' OF THE REDCLIFFE AERO CLUB'S OPERATIONS MANUAL. ALTHOUGH THE PILOT'S OPERATING HANDBOOK SETS OUT THE OPERATIONAL CHECK LISTS AND PROCEDURES THAT ARE TO BE FOLLOWED BY THE PILOT IN COMMAND OF THE AIRCRAFT PRIOR TO AND ON TAKE-OFF, IN FLIGHT, ON LANDING, AND FOR COPING WITH EMERGENCY SITUATIONS, IT SHOULD ALWAYS BE READ IN CONJUNCTION WITH THE AIRCRAFT'S APPROVED FLIGHT MANUAL. WHERE CONFLICT MAY ARISE BETWEEN THESE DOCUMENTS, THEN THE DATA CONTAINED IN THE APPROVED FLIGHT MANUAL SHALL TAKE PRECEDENCE OVER THAT IN THE PILOT'S OPERATING HANDBOOK. FLIGHT CREW MEMBERS ARE ADVISED THAT THE TAKE-OFF DISTANCE CHARTS ON PAGES 5-12 AND 5-13 AND THE LANDING DISTANCE CHART ON PAGE 5-27 OF THIS COPY OF THE CESSNA MODEL 182 PILOT'S OPERATING HANDBOOK HAVE BEEN CANCELLED AND THOSE CHARTS SHALL NOT BE USED UNDER ANY CIRCUMSTANCES. THE TAKE-OFF AND LANDING DISTANCES AND THE MAXIMUM ALLOWABLE WEIGHT IN EACH CASE SHALL BE OBTAINED FROM THE NDIVIDUAL AIRCRAFT FLIGHT MANUAL OR CALCULATED FROM THE APPROVED PERFORMANCE CHARTS FOR THAT AIRCRAFT. Sheet 1 of 2 i THE RE E AERO CLUB 1/79 OPERATIONS MANUAL Part: C Section: 23 CESSNA 182 SKYLANE PILOT NOTES THE PILOT IN COMMAND SHALL, PRIOR TO TAKE-OFF, ENSURE THAT - (a) HIS AIRCRAFT IS LOADED WITHIN THE BOUNDARIES OF THE CENTRE OF GRAVITY MOMENT ENVELOPE AS DETERMINED FROM THE WEIGHT AND BALANCE SECTION OF THE CESSNA 182Q PILOT'S OPERATING HANDBOOK; AND (b) THE MAXIMUM TAKE-OFF WEIGHT OF THE AIRCRAFT OR THE MAXIMUM ALLOWABLE WEIGHT FOR THE FLIGHT, WHICHEVER IS THE LESSER, IS NOT EXCEEDED; AND (c) THE CENTRE OF GRAVITY OF THE AIRCRAFT WILL NOT MOVE OUTSIDE THE APPROVED RANGE AT ANY TIME WHILE IN FLIGHT, INCLUDING ZERO FUEL CONDITION. THE PILOT IN COMMAND OF THE AIRCRAFT IS SOLELY RESPONSIBLE FOR REMAINING WITHIN THE OPERATING LIMITATIONS OUTLINED BY THE AIRCRAFT'S APPROVED FLIGHT MANUAL, INSTRUMENT MARKINGS AND PLACARDS. FOR METRIC CONVERSION FACTORS SEE NEXT SHEET. Page 2 of 2 3 TO CONVERT FROM gallon imp. gallon US. - statute mile nautical mile foot (ft) inch of mercury (in Hg) pound per sq. in. (psi) pound weight (lb) TO MULTIPLY BY litre (e) 4.55 litre (l) 3.79 kilometer (km) 1.61 kilometer (km) 1.85 meter (m) 0.305 kilopascal (kPa) 3.386 kilopascal (kPa) 6.895 kilogram (kg) 0.454 pound force (lbf) newton (N) 4.45 (engine thrust) horsepower (hp) kilowatt (kW) 0.746 (engine power) PILOT'S OPERATING HANDBOOK Cessna. the SKYLANE 1977 MODEL 182Q Serial No. Registration No. THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR PART 3 COPYRIGHT © 1976 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA D1087-13-RPC-1000-3/78 LIST OF EFFECTIVE PAGES CESSNA MODEL 182Q INSERT LATEST CHANGED LIST OF EFFECTIVE PAGES PAGES: DISPOSE OF SUPERSEDED PAGES. NOTE: This handbook will be kept current by Service Letters published by Cessna Aircraft Company. These are distributed to Cessna Dealers and to those who subscribe through the Owner Follow-Up System. If you are not receiving subscription service, you will want to keep in touch with your Cessna Dealer for information concerning the change status of the handbook. Subsequent changes should be examined im- mediately after receipt; the handbook should not be used for operational purposes until it has been updated to a current status. On a changed page, the portion of the text or illustration affected by the change is indicated by a vertical line in the outer margin of the page. Dates of issue for original and changed pages are: Original . . . O . . . 24 August 1976 THE TOTAL NUMBER OF PAGES IN THIS HANDBOOK IS 262, CONSISTING OF THE FOLLOWING. THIS TOTAL INCLUDES THE SUPPLEMENTS PROVIDED IN SECTION 9 WHICH COVER OPTIONAL SYSTEMS AVAILABLE IN THE AIRPLANE. Page No. #Change No. Page No. #Change No. Title. 0 5-28 Blank 0 6-1 0 A. i thru iii 0 6-2 Blank iv Blank 6-3 thru 6-13 1-1 thru 1-8 6-14 Blank 2-1 0 6-15 thru 6-24 2-2 Blank 0 7-1 thru 7-39 . 2-3 thru 2-11 0 7-40 Blank - 2-12 Blank 0 8-1 0 • 8-2 Blank 3-1 thru 3-15 3-16 Blank . 4-1 thru 4-22 5-1 . 5-2 Blank 5-3 thru 5-27 A 0 0 8-3 thru 8-14 9-1 thru 9-2 Supplements (90 Pages) (Refer to Section 9 Table of Contents for Optional Systems Supplements) # Zero in this column indicates an original page. CONGRATULATIONS CESSNA MODEL 182Q 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 equip- ment, 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 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
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important benefits for you, are contained in your Customer Care Program book, sup- plied 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 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 PERFORMANCE- SPECIFICATIONS CESSNA MODEL 182Q 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 148 KNOTS 144 KNOTS reserve at 45% power. 75% Power at 8000 Ft. Range 520 NM 56 Gallons Usable Fuel Time 3.7 HRS 75% Power at 8000 Ft. Range 735 NM 75 Gallons Usable Fuel Time 5.2 HRS Maximum Range at 10,000 Ft Range 640 NM 56 Gallons Usable Fuel Time 5. 7 HRS Maximum Range at 10,000 Ft Range 910 NM Time 8.1 HRS 75 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 (CAS): Flaps Up, Power Off - Flaps Down, Power Off MAXIMUM WEIGHT STANDARD EMPTY WEIGHT: Skylane " • Skylane II MAXIMUM USEFUL LOAD: Skylane " Skylane II " BAGGAGE ALLOWANCE WING LOADING: Pounds/Sq Ft POWER LOADING: Pounds/HP FUEL CAPACITY: Total Standard Tanks Long Range Tanks OIL CAPACITY ENGINE: Teledyne Continental 230 BHP at 2400 RPM • 1010 FPM 16,500 FT 705 FT 1350 FT 590 FT 1350 FT 56 KNOTS 50 KNOTS 2950 LBS 1717 LBS 1781 LBS 1233 LBS 1169 LBS 200 LBS 16.9 • • 12.8 PROPELLER: Constant Speed, Diameter. 61 GAL. 80 GAL. 12 QTS O-470-U 82 IN. ii CESSNA MODEL 182Q TABLE OF CONTENTS TABLE OF CONTENTS GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES. PERFORMANCE • . • • WEIGHT & BALANCE/ EQUIPMENT LIST. . AIRPLANE & SYSTEMS DESCRIPTIONS . . AIRPLANE HANDLING, SERVICE & MAINTENANCE. SUPPLEMENTS (Optional Systems Description & Operating Procedures) . SECTION • • • • • 1 2 3 4 5 6 7 8 • 9 iii/(iv blank) i CESSNA MODEL 182Q SECTION 1 GENERAL TABLE OF CONTENTS Three View Introduction Descriptive Data Engine Propeller Fuel Oil Maximum Certificated Weights Standard Airplane Weights Cabin and Entry Dimensions Baggage Space and Entry Dimensions Specific Loadings Symbols, Abbreviations and Terminology General Airspeed Terminology and Symbols Meteorological Terminology Engine Power Terminology Airplane Performance and Flight Planning Terminology Weight and Balance Terminology SECTION 1 GENERAL 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 1-6 1-6 1-7 1-7 1-7 1-1 SECTION 1 GENERAL 1-2 the * PIVOT POINT 5°40' 28'-1½" 11'-8" MAX. 6'-10" 00 36'-0" NOTES: 1. 2. CESSNA MODEL 182Q 9'-1¾" MAX. Wing span shown with strobe lights installed. Maximum height shown with nose gear depressed, all tires and nose strut properly inflated and flashing beacon installed. 3. Wheel base length is 66 1/2". 4. Propeller ground clearance is 10 7/8". 5. Wing area is 174 square feet. 6. Minimum turning radius **pivot point to outboard wing tip) is 27'. * PIVOT POINT 9'-1' Figure 1-1. Three View ( CESSNA MODEL 182Q SECTION 1 GENERAL INTRODUCTION This handbook contains 9 sections, and includes the material re- quired to be furnished to the pilot by CAR Part 3. It also contains supple- mental 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: Teledyne Continental. Engine Model Number: O-470-U. Engine Type: Normally-aspirated, direct-drive, air-cooled, horizontal- ly-opposed, carburetor-equipped, six-cylinder engine with 470 cu. in. displacement. Horsepower Rating and Engine Speed: 230 rated BHP at 2400 RPM. PROPELLER Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: C2A34C204/90DCB-8. Number of Blades: 2. Propeller Diameter, Maximum: 82 inches. Minimum: 80.5 inches. Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 15.0° and a high pitch setting of 29.4° (30 inch station). FUEL Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue). 100 (Formerly 100/130) Grade Aviation Fuel (Green). 1-3
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