1980 TR182 POH - Cessna Pilots Association
CESSNA 182P SKYLANE · Pilot's Operating Handbook
Overview
The Cessna T-182 Turbo Skylane Pilot's Operating Handbook (POH) provides essential information for pilots operating the T-182 model. This document includes detailed specifications, operating procedures, and performance data necessary for safe and efficient flight operations. It serves as a comprehensive guide for both new and experienced pilots, ensuring they understand the aircraft's capabilities and limitations. The handbook covers various aspects of flight, including preflight checks, emergency procedures, and performance charts, making it a vital resource for flight planning and execution.
- Maximum takeoff weight: 3,100 lbs (1,406 kg)
- Cruise speed: 145 knots
- Stall speed: 54 knots (landing configuration)
- Takeoff distance: approximately 1,600 feet
- Climb rate: about 1,000 feet per minute
Document
Source
Originally published by cessna.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 215
- File size
- 14 MB
- Publisher
- cessna.org
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 825
- Engine (hp)
- 235
- Propeller
- 2-Bladed Constant Speed
- Engine model
- O-540-L3C5D
- Max speed (kt)
- 187
- Cruise speed (kt)
- 173
- Empty weight (lb)
- 1,791
- Fuel capacity (gal)
- 92
- Rate of climb (fpm)
- 1,040
- Service ceiling (ft)
- 20,000
- Max takeoff weight (lb)
- 3,100
Performance
- Landing over 50ft
- 1,320
- Takeoff over 50ft
- 1,570
- Landing distance (ft)
- 820
- Takeoff distance (ft)
- 600
- Stall speed clean (kt)
- 54
- Stall speed landing (kt)
- 50
V-speeds
- VS1
- 54
- VSO
- 50
Weight & balance
- Useful load (lb)
- 1,321
- Max ramp weight (lb)
- 3,112
- Baggage allowance (lb)
- 200
- Basic empty weight (lb)
- 1,791
- Max landing weight (lb)
- 3,100
- Max takeoff weight (lb)
- 3,100
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
The Cessna T-182 Turbo Skylane features a maximum takeoff weight of 3,100 lbs (1,406 kg) and a useful load of approximately 1,150 lbs (521 kg). The aircraft is powered by a Lycoming IO-540-U4A5 engine, producing 235 horsepower. The cruise speed is around 145 knots, with a stall speed of 54 knots in landing configuration.
Operating Procedures
Pilots must perform a thorough preflight inspection, including checking fuel levels, oil quantity, and control surfaces. The recommended fuel type is 100LL (low lead) aviation gasoline. During engine start, ensure the mixture is set to rich and the throttle is open 1/4 inch. Follow the checklist for engine run-up before takeoff.
Performance Data
The T-182 has a takeoff distance of approximately 1,600 feet at sea level under standard conditions. The climb rate is about 1,000 feet per minute at sea level. The aircraft has a maximum range of approximately 800 nautical miles with standard fuel reserves.
Emergency Procedures
In the event of an engine failure during takeoff, the pilot should maintain control and execute a forced landing. If an engine failure occurs in flight, the pilot should establish best glide speed and look for a suitable landing area. Emergency checklists should be followed as outlined in the handbook.
Safety notes
- Always perform a thorough preflight inspection before flight.
- Ensure fuel type is 100LL aviation gasoline.
- Follow emergency procedures as outlined in the handbook.
Full document text
PILOT'S OPERATING HANDBOOK and FAA APPROVED AIRPLANE FLIGHT MANUAL THIS DOCUMENT MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES. CESSNA AIRCRAFT COMPANY 1980 MODEL TR182 Serial No. R18201454 Registration No.. N4915 THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY CAR PART 3 AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. Member of GAMA COPYRIGHT 1979 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 1 OCTOBER 1979 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON 2-7-80 SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY IN- SERTED. Dr. Kitth CESSNA AIRCRAFT COMPANY, PAWNEE DIVISION + REVISION TURBO SKYLANE RG 1980 MODEL TR182 PILOT'S OPERATING HANDBOOK REVISION 4 10 NOVEMBER 1980 B D1178R4-13PH INSERT THE FOLLOWING REVISED PAGES INTO BASIC PILOT'S OPERATING HANDBOOK " REVISION TURBO SKYLANE RG 1980 MODEL TR182 PILOT'S OPERATING HANDBOOK REVISION 3 30 JUNE 1980 D1178R3-13PH INSERT THE FOLLOWING REVISED PAGES INTO BASIC PILOT'S OPERATING HANDBOOK REVISION TURBO SKYLANE RG 1980 MODEL TR182 PILOT'S OPERATING HANDBOOK REVISION 2 28 MARCH 1980 D1178R2-13PH INSERT THE FOLLOWING REVISED PAGES INTO BASIC PILOT'S OPERATING HANDBOOK CESSNA MODEL TR182 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. 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 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 s service. ⚫FACTORY APPROVED SERVICE EQUIPMENT to provide you efficient and accurate workmanship. INE CESS 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 Service Letters and Service News Letters, published by Cessna Aircraft Company. We urge all Cessna owners 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. 1 October 1979 i PERFORMANCE- SPECIFICATIONS CESSNA MODEL TR182 PERFORMANCE SPECIFICATIONS - SPEED: Maximum at 20,000 Ft Cruise. 75% Power at 20,000 Ft . " Cruise. 75 Power at 10,000 Ft CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. 75% Power at 20,000 PL 88 Gallons Usable Fuel 75 Power at 10.000 Ft 88 Gallons Usable Fuel Maximum Range at 20,000 Ft 68 Gallons Usable Fuel Maximum Range at 10.000 Ft Gallons Usable Fuel RATE OF CLIMB AT SEA LEVEL 187 KNOTS 173 KNOTS " 158 KNOTS Range Time 825 NM 5.0 HRS Range Time 800 NM 5.1 HAS " " Range 1010 NM Time 8.1 HRS Range 1030 NM Time CERTIFICATED MAXIMUM OPERATING ALTITUDE 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: Hamp Takeoff or Landing STANDARD EMPTY WEIGHT: Turbo Skylane RG Turbo Skylane RG II MAXIMUM USEFUL. LOAD: Turbo Skylane RO Turbo Skylane RG II BAGGAGE ALLOWANCE WING LOADING: Pounds/Sq Ft POWER LOADING: Pounds/HP PUEL CAPACITY: Total OIL CAPACITY ENGINE: Turbocharged Aveo Lycoming 235 BHP at 2400 RPM PROPELLER: 2-Bladed Constant Speed, Diameter " I 8.5 HRS 1040 FPM 20,000 FT 820 FT 1570 FT 600 FT 1320 FT 54 KNOTS 50 KNOTS 3112 LBS 3100 LBS 1791 LBS " 1844 LBS 1321 LBS 1268 LBS 200 LBS 17.8 ΣΕΙ 92 GAL 9 QTS " 0-540-L3C5D 82 IN Performance with an optional 3-bladed propeller is essentially the same as shown above. い 1 October 1979 Revision 4 -10 November 1980 CESSNA MODEL R182 COVERAGE/REVISIONS/ LOG OF EFFECTIVE PAGES COVERAGE The Pilot's Operating Handbook in the airplane at the time of delivery from Cessna Aircraft Company contains information applicable to the 1980 Model R182 airplane designated by the serial number and registration number shown on the Title Page of this handbook. REVISIONS Changes and/or additions to this handbook will be covered by revisions published by Cessna Aircial Company. These ressions are distributed to all Cessna Dealers and to owners of L. 4. 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. Owners should contact their Cessna Dealer whenever the revision status of their handback is in question.
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A revision hat will extend the full length of new or revised test and/or illustrations added on new or presently existing pages. This bar will be located adjacent to the applicable revised area on the puter margin at the page. All evised pages will carry the revision number and date on the applicable paje The following Log of Effective Pages provides the dates of issue for original and revived pages, and a listing of all pages in the handbook. Pages affected by the current recision are indicated by an asterisk preceding the pages listed. LOG OF EFFECTIVE PAGES Does of issue for original and revised papes are. Original R1 Reviriun 2 1ber 1979 15 Nov 1979 Page 51 + 10 November 1980 Tule THE 14 1:4 thru 1.9 2-1 1-2 Blank 2-1 thn 2-1 26 thn 2-10 2.11 2-12 Blank 3.1 thru 3-19 3-20 Bank 4.1 thru 4.3 October 1979 1 October 1979 1 October 1979 10 November 1' 24 May 19112 1 Orinber 19179 10 November 1980 1 Oriner 19N 10 November PIND 1 De inter 1 November URO 1 Deinber 1979 28 March 1960 1 Quimber 199 1 Del 197 Eximber 1979 1 October 1979 15 Newmber 1979 1 D 1974 15 November 1974 1-3 Blank 5-1 the 5-10 וויי 1-12 thru 5-2 6-1 6-2 Blank th-1] 6-14 Blink 6-11 4--16 -17 thru -26 Blink 7-17-22 1-24 mia mami 7-24 iliru 7-36 7-17 7-411 thru 7-16 - Blink 11-1 thru 17 HI Bank הוי וידוי 4.10 411 4-12 k 4.13 thou 4-31 4.24 1979 1er 1979 H1 Novemise 1980 1-2 thr $1 1.4 Bunk 24 May 1982 Bake 16br 1979 1 Od 1979. 14 1979 24 May 18. 1 October 1979 11979 1 Cher 1970 1 1979 - 1 October 1979 11979 10 Net 190 1 October 1979 Chr Cbr 1979 Nember 1940 1 October 1964 15 Ninculer 197 In 1974 1 Cor 1929 1 Chober 1979 Chinler 1974 October 1929 maal 15 Ninmiler 1979 Cher 1974 1 Chile 1Z0- Contents for supple MOIL Heer in Section Table month applicable to optional tem 1 October 1979 Revision 4 - 24 May 1982/01177-4-13PH iii TABLE OF CONTENTS iv CESSNA MODEL R182 TABLE OF CONTENTS GENERAL. LIMITATIONS... EMERGENCY PROCEDURES... NORMAL PROCEDURES.. PERFORMANCE... WEIGHT & BALANCE/ EQUIPMENT LIST AIRPLANE & SYSTEMS DESCRIPTIONS SECTION 1 2 - 3 4 5 6 7 AIRPLANE HANDLING, SERVICE & MAINTENANCE...... 8 SUPPLEMENTS (Optional Systems Description & Operating Procedures) ....... ... 9 1 October 1979 い 1 GENERAL CESSNA MODEL TR182 SECTION 1 GENERAL TABLE OF CONTENTS Three View Introduction " " Descriptive Data Engine Propeller (2-Bladed) Propeller (3-Bladed) Fuel Oil - " SECTION 1 GENERAL 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 " 1 October 1979 Page 1-2 1-3 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 1-7 " 1-7 " 1-7 1-8 Revision 4 -10 November 1980 1-1 SECTION 1 GENERAL CESSNA MODEL TR182 1-2 * PIVOT POINT MAX. 12" -28-7 1/2"- 0 0 36-0 Figure 1-1. Three View MAX. NOTES 1. Dimension shown are based on tandard empty weight and proper nou gear and 2. Wings with strobe lights installed. 3 Maximum height shown with no gar depressed as far as possible and lushing beacon installed 4 Wheelbase length is 657 5. Proceller ground carance is 11 1/2″, 6. Wing 174 square f ! Minimum turning rather bõpivot point to outboard wing tipli is 27'-0”. * P VOT POINT 1 October 1979 CESSNA MODEL TR182 SECTION 1 GENERAL L INTRODUCTION This handbook contains 9 sections, and includes the material required .o 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: 0-540-L3C5D. Engine Type: Turbocharged, direct-drive, air-cooled. horizontally- opposed, carburetor equipped, six-cylinder engine with 541.5 cu. in. displacement. Horsepower Rating and Engine Speed: 235 rated BHP at 31 inches Hg and 2400 RPM. PROPELLER (2-BLADED) Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: B2D34C219/90DHB-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 15.8° and a high pitch setting of 31.9° (30 inch station). PROPELLER (3-BLADED) Propeller Manufacturer: McCauley Accessory Division. Propeller Model Number: B3D32C407/82NDA-3. Number of Blades: 3. Propeller Diameter, Maximum: 79 inches. Minimum: 78 inches. Propeller Type: Constant speed and hydraulically actuated, with a low pitch setting of 16.0° and a high pitch setting of 31.7° (30 inch station). FUEL Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Bluc). 100 (Formerly 100/130) Grade Aviation Fuel (Green). 1 October 1979 Revision 410 November 1980 1-3 SECTION 1 GENERAL CESSNA MODEL TR182 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. Total Capacity: 92 gallons. Total Capacity Each Tank: 46 gallons. Total Usable: 88 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 Oil Grade (Specification): MIL-L-6082 Aviation Grade Straight Mineral Oil: Use to replenish supply during first 25 hours and at the first 25-hour oil change. Continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. MIL-L-22851 Ashless Dispersant Oil: This oil must be used after first 50 hours or oil consumption has stabilized. Recommended Viscosity For Temperature Range: MIL-L-6082 Aviation Grade Straight Mineral Oil: All temperatures, use SAE 20W-50 or Above 16°C (60°F), use SAE 40 or 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 40 or SAE 30 Below -12°C (10°F), use SAE 30 MIL-L-22851 Ashless Dispersant Oil: All temperatures, use SAE 20W-50 or Above 16°C (60°F), use SAE 40 or 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 40 or SAE 30 Below -12°C (10°F), use SAE 30 Oil Capacity: Sump: 8 Quarts. Total: 9 Quarts. 1-4 1 October 1979 CESSNA MODEL TR182 SECTION 1 GENERAL MAXIMUM CERTIFICATED WEIGHTS Ramp: 3112 lbs. Takeoff: 3100 lbs. Landing: 3100 lbs. Weight in Baggage Compartment: Baggage Area "A" (or passenger on child's seat) - Station 82 to 110: 120 lbs. See note below. Baggage Area "B" Station 110 to 134: 80 lbs. See note below. NOTE The maximum combined weight capacity for baggage areas A and B is 200 lbs. STANDARD AIRPLANE WEIGHTS Standard Empty Weight, Turbo Skylane RG: 1791 lbs. Turbo Skylane RG II: 1844 lbs. Maximum Useful Load, Turbo Skylane RG: 1321 lbs. Turbo Skylane RG II: 1268 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: 17.8 lbs./sq. ft. Power Loading: 13.2 lbs./hp. 1 October 1979 1-5
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