Cessna 182P Skylane Pilot's Operating Handbook
CESSNA 182P SKYLANE · Other Documents
Overview
The Cessna 182T Skylane is a high-performance single-engine aircraft known for its reliability and versatility. This Pilot's Operating Handbook (POH) serves as a comprehensive guide for pilots operating the 182T model equipped with NAV III avionics and KAP 140 autopilot. It includes essential information on the aircraft's specifications, performance data, operational procedures, and maintenance guidelines. The 182T is designed to provide excellent performance in various flight conditions, making it suitable for both personal and commercial use. The handbook emphasizes the importance of understanding the aircraft's systems and adhering to safety protocols to ensure a safe flying experience.
- The Cessna 182T is equipped with advanced avionics and autopilot systems for enhanced navigation and control.
- Understanding performance specifications is crucial for safe operation and flight planning.
- Regular maintenance and adherence to operational guidelines are essential for aircraft safety.
Document
Source
Originally published by txwg.cap.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Other Documents
- Pages
- 386
- File size
- 5.4 MB
- Publisher
- txwg.cap.gov
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
Performance Specifications
- Maximum Speed at Sea Level: 150 knots - Cruise Speed at 80% Power (7000 ft): 145 knots - Rate of Climb at Sea Level: 924 FPM - Service Ceiling: 18,100 feet - Takeoff Performance: Ground Roll: 795 feet, Total Distance Over 50 ft Obstacle: 1514 feet - Landing Performance: Ground Roll: 590 feet, Total Distance Over 50 ft Obstacle: 1350 feet - Stall Speed (KCAS): Flaps UP: 54 KCAS, Flaps FULL: 49 KCAS.
Weight and Balance
- Maximum Weight: 3110 pounds (Ramp), 3100 pounds (Takeoff), 2950 pounds (Landing) - Standard Empty Weight: 1924 pounds - Maximum Useful Load: 1186 pounds - Baggage Allowance: 200 pounds.
Engine and Fuel
- Engine: Textron Lycoming IO-540-AB1A5, 230 BHP at 2400 RPM - Fuel Capacity: 92 gallons (usable) - Oil Capacity: 9 quarts.
Safety notes
- Warnings, cautions, and notes are used throughout the manual to highlight critical operational procedures.
- In emergencies, land as soon as possible at the nearest suitable airport.
Full document text
Member of GAMA Cessna TEXTRON AVIATION Pilot's Operating Handbook And FAA Approved Airplane Flight Manual SKYLANE Model 182T SERIAL NUMBER 8281386 NAV III Avionics - KAP 140 Autopilot REGISTRATION NUMBER N351CP Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875 This publication includes the material required to be furnished to the pilot by 14 CFR 23. COPYRIGHT © 2004 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 182TPHAUS-05 APPROVED BY FAA APPROVED UNDER FAR 21 SUBPART J The Cesana Aircraft Co. Delegation Option Authorization DOA-100129-C Wisden Holly Executive Eng DATE OF APPROVAL 03 JUNE 2004 ORIGINAL ISSUE - 3 JUNE 2004 REVISION 5-16 JULY 2015 U.S. 83254 THIS MANUAL WAS PROVIDED FOR THE AIRPLANE IDENTIFIED ON THE TITLE PAGE ON SUBSEQUENT REVISIONS SUPPLIED BY CESSNA AIRCRAFT COMPANY MUST BE PROPERLY INSERTED. Cessna Aircraft Company C CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT INTRODUCTION PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL CESSNA MODEL 182T NAV III AVIONICS OPTION - KAP 140 AUTOPILOT SERIALS 18281228 AND 18281318 THRU 18281868 AND 18281870 THRU 18281875 ORIGINAL ISSUE - 3 JUNE 2004 REVISION 5 - 16 JULY 2015 PART NUMBER: 182TPHAUS-05 |182TPHAUS-05 U.S. i/ii C 1 I CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT CONGRATULATIONS INTRODUCTION Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot's Operating Handbook has been prepared as a guide to help you get the most utility from your airplane. It contains information about your airplane's equipment, operating procedures, performance and suggested service and care. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Authorized Service Facility: . • • . • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Authorized Service Facilities worldwide. Warranty provisions and other important information are contained in the Customer Care Program Handbook supplied with your airplane. The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented to any Cessna Authorized Service Facility at the time of warranty service. 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 are available when you need them. THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNA AIRPLANES. Cessna Authorized Service Facilities have all of the current Maintenance Manuals, Illustrated Parts Catalogs and various other support publications produced by Cessna Aircraft Company. A current Cessna Authorized Service Facilities Directory accompanies your new airplane. The Directory is revised annually, and a current copy can be obtained from your nearest Cessna Authorized Service Facility. We urge all Cessna owners/operators to utilize the benefits available within the Cessna Organization. 182TPHAUS-05 U.S. iii INTRODUCTION CESSNA PERFORMANCE - SPECIFICATIONS *SPEED Maximum at Sea Level Cruise, 80% Power at 7000 Feet. . . MODEL 182T NAV III KAP 140 AUTOPILOT 150 KNOTS 145 KNOTS CRUISE - Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. 80% Power at 7000 Feet.. 87 Gallons Usable Fuel.. 75% Power at 8000 Feet. 87 Gallons Usable Fuel. . Max Range at 10,000 Feet, 55% Power 87 Gallons Usable Fuel. .... RATE OF CLIMB AT SEA LEVEL: . SERVICE CEILING: . . . TAKEOFF PERFORMANCE: Range - 773 NM Time - 5.4 HOURS . Range - 813 NM Time - 5.8 HOURS ... Range - 930 NM Time - 7.6 HOURS .924 FPM 18,100 FEET Ground Roll ……………… 795 FEET Total Distance Over 50 Foot Obstacle. 1514 FEET LANDING PERFORMANCE: Ground Roll . . . . 590 FEET Total Distance Over 50 Foot Obstacle. 1350 FEET STALL SPEED (KCAS): Flaps UP, Power Idle Flaps FULL, Power Idle (Continued Next Page) .54 KCAS .49 KCAS liv U.S. 182TPHAUS-05 CESSNA INTRODUCTION MODEL 182T NAV III KAP 140 AUTOPILOT PERFORMANCE - SPECIFICATIONS (Continued) MAXIMUM WEIGHT: Ramp. Takeoff. Landing. STANDARD EMPTY WEIGHT: MAXIMUM USEFUL LOAD: BAGGAGE ALLOWANCE: WING LOADING:. POWER LOADING: . . . FUEL CAPACITY: 3110 POUNDS 3100 POUNDS . 2950 POUNDS 1924 POUNDS 1186 POUNDS 200 POUNDS 17.8 lbs/sq. ft. 13.5 lbs/HP . 92 GALLONS OIL CAPACITY: ENGINE: Textron Lycoming. 230 BHP at 2400 RPM 9 QUARTS .IO-540-AB1A5 PROPELLER: 3-Bladed, Constant Speed, Diameter. . . . . . 79 INCHES NOTE *Speed performance and range are shown for an airplane equipped with the standard wheel and brake fairings. These fairings increase the speeds approximately 3 knots over an airplane without the fairings. The above performance figures are based on the indicated weights, standard atmospheric conditions, level, hard-surfaced dry runways and no wind. They are calculated values derived from flight tests conducted by Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes and numerous factors affecting flight performance. 182TPHAUS-05 U.S. INTRODUCTION CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT COVERAGE The Pilot's Operating Handbook (POH) in the airplane at the time of delivery from Cessna Aircraft Company contains information applicable to the Model 182T Nav III airplanes by serial number and registration number shown on the Title Page. This POH is applicable to 182T airplanes, Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875, equipped with the NAV III Avionics Option and Bendix/King KAP 140 Autopilot. All information is based on data available at the time of publication. This POH consists of nine sections that cover all operational aspects of
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a standard equipped airplane. Section 9 contains the supplements which provide amended operating limitations, operating procedures, performance data and other necessary information for airplanes conducting special operations for both standard and optional equipment installed in the airplane. Supplements are individual documents, and may be issued or revised without regard to revision dates which apply to the POH itself. These supplements contain a Log of Effective Pages, which should be used to determine the status of each supplement. Ivi U.S. 182TPHAUS-05 C CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT ORIGINAL ISSUE AND REVISIONS INTRODUCTION This Pilot's Operating Handbook and FAA Approved Airplane Flight Manual is comprised of the original issue and any subsequent revisions. To make sure that information in this manual is current, the revisions must be incorporated as they are issued. As revisions are issued, they will be noted in the Log of Effective Pages. The part number of this manual has also been designed to further aid the owner/operator in determining the revision level of any POH. Refer to the example below for a breakdown: 182T PHAUS -00 Revision Level (Original Issue) Manual (Pilot's Operating Handbook Nav III KAP 140 Autopilot, U.S.) (Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875) Airplane Model - (182T) It is the responsibility of the owner to maintain this POH in a current status when it is being used for operational purposes. Owners should contact a Cessna Authorized Service Facility whenever the revision status of their POH is in question. Revisions are distributed to owners of U.S. Registered aircraft according to FAA records at the time of revision issuance, and to Internationally Registered aircraft according to Cessna Owner Advisory records at the time of issuance. Revisions should be read carefully upon receipt and incorporated in this POH. 182TPHAUS-05 U.S. vii INTRODUCTION REVISION FILING INSTRUCTIONS REGULAR REVISIONS CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT Pages to be removed or inserted in the Pilots' Operating Handbook and FAA Approved Airplane Flight Manual are determined by the Log of Effective Pages located in this section. This log contains the page number and revision level for each page within the POH. As revisions to the POH occur, the revision level on effected pages is updated. When two pages display the same page number, the page with the latest revision level shall be inserted into the POH. The revision level on the Log Of Effective Pages shall also agree with the revision level of the page in question. TEMPORARY REVISIONS Under limited circumstances, temporary revisions to the POH may be issued. These temporary revisions are to be filed in the applicable section in accordance with filing instructions appearing on the first page of the temporary revision. Temporary Revisions will remain current until they have either been incorporated into the next POH revision or another temporary revision has been issued that supersedes that temporary revision. Each temporary revision is issued with a current List of Temporary Revisions that is to be inserted opposite the first page of the Log of Effective Pages in the front of the POH and will supersede any previously issued List of Temporary Revisions. This list is used to track the status of temporary revisions issued against this POH and is to be removed and discarded at the next revision to the POH. Removal of temporary revisions from the POH is accomplished per the removal instructions on each temporary revision. viii U.S. 182TPHAUS-05 C C CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT IDENTIFYING REVISED MATERIAL INTRODUCTION A bar will extend the full length of deleted, new, or revised text added on new or previously existing pages. This bar will be located adjacent to the applicable text in the margin on the left side of the page. A bar in the footer will indicate a revision to the header/footer, a new page, format or spelling/grammar changes and/or that information has slipped to or from that page. A bar located adjacent to the figure number in the margin on the left side of the page will be used to indicate that the figure number only has changed. An asterisk located at the end of a figure number will be used to indicate that an illustration has been revised or is all new material (Ex: Figure 3-4*). All revised pages will carry the revision number opposite the page number on the applicable page. A list of revisions is located at the beginning of the Log Of Effective Pages. 182TPHAUS-05 U.S. ix INTRODUCTION CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT WARNINGS, CAUTIONS AND NOTES Throughout the text, warnings, cautions and notes pertaining to airplane handling and operations are utilized. These adjuncts to the text are used to highlight or emphasize important points. OPERATING WARNING PROCEDURES, TECHNIQUES, ETC., WHICH CAN RESULT IN PERSONAL INJURY OR LOSS OF LIFE IF NOT CAREFULLY FOLLOWED. CAUTION OPERATION PROCEDURES, TECHNIQUES, ETC., WHICH CAN RESULT IN DAMAGE TO EQUIPMENT IF NOT CAREFULLY FOLLOWED. NOTE An operating procedure, technique, etc., which is considered essential to emphasize. LAND AS SOON AS POSSIBLE Land at the nearest suitable airport. Unless otherwise specified, use Normal Procedures for Approach, Before Landing, and Landing. Extreme situations can require an off-airport landing. Primary consideration is safety of occupants. LAND AS SOON AS PRACTICAL Land at a suitable airport. Unless otherwise specified, use Normal Procedures for Approach, Before Landing, and Landing. The primary consideration is the urgency of the emergency or abnormal situation. Continuing to the destination or an alternate with appropriate service facilities can be an option. 1x U.S. 182TPHAUS-05 CESSNA INTRODUCTION MODEL 182T NAV III KAP 140 AUTOPILOT LOG OF EFFECTIVE PAGES Use this page to determine the currency and applicability of your POH. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages listed under the Page Number column. Revision Level Original Issue Date of Issue 3 June 2004 Revision Level Revision 3 Date of Issue 19 July 2005 Revision 1 24 June 2004 Revision 4 22 December 2005 Revision 2 27 June 2005 Revision 5 16 July 2015 Page Number Page Status Revision Number * Title Revised Assignment Record Revised * i/ii thru xiii/xiv * xv/xvi Revised Added 52 505 5 · 1-1/1-2 thru 1-28 Revised * 1-29/1-30 Added 2-1/2-2 thru 2-22 Revised * 2-23 thru 2-26 Added * 3-1 thru 3-36 Revised * 3-37/3-38 Added * 4-1 thru 4-50 Revised * 4-51 thru 4-52 Deleted 55 55 55 55 5 * 5-1/5-2 thru 5-36 Revised * 5-37/5-30 Added * 6-1/6-2 thru 6-25/6-26 Revised 55 50 182TPHAUS-05 (Continued Next Page) U.S. ✗. INTRODUCTION CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT LOG OF EFFECTIVE PAGES (Continued) Page Number Page Revision Status Number * 7-1 thru 7-76 Revised * 7-77 thru 7-83/7-84 Added 55 * 8-1 thru 8-24 • 8-25/8-26 * 9-1/9-2 Revised Added Revised 5 5 1040 5 10 FOR APPROVED BY Tall Pe Randy Shields, Lead ODA Administrator Cessna Aircraft Company Organization Delegation Authorization ODA-100129-CE FAA Approved Under 14 CFR Part 183 Subpart D DATE OF APPROVAL 7-16-2015 ■xii U.S. 182TPHAUS-05 C C CESSNA MODEL 182T NAV III KAP 140 AUTOPILOT INTRODUCTION ISERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this manual. This list contains only those Service Bulletins that are currently active. Revision Incorporated Incorporated in Airplane Number Title Airplane Serial Effectivity SB08-34-03 Forward Looking Terrain Avoidance 18281228 and 5 18281318 thru (FLTA) Alert Over The 18281868 and Open Ocean/Sea 18281870 thru 18281875 MK206-34-08 Garmin G1000 GPS/18281228 and WAAS Installation 5 18281318 thru 18281868 and 18281870 thru 18281875 SB09-34-06 Garmin G1000 System 18281228 and 5 Software Upgrade to 18281318 thru 563.14 18281868 and 18281870 thru 18281875 182TPHAUS-05 U.S. xiii/xiv
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