Model 162 SERIAL NUMBER Serials 16200001 and On REGISTRATION NUMBER This publication includes the material required to be furnished to the pilot by ASTM F2245. COPYRIGHT © 2009 ORIGINAL ISSUE - 22 JULY 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA REVISION 4 - 21 OCTOBER 2011 162PHUS-04 U.S. CESSNA INTRODUCTION MODEL 162 GARMIN G300 PILOT’S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT CESSNA MODEL 162 SERIALS 16200001 AND ON ORIGINAL ISSUE - 22 JULY 2009 REVISION 4 - 21 OCTOBER 2011 PART NUMBER: 162PHUS-04 162PHUS-04 U.S. i/ii CESSNA INTRODUCTION MODEL 162 GARMIN G300 CONGRATULATIONS 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 Service Station: • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Care 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 your local Cessna Service Station 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 Service Stations have all of the current Maintenance Manuals, Illustrated Parts Catalogs and various other support publications produced by Cessna Aircraft Company. A Cessna Service Station locator is available at www.cessnasupport.com. We urge all Cessna owners/operators to utilize the benefits available within the Cessna Organization. 162PHUS-01 U.S. iii INTRODUCTION CESSNA MODEL 162 GARMIN G300 PERFORMANCE - SPECIFICATIONS *SPEED: Maximum at Sea Level . . . . . . . . . . . . . . 118 KNOTS (218.5 km/hr) Cruise, 69% Power at 6000 Feet. . . . . . . 109 KNOTS (201.9 km/hr) CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 30 minutes reserve. RANGE: 69% Power at 6000 Feet. . . . . . . . . . . . . . . . . . . . .Range - 336 NM 24 Gallons Usable Fuel . . . . . . . . . . . . . . . . . . . Time - 3.16 HOURS RATE OF CLIMB AT SEA LEVEL . . . . . . . . . . . 880 FPM (268.2 mpm) SERVICE CEILING . . . . . . . . . . . . . . . . . . . . 14,625 FEET (4457.7 m) TAKEOFF PERFORMANCE AT SEA LEVEL: Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . .640 FEET (195.1 m) Total Distance Over 50 Foot Obstacle. . . . . . .1138 FEET (346.9 m) LANDING PERFORMANCE AT SEA LEVEL: Ground Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . .671 FEET (204.6 m) Total Distance Over 50 Foot Obstacle. . . . . . .1369 FEET (417.3 m) STALL SPEED: Flaps UP, Power Idle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41 KIAS Flaps FULL, Power Idle. . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 KIAS NOTE * Speed performance is shown for airplanes not equipped with the optional wheel fairings. Airplanes equipped with optional wheel fairings will notice an increase in speeds by approximately 2 knots. There is a corresponding difference in range, while all other performance figures are unchanged when speed fairings are installed. The above performance figures are based on airplane weights at 1320 pounds (598.7 kg), 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. (Continued Next Page) iv U.S. 162PHUS-03 CESSNA INTRODUCTION MODEL 162 GARMIN G300 PERFORMANCE - SPECIFICATIONS (Continued) MAXIMUM WEIGHT: Ramp. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1324 POUNDS (600.5 kg) Takeoff. . . . . . . . . . . . . . . . . . . . . . . . . . . 1320 POUNDS (598.7 kg) Landing . . . . . . . . . . . . . . . . . . . . . . . . . . 1320 POUNDS (598.7 kg) Maximum Empty Weight . . . . . . . . . . . . . . 894 POUNDS (405.5 kg) STANDARD EMPTY WEIGHT. . . . . . . . . . . . 834 POUNDS (378.3 kg) MAXIMUM USEFUL LOAD . . . . . . . . . . . . . . 490 POUNDS (222.3 kg) BAGGAGE ALLOWANCE . . . . . . . . . . . . . . . . 50 POUNDS (22.68 kg) WING LOADING . . . . . . . . . . . . . . . . . . . 11.0 lbs/sq. ft. (53.7 kg/sq m) POWER LOADING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13.2 lbs/HP FUEL CAPACITY (Usable) . . . . . . . . . . . . . . . . . 24 GALLONS (90.8 l) OIL CAPACITY (Sump) . . . . . . . . . . . . . . . . . . . . . . 5 QUARTS (4.73 I) ENGINE: Teledyne Continental Motors . . . . . . . . . . . . . . . . . . . O-200D 100 BHP at 2750 RPM PROPELLER: Fixed Pitch, Diameter . . . . . . . . . . . . . . . . . . . .67 INCHES (1.70 m) 162PHUS-04 U.S. v INTRODUCTION CESSNA MODEL 162 GARMIN G300 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 162 airplanes by serial number and registration number shown on the Title Page. This POH is applicable to Model 162 airplanes, Serials 16200001 and On, equipped with Garmin G300 Integrated Cockpit System. All information is based on data available at the time of publication. This POH consists of nine sections that cover all operational aspects of 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. vi U.S. 162PHUS-04 CESSNA INTRODUCTION MODEL 162 GARMIN G300 ORIGINAL ISSUE AND REVISIONS This Pilot’s Operating Handbook 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: 162 PHUS -00 Revision Level (Original Issue) Manual (Pilot’s Operating Handbook, U.S.) (Serials 16200001 and On) Airplane Model - (162) 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 Service Station 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. 162PHUS-00 U.S. vii INTRODUCTION CESSNA MODEL 162 GARMIN G300 REVISION FILING INSTRUCTIONS REGULAR REVISIONS Pages to be removed or inserted in the Pilots’ Operating Handbook 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. 162PHUS-00