January 2012Beginning With Serial # T18209056

M O D E L T 1 8 2 T

Initial

Specification &Description

Exhibit “A”

S P E C I F I C AT I O N A N D D E S C R I P T I O N

E X H I B I T “ A ”

J A N U A R Y 2 0 1 2

B E G I N N I N G W I T H S E R I A L # T 1 8 2 0 9 0 5 6

Copyright 2012 Cessna Aircraft Company

Cessna Single Engine Piston Aircraft2625 S. Hoover Rd.

Wichita, Kansas 67215

January 2012

1

I N T R O D U C T I O N

This document is published for the purpose of providinggeneral information for the evaluation of design, per-formance and equipment of the Cessna Turbo Skylane.Should more information be required, please contact:

Cessna Aircraft CompanySingle Engine Piston Aircraft2625 S. Hoover Rd.Wichita, Kansas 672151-800-4-CESSNAwww.se.cessna.com

This document supersedes all previous Specificationand Description documents and describes only theTurbo Skylane Model T182T, its powerplant and equip-ment. Also included are the warranties applicable to theTurbo Skylane Model T182T aircraft, the TextronLycoming TIO-540-AK1A engine, the McCauley pro-peller and the OEM-installed Bendix/King and Garminavionics. In the event of any conflict or discrepancybetween this document and the basic purchase agree-

ment, the basic purchase agreement language shallgovern. Due to the time span between the date of thisSpecification and Description and the scheduled deliverydate of the aircraft, Cessna reserves the right to revisethe “Specification” whenever occasioned by productimprovements, government regulations or other goodcause.

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January 2012

TA B L E O F C O N T E N T SSection Page

1. General Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31.1 Certification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31.2 Approximate Dimensions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .31.3 Design Weights and Capacities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .6

2. Performance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

3. Powerplant & Accessories . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

4. Skylane Equipment List . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

5. Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

6. Electrical Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

7. Engine Indicating System (Electronic) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

8. Environmental . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

9. Exterior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

10. Exterior Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

11. Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

12. Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

13. Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

14. Interior Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

15. Exterior Striping Options . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

16. Training . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

17. Limited Warranties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1417.1 Cessna’s Limited Warranty - Single Engine Piston . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1417.2 Aircraft Paint and Graphics - Single Engine Piston Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1417.3 Textron Lycoming Warranty (Limited) New Reciprocating Aircraft Engines . . . . . . . . . . . . . . . . . . . . . .1517.4 McCauley Propeller Systems Standard Limited Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1617.5 Bendix/King Equipment Retail Warranty Statement For Cessna

Aircraft Company Single Engine Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1717.6 Garmin Avionics Installed in Single Engine Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .17

FIGURE I — SKYLANE EXTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4FIGURE II — SKYLANE INTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5FIGURE III — SKYLANE INSTRUMENT PANEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

January 2012

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1 . G E N E R A L D E S C R I P T I O N

All information herein applies to the Turbo Skylane(Model T182T). The Skylane aircraft is an all-metal, sin-gle-engine piston, high-wing monoplane with a four-per-son seating capacity including a crew of one or two.Suitable allowance for luggage is provided.

1.1 Certification

The Model T182T is certified to the requirements of U.S.FAA Federal Aviation Regulation Part 23 throughamendment 23-6, including day, night, VFR and IFR.

1.2 Approximate Dimensions

Overall Height . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 ft 4 in (2.84m)Overall Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 ft (8.84m)

Wing

Span (overall) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 36 ft (10.97m)Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 174 sq ft (16.2sq m)

Cabin

Height (max) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48.5 in (1.23m)Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42 in (1.07m)Length (firewall to aft baggage bulkhead) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 134 in (3.40m)

Cabin Door

Height (front) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .41 in (1.04m)Height (rear) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .38.5 in (.98m)Width (top) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .32 in (.81m)Width (bottom) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .36.5 in (.93m)

Baggage Door

Height (front) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .22 in (.56m)Height (rear) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20.5 in (.52m)Width . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .15.8 in (.40m)

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January 2012

FIGURE I — SKYLANE EXTERIOR DIMENSIONS

9’ -4”

36’ -0”

29’ -0”

1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d )

11’ -8”

9’ -0” Max

January 2012

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FIGURE II — SKYLANE INTERIOR DIMENSIONS

1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d )

68.75 65.25

33.00 42.00 48.50

*34.00**41.50

*36.00**42.50

*31.00**34.50

Tiedown Rings(10 Standard)

Firewall

Firewall

Face ofInstrumentPanel

Code

* Cabin Floor** Lower Window Line

Baggage Shelf

48.00

58.75 48.25

13.00

Rear Wall of Cabin

ForwardDoorpostBulkhead

RearDoorpostBulkhead

Cabin Height Dimensions

Cabin Width Dimensions

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1 . G E N E R A L D E S C R I P T I O N ( C o n t i n u e d )

1.3 Design Weight and Capacities

Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,112 lbs (1,412 kg)

Maximum Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3,100 lbs (1,406 kg)

Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,950 lbs (1,338 kg)

Standard Empty Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2,095 lbs (950 kg)

Maximum Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,030 lbs (467 kg)

Baggage Allowance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .200 lbs (91 kg)

Fuel Capacity

Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .92 gal (348.2 L)

Total Useable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .87 gal (329.3 L)

Total Capacity each Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .46 gal (174.1 L)

Total Useable Capacity each Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .43.5 gal (164.6 L)

Oil Capacity

Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 qts (7.5 L)

Total Capacity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9 qts (8.5 L)

January 2012

January 2012

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2 . P E R F O R M A N C E

Maximum Operating Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20,000 ft

Takeoff Distance S.L. (Ground Roll) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .775 ft

Takeoff Distance S.L. (To Clear 50ft. Obstacle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1385 ft

Max Climb Rate S.L. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1,040 fpm

Max Speed (20,000 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .176 kts / 203 mph

Max Range and Endurance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .971 nm / 8.9 hrs

Cruise Speed (88% pwr at 12,500 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .159 kts / 183 mph

Cruise Range and Endurance (88% pwr at 12,500 ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .615 nm / 4.0 hrs

Landing Distance (Ground Roll) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .590 ft

Landing Distance (To Clear 50 ft Obstacle) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1350 ft

All estimated performance data are based on airplaneweights at 3,100 pounds; standard atmospheric condi-tions; level, hard surface, dry runways; and no wind.They are calculated values derived from flight tests con-

ducted by Cessna Aircraft Company under carefully doc-umented conditions and will vary with individual air-planes, pilots, and numerous other factors affecting flightperformance.

3 . P O W E R P L A N T & A C C E S S O R I E S

Lycoming TIO-540-AK1A Engine235 HP @2400 RPMCertified for 100LL & 100 FuelTurbocharging System (Fully Automatic)Fuel Injection SystemTubular Steel Engine MountDynafocal Rear Engine MountEngine Driven Vacuum PumpAutomatic Alternate Engine AirOil CoolerRigid - Mounted CowlingManual Cowl FlapsInduction Air FilterFull Flow Oil FilterThrottle ControlVernier Mixture ControlVernier Propeller ControlDual Ignition System, Shielded MagnetoEngine Exhaust MufflerMcCauley Constant Speed, 3 Blade Metal Prop with De- ice Boots

Propeller GovernorPropeller Spinner, PolishedElectric Starter

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January 2012

GMA-1347 Digital Audio Panel with MarkerBeacon/IntercomGTX-33 Transponder-Mode S w-TISGIA-63W NAV/COM/GPS/WAAS with GS #1GIA-63W NAV/COM/GPS/WAAS with GS #2GDU-1044B Primary Flight Display (PFD)GDU-1044B Multi-Function Display (MFD)GEA-71 Engine/Airframe ComputerGRS-77 AHRSGDC-74A Air Data Computer with OAT ProbeGMU-44 MagnetometerGarmin SafeTaxi & FliteChartsGFC-700 Autopilot

• Go-Around Switch• Electric Trim• A/P Disconnect• Control Wheel Steering Button

GDL-69A Flight Information System (FIS) with XMRadioWX-500 StormscopeElectronic ChecklistsME406 Two Frequency Emergency LocatorTransmitterEmergency Locator Transmitter Remote Mounted SwitchBackup Attitude Gyro, Altimeter and AirspeedIndicatorControl Wheel Push-To-Talk Switch-Pilot/CopilotMic & Phone Jacks-Pilot/Copilot/PassengersAuxiliary Stereo Input JackAntennas:

• Marker Beacon Antenna• Transponder Antenna• VHF/GPS Antenna (2)• XM Antenna• NAV Antenna• Emergency Locator Transmitter External Antenna• Stormscope Antenna

Pitot System - HeatedStatic System

Hand Held MicrophoneAlternate Static SourceCompass

4 . S K Y L A N E E Q U I P M E N T L I S TThe following list of equipment is included on the stan-dard aircraft and it does not reflect optional equipment.

NAV III Avionics Package

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January 2012

1. MASTER Switch (ALT and BAT)2. STBY BATT Switch3. STBY BATT Test Annunciator4. AVIONICS Switch (BUS 1 and BUS 2)5. Electrical Switches6. GDU-1044B Primary Flight Display7. Backup Attitude Gyro, Airspeed & Altimeter

Indicator8. GMA-1347 Audio Panel9. Backup Compass10. GDU-1044B Multi-Function Display11. ELT Remote Switch/Annunciator

12. Flight Hour Recorder (Hobbs Meter)13. Cabin Air Control14. Wing Flap Switch Lever And Position Indicator15. Mixture Control16. Propeller Control Knob17. Throttle (With Friction Lock)18. ALT Static Air Valve Control19. Go-Around Switch20. Electrical and Avionics Circuit Breakers21. Magnetos/Start Switch, Key Operated22. Dimming Panel

5 . I N S T R U M E N T PA N E L

FIGURE III — SKYLANE INSTRUMENT PANEL

19 18 17 16 15 14 132021

22

1

2

3

4 5 6 8 10 11 12

7

9

10

January 2012

6 . E L E C T R I C A L P O W E R

Alternator, 28 Volt, 95 AmpBattery, 24 Volt, 10.0 AH (1 hr rate), Manifold TypeStandby Battery, 24 volt, 6.2 AH (1 hr rate) Sealed TypeStandby Battery ControllerElectrical Circuit Panel• Alternator/Battery Master Switch• Split Avionics Master Switch• Circuit Breakers, Electrical• Switches, Electrical

Electrical J-Box• Alternator Control Unit• Battery Current Sensor• Ground Service Receptacle• Starter Relay• Alternator Relay• Battery Relay• Ground Power Relay• Bus Circuit ProtectionCabin Power Jack -12 Volt (fore & aft), 10 ampPropeller De-Ice Timer• Propeller Heat

7 . E N G I N E I N D I C AT I N G S Y S T E M ( E L E C T R O N I C )

AmmetersVoltmetersVacuumManifold PressureOil Pressure and TemperatureTachometer - Hour RecorderFuel Flow (GPH)LH/RH Fuel QuantityCHT - Cylinder Head TemperatureTIT - Turbine Inlet TemperatureEGT - Exhaust Gas TemperatureBackup Single Pump Vacuum SystemAnnunciation – Caution and WarningAlerts (PFD)

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January 2012

9 . E X T E R I O R

Epoxy Corrosion Proofing, All StructureLH Door, Pilot with Hinged Window, Lock and KeyRH Door, Copilot with Hinged WindowLH Baggage Door, with Lock and KeyRear WindowAll Windows TintedGear Jack PadsFixed Landing GearWhite Polyurethane Exterior Paint

Refueling Steps and Handles, Wing Struts andFuselageFixed Cabin Entrance StepsTie Down Rings, LH/RH Wing & TailTube Type Tires• Nose – 5.00 X 5• Mains - 6.00 X 6Conical Camber Wing TipStrut Braced, Camber Lift WingsStatic Wicks

Windshield Defroster, PilotVentilator, Adjustable (6 places)Heating System, Shrouded Muffler with Firewall ValveInsulation / SoundproofingCarbon Monoxide Detection System

Precise Flight Oxygen System - Consists of a micro-phone mask and A5 flowmeter and oxymizer cannulafor the pilot, and standard mask, A5 flowmeter, andoxymizer cannulas for each passenger position.

4 place oxygen equipment bag

8 . E N V I R O N M E N TA L

LED Ground Recognition Beacon - Vertical TailLED Navigation, LH/RH Wing Tip & TailNavigation Light Detectors, LH/RHWing Tip Strobe, LH/RH

Dual Wing LED Landing and Taxi Lights withintegrated Pulse Recognition TechnologyUnderwing Courtesy, LH and RH

1 0 . E X T E R I O R L I G H T S

Hydraulic Brakes, Toe-OperatedParking BrakeStainless Steel Control CablesDual Flight Controls - Aileron/Elevator/RudderLeather Wrap Control Wheels, All Purpose Pilot/CopilotPilot Control Wheel Switches• Pitch Trim• AP Disconnect• Control Wheel Steering ButtonGo-Around SwitchElevator Trim - Manual/ElectricRudder Trim - Manual

Electrical Preselect - FlapsSteerable Nose WheelAileron and Elevator Control Lock

1 1 . F L I G H T C O N T R O L S

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January 2012

LED Pilot/Copilot Cabin Overhead LED LightsLED Passenger Overhead LightInterior Lights Dimming ControlsMap Light, Pilot Control WheelSub-Panel Lighting (LED Backlighted)• Flaps• Throttle• Mixture• Propeller• Cowl Flap• Environmental Controls (Air and Heat)Switch Panel Lighting (LED Backlighted)• Avionics and Master Switches• Dimming Rheostats

• Landing, Taxi and Nav Switches• Beacon, Strobe, Fuel Pump, Pitot Heat, Prop Heat• 12 Volt Cabin Power• Standby Battery Switch• Circuit Breakers• Ignition / Start SwitchLCD Lighted Glass Panel Displays:• Electronic Flight Instruments• Electronic Avionics Instruments• Electronic Engine InstrumentsAudio Panel Bezel (Backlighted)Radio Call Plate (Backlighted)Compass Internally LightedBackup Attitude, Altimeter, Airspeed Internally Lighted

1 4 . I N T E R I O R L I G H T I N G

Electric Auxiliary Fuel PumpEngine Driven Fuel PumpIntegral Wet Wing Fuel Tanks, 87 Gal. UsableFuel Selector Valve, Left/Both/Right/Off

Fuel Strainer, Incorporated with Fuselage Quick DrainFuel Tank Quick Drain, 5 per wingFuel Sampler CupFuel Vapor Return System

1 2 . F U E L S Y S T E M

High Contrast Sport Interior Theme - Light Taupe andBlack

Light Taupe Leather Seating Surface with BlackPerforated (Embossed) Leather Inserts on SeatCushion and Seat Back

Door Panel, Upper Sidewall Accent - Black Perforated(Embossed) Leather

Door, Lower Sidewall, Kick Panel - Black KydexVinyl Grip Flooring in Crew AreaCarpeting in Passenger AreaPilot/ Copilot Amsafe Inflatable Seat Belts &Shoulder Harness STC, Inertia reelRear Seat Bench with One Piece Reclining Back,Seat Belts & Shoulder Harness, Inertia ReelPassenger Side WallPilot and Copilot Seats

• Adjustable Fore and Aft• Reclining Backs• Vertical Adjustment

Pilot & Copilot Door Armrests

Approach Plate Holder on Pilot Control WheelPilot's Check ListPilot's Operating HandbookHand Held Fire ExtinguisherGlareshieldClothes Hanger BarMetal Instrument Panel, with Removable Stby Instr.SubpanelMetal Instrument Panel, with Removable SubpanelsMap/Glove CompartmentBaggage NetRadio Call PlateMap & Storage PocketsCabin Door Scuff PlatesPilot/Copilot Sun VisorsPassenger Cup HoldersJepp Manual Storage Console with Cup HoldersTow Bar

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1 5 . E X T E R I O R S T R I P I N G O P T I O N SDistinctive exterior styling in a variety of colors is pro-vided.

Cessna will offer one G1000 training course at noadditional charge and one G1000 ground schoolcourse for a second person at no additional charge,with purchase of a new aircraft. This offer is valid for12 months after aircraft delivery.

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17.1 CESSNA'S LIMITED WARRANTY - SINGLEENGINE PISTON AIRCRAFTCessna warrants the aircraft and all parts included there-in to be free from defects in material and workmanshipunder normal use and service for a period of twenty-four(24) months after the Warranty Start Date, except ashereafter noted. Engines, engine part accessories,avionics, batteries, propellers and governors are specif-ically excluded from this warranty. Paint and graphicswarranties are addressed separately.Spare parts sold by Cessna, excluding engines, enginepart accessories, avionics, batteries, propellers and gov-ernors are warranted for six (6) months after installation,except as hereafter noted.Cessna's obligation under this warranty is limited torepairing or replacing, at its option, with exchange, over-hauled, or new parts, items found defective by Cessna’sexamination which are returned at the owner’s expensewithin the applicable twenty-four (24) or six (6) monthperiod to any Cessna Service Station.A new warranty period is not established for replace-ment parts. Replacement parts are warranted only forthe remainder of the applicable twenty-four (24) or six(6) month original warranty period.The repair or replacement of defective parts under thiswarranty will be made without charge to the owner forparts and labor for removal, installation and/or actualrepair, except that the owner shall pay all import dutiesand sales and use taxes on replacements and repairs. This limited warranty does not apply to parts subjectedto misuse, negligence, improper installation, accident,alteration; repairs not authorized by Cessna; normalmaintenance services (cleaning, control rigging, brakeand other mechanical adjustments, maintenanceinspections, etc.); replacement of service items (lightbulbs, brake linings, filters, hoses, tires, cowl mounts,etc.); or to normal deterioration of soft trim or appear-ance items (paint, upholstery, rubber-like items, etc.)due to corrosion, wear and exposure.WITH THE EXCEPTION OF THE WARRANTY OFTITLE, TO THE EXTENT ALLOWED BY APPLICABLELAW, THIS WARRANTY IS EXPRESSLY IN LIEU OFANY OTHER WARRANTIES, EXPRESSED ORIMPLIED IN FACT OR BY LAW, INCLUDING ANYIMPLIED WARRANTY OF MERCHANTABILITY ORFITNESS FOR A PARTICULAR PURPOSE. THEREMEDIES OF REPAIR OR REPLACEMENT ASABOVE SET FORTH ARE THE ONLY REMEDIESUNDER THIS WARRANTY. CESSNA DISCLAIMS ANYOBLIGATION OR LIABILITY WHETHER IN CON-TRACT OR IN TORT (AND WHETHER FOR NEGLI-GENCE, STRICT LIABILITY, PRODUCT LIABILITYOR OTHERWISE), INCLUDING LOSS OF USE OFTHE PRODUCT WARRANTED, LOSS OF TIME,INCONVENIENCE, COMMERCIAL LOSS OR ANYOTHER DIRECT, CONSEQUENTIAL, SPECIAL OR

INCIDENTAL DAMAGES. THIS WARRANTY IS INLIEU OF ANY OTHER OBLIGATION OR LIABILITY OFCESSNA OF ANY NATURE WHATSOEVER BY REA-SON OF THE MANUFACTURE, SALE OR LEASE OFSUCH AIRCRAFT PRODUCTS AND CESSNA NEI-THER ASSUMES NOR AUTHORIZES ANYONE TOASSUME FOR IT ANY OTHER OBLIGATION OR LIA-BILITY IN CONNECTION WITH SUCH AIRCRAFTPRODUCTS. COMPLIANCE WITH THIS LIMITEDWARRANTY MAY BE AFFECTED IF EXPORTLICENSES ARE REQUIRED TO BE REQUESTEDAND APPROVED BEFORE SPARE PARTS CAN BESHIPPED TO CERTAIN FOREIGN COUNTRIES. 17.2 AIRCRAFT PAINT AND GRAPHICS– SINGLEENGINE PISTON AIRCRAFTCessna endeavors to select and use high qualitypolyurethane paints from the leading manufacturers.Polyurethane paints and graphics are used because oftheir high gloss characteristics and ability to withstanddramatic temperature and pressure changes. The painton your new aircraft will maintain its high gloss charac-teristics for an extended period of time provided it iscared for properly.The painted exterior surfaces require an initial curingperiod which may be as long as ninety (90) days afterthe finish is applied. During this curing period, some pre-cautions should be taken to avoid damaging the finish orinterfering with the curing process. The finish should becleaned only by washing with clean water and mild soap,followed by a water rinse and drying with a cloth orchamois. Do not use polish or wax, which would excludeair from the surface, during this ninety (90) day curingperiod. Once the finish has cured completely, it may bewaxed with a good automotive wax, but power buffingshould be avoided to prevent damage to the paint sur-face.Normal paint maintenance will include but is not limitedto; touchup of abrasion and wear of the paint on screwsheads, around access panels, the radome, wing leadingedges, vertical and horizontal stabilizer leading edges,windshield retainers and other leading edge surfacesincluding parts on the landing gear subject to damage orerosion from airborne particles. Proper maintenanceincludes keeping surfaces clean, polished, and touchingup chipped or eroded areas to prevent further damageand corrosion.Paint and graphics warranty applies only to defects inmaterial and workmanship for a period of one (1) yearfrom the Warranty Start Date. Deterioration of paint andgraphics due to normal wear, exposure, or impropercare is not covered by the warranty. If proper paint main-tenance procedures have been followed and paint peel-ing, blistering or cracking is evident in areas other thanimmediate leading edge surfaces, warranty considera-tion may be requested thorough a Cessna ServiceStation.

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Generally speaking, warranty repair of paint is confinedto a limited surface area. Workmanship or materialdefects can usually be identified to localized surfaceareas that were improperly prepared prior to paint appli-cation, or to areas where the paint or subsurface primerhas been improperly applied. Complete strip and repaint of an entire airplane canONLY be authorized if there is evidence of paint defectson several major surface areas of the aircraft. Contactyour Cessna Field Service Engineer concerning paintdefects on any major surface of an aircraft.17.3 Textron Lycoming Warranty (Limited) NewReciprocating Aircraft EngineWhat Textron Lycoming Promises YouEngine Model Aircraft ModelIO-360-L2A Cessna-172R, 172SIO-540-AB1A5 Cessna-182TIO-540-AC1A5 Cessna-206HTIO-540-AK1A Cessna-T182TTIO-540-AJ1A Cessna-T206HTextron Lycoming warrants the above listed new recip-rocating engine models sold by it to be free from defectsin material and workmanship for a period of twenty-four(24) months after aircraft delivery to the original retailpurchaser or first user. The date of first operation mustnot exceed two (2) years from the date of shipment fromTextron Lycoming.Textron Lycoming's obligation under this warranty shallbe limited to its choice of repair or replacement, on anexchange basis, of the engine or any part of the engine,when Textron Lycoming has determined that the engineis defective in material or workmanship. Such repair orreplacement will be made by Textron Lycoming at nocharge to you. Textron Lycoming will also bear the costfor labor in connection with the repair or replacement asprovided in Textron Lycoming's then current Removaland Installation Labor Allowance Guidebook.Any engine or part so repaired or replaced will be enti-tled to warranty for the remainder of the original warran-ty period.

YOUR OBLIGATIONSThe engine must have received normal use and service.You must apply for warranty with an authorized TextronLycoming distributor within 30 days of the appearance ofthe defect in material or workmanship.Textron Lycoming's warranty does not cover normalmaintenance expenses or consumable items, the obli-gations on the part of Textron Lycoming set forth aboveare your exclusive remedy and the exclusive liability ofTextron Lycoming. This warranty allocates the risk ofproduct failure between you and Textron Lycoming, aspermitted by applicable law.

Textron Lycoming reserves the right to deny any warran-ty claim if it reasonably determines that the engine orpart has been subject to accident or used, adjusted,altered, handled, maintained, or stored other than asdirected in your operator's manual, or if non-genuineTextron Lycoming parts are installed in or on the engineand are determined to be a possible cause of the inci-dent for which the warranty application is filed.Textron Lycoming may change the construction ofengines at any time without incurring any obligation toincorporate such alterations in engines or parts previ-ously sold.THIS LIMITED WARRANTY IS EXCLUSIVE AND INLIEU OF ALL OTHER WARRANTIES AND REPRE-SENTATIONS, EXPRESS OR IMPLIED OR STATUTO-RY, WHETHER WRITTEN OR ORAL, INCLUDING BUTNOT LIMITED TO ANY WARRANTY OF MER-CHANTABILITY OR FITNESS FOR ANY PARTICULARPURPOSE, AND ANY IMPLIED WARRANTY ARISINGFROM ANY COURSE OF PERFORMANCE OR DEAL-ING OR TRADE USAGE. THIS WARRANTY IS ALSOIN LIEU OF ANY OTHER OBLIGATION, LIABILITY,RIGHT, OR CLAIM, WHETHER IN CONTRACT OR INTORT, INCLUDING ANY RIGHT IN STRICT LIABILITYIN TORT OR ANY RIGHT ARISING FROM NEGLI-GENCE ON THE PART OF TEXTRON LYCOMING,AND TEXTRON LYCOMING'S LIABILITY ON SUCHCLAIM SHALL IN NO CASE EXCEED THE PRICEALLOCABLE TO THE ENGINE OR PART WHICHGIVES RISE TO THE CLAIM. LIMITATION OF LIABILITY IN NO EVENT, WHETHERAS A RESULT OF A BREACH OF WARRANTY, CON-TRACT, OR ALLEGED NEGLIGENCE, SHALL TEX-TRON LYCOMING BE LIABLE FOR SPECIAL ORCONSEQUENTIAL OR ANY OTHER DAMAGES,INCLUDING BUT NOT LIMITED TO LOSS OF PROF-ITS OR REVENUES, LOSS OF USE OF THE ENGINE,OR COST OF A REPLACEMENT.No agreement varying this warranty or TextronLycoming's obligations under it will be binding uponTextron Lycoming unless in writing signed by a dulyauthorized representative of Textron Lycoming.

Cessna Model Aircraft OnlyTextron Lycoming Engines652 Oliver StreetWilliamsport, Pennsylvania 17701(570) 323-6181www.lycoming.textron.comOriginal Engine Installation OnlyEffective 2000

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17.4 McCauley Propeller Systems Standard LimitedWarrantyMcCauley Propeller Systems, a Division of CessnaAircraft Company, Wichita, Kansas, U.S.A., expresslywarrants new and remanufactured products producedand sold by McCauley to be free from defects in materi-al and workmanship under normal use and service for aperiod of thirty-six (36) months after delivery to the orig-inal retail purchaser or until the expiration of the maxi-mum hours of use or calendar limits for overhaul pub-lished by McCauley for the subject product, whicheveroccurs first.McCauley’s obligation under this limited warranty is lim-ited to repairing or replacing, at its sole option, any pro-peller, propeller parts, governor or governor parts deter-mined by McCauley to have been defective and whichare properly returned by the owner, with a written state-ment describing the alleged defect, to any McCauleyAuthorized Service Center authorized to service the indi-vidual McCauley product. The repair or replacement ofdefective parts will be made without charge to the ownerfor parts, or labor for removal and installation, exceptexport/import duties, and/or sales or use taxes, if anywhich are solely the owner’s responsibility. McCauleywill warrant a part replaced pursuant to this limited war-ranty under the same terms as the original part for theremainder of he applicable warranty period of the origi-nal part. This limited warranty is not intended to anddoes not cover the costs of normal maintenance of over-haul.In addition, McCauley will repair or replace, at its option,any propeller, propeller parts, governor, or governorparts requiring replacement due to manufacturing defectif found at or before the first recommended overhaulinterval as described in McCauley published serviceinformation. This first overhaul coverage does notinclude labor, standard overhaul replacement parts,parts repairable via published service information (re-plating, painting, etc.), other costs associated with thepropeller or governor overhaul, or export/import duties,and/or sales or use taxes, nor does it apply to defectsfound after McCauley published overhaul hour or calen-dar limits. The provisions of this limited warranty do notapply to: any McCauley parts which have been subjectto misuse, negligence or accident or which have beenrepaired or altered in any way that, in the sole judgmentof McCauley, adversely affects their performance, stabil-ity or reliability; to normal maintenance services (such ascleaning, mechanical adjustments and maintenanceinspections); to the replacement of service items madein connection with normal maintenance; to normal dete-rioration of soft trim and appearance items (such aspaint and rubber-like items) due to wear and exposure;to propellers, governors or parts found defective beyondthe McCauley recommended overhaul period; or to parts

which have been improperly installed by entities otherthan McCauley and/or McCauley Authorized ServiceCenters.The McCauley limited warranty is void on any new orremanufactured product installed, without McCauley’sprior written approval, on a non-type certificated engine,or on any engine which has received an overhaul ormodification which is not approved by the engine manu-facturer and that results in a change to the vibratoryenvironment of the engine such as, but not limited to, analteration of horsepower, operating RPM, crankshaftdamper configuration, compression ratio, magneto tim-ing, camshaft design, or any other overhaul or modifica-tion not expressly approved by the original engine man-ufacturer. The McCauley limited warranty is also void onany McCauley product shipped new from the factory ordistributor in disassembled state, then later re-assem-bled by an unauthorized party. Parties authorized to re-assemble factory-new product must have specific writ-ten permission from McCauley to do so, otherwise allMcCauley warranty on the affected unit is void. NoMcCauley warranty coverage is offered for leakage onproduct assembled outside McCauley, regardless of theassembling party.To the extent allowed by applicable law, THIS WAR-RANTY IS EXPRESSLY IN LIEU OF ANY OTHERWARRANTIES, EXPRESSED OR IMPLIED IN FACTOR BY LAW, INCLUDING ANY IMPLIED WARRANTYOF MERCHANTABILITY OR FITNESS FOR A PAR-TICULAR PURPOSE. THE REMEDIES OF REPAIR ORREPLACEMENT SET FORTH HEREIN ARE THEONLY REMEDIES UNDER THIS LIMITED WARRAN-TY. McCAULEY DISCLAIMS ANY OBLIGATION ORLIABILITY, WHETHER IN CONTRACT OR IN TORT ,INCLUDING LOSS OF USE OF THE PRODUCT WAR-RANTED, LOSS OF TIME, INCONVENIENCE, LOSSOF PROFITS, COMMERCIAL LOSS, OR ANY OTHERDIRECT, CONSEQUENTIAL, SPECIAL, OR INCIDEN-TAL DAMAGES. THIS WARRANTY IS IN LIEU OFANY OBLIGATION OR LIABILITY ON THE PART OFMcCAULEY TO ANYONE OF ANY NATURE WHAT-SOEVER BY REASON OF THE MANUFACTURE,SALE, LEASE, OR USE OF THE WARRANTEDPRODUCTS AND McCAULEY NEITHER ASSUMESNOR AUTHORIZES ANYONE TO ASSUME FOR ITANY OTHER OBLIGATION OR LIABILITY IN CON-NECTION WITH SUCH WARRANTED PRODUCTS.THE UNITED NATIONS CONVENTION ON CON-TRACTS FOR THE INTERNATIONAL SALE OFGOODS, 1980, AND ANY SUCCESSOR THERETO, ISEXPRESSLY EXCLUDED FROM THIS WARRANTY.Issued 9/1/2003

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17.5 Bendix/King Equipment Retail WarrantyStatement For Cessna Aircraft Company SingleEngine ProgramA. General Aviation Avionics products manufactured byHoneywell under the brand name Bendix/King (collec-tively referred to herein as "Honeywell") are warrantedagainst defects in design, material, or workmanshipcaused by Honeywell or its authorized agent(s) for thewarranty period as defined in Paragraph (B) of this state-ment, which occur under normal and intended use andservice, subject to all of the qualifications and conditionshereinafter stated.B. The warranty term for new product(s) installed on newaircraft shall be twenty-four (24) months from delivery tothe original retail purchaser or first user. Cessna to pro-vide warranty start date information. C. Any productHoneywell finds to be in violation of the warranty as setout in Paragraph (A) hereof, at the option of Honeywell,shall be repaired, replaced, or exchanged in accordancewith the following procedures:

1. Products shall be returned to any authorized Honeywell Service Center or Honeywell Regional Product Support Repair/Overhaul Facility, with transport harges prepaid.2. After correction, the products shall be returned to the purchaser with surface transportation charges prepaid.3. The risk of loss or damage to all products in transit shall be borne by the party initiating the transportation of such products unless the purchaser makes a request for specific mode of transportation. In such case, the risk of loss and the cost of shipment shall be borne by the purchaser. All items repaired or replaced hereunder shall be warranted for the unexpired portion of the original warranty period.

D. This warranty specifically excludes defects thatHoneywell determines to be the result of any or all of thefollowing:

1. Abuse, accident, or misuse;2. Contamination, negligence, tampering, or improper storage or maintenance;3. Repair or attempted repair by unauthorized persons or use of non-Honeywell or unauthorized repair or replacement parts;4. Products not installed by an authorized Honeywell Installation Facility in accordance with the appropriate installation manual.

E. The warranty as set out in Paragraph (A) is the onlywarranty for Honeywell products and is in lieu of all other

warranties expressed or implied, including the impliedwarranties of merchantability and fitness for a particularpurpose that are herewith expressly excluded and dis-claimed.F. The remedies as set out in Paragraph (C) hereof statethe entire liability of Honeywell and constitute the soleand exclusive remedy of the purchaser. Honeywell shallnot be liable for any other claim, loss, or damage, includ-ing, but not limited to, incidental, consequential, or otherkinds of damages whether based on contract, tort, neg-ligence, or other theory of product liability.G. Honeywell reserves the right to make designchanges, additions to, and improvements in its productswithout the obligation to install same in products previ-ously manufactured.

THIS IS A LIMITED WARRANTYHoneywell23500 W. 105th StreetOlathe, Kansas 66061

17.6 Garmin Avionics Installed in Single EngineAircraftAircraft OEM-Installed Avionics 2-Year LimitedWarranty PolicyThis GARMIN Product is warranted to be free fromdefects in materials or workmanship for two years fromthe date of warranty activation. Within this period,GARMIN International, Inc. will at its sole option, repairor replace any components which fail in normal use.Such repairs or replacement will be made at no chargeto the customer for parts or labor, provided that the cus-tomer shall be responsible for any transportation cost.This warranty does not cover failures due to abuse, mis-use, accident or unauthorized alteration or repairs.THE WARRANTIES AND REMEDIES CONTAINEDHEREIN ARE EXCLUSIVE AND IN LIEU OF ALLOTHER WARRANTIES EXPRESS OR IMPLIED ORSTATUTORY, INCLUDING ANY LIABILITY ARISINGUNDER ANY WARRANTY OF MERCHANTABILITYOR FITNESS FOR A PARTICULAR PURPOSE,STATUTORY OR OTHERWISE. THIS WARRANTYGIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAYVARY FROM STATE TO STATE.IN NO EVENT SHALL GARMIN BE LIABLE FOR ANYINCIDENTAL, SPECIAL, INDIRECT OR CONSE-QUENTIAL DAMAGES, WHETHER RESULTINGFROM THE USE, MISUSE OR INABILITY TO USETHIS PRODUCT OR FROM DEFECTS IN THE PROD-UCT. Some states do not allow the exclusion of inciden-

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tal or consequential damages, so the above limitationsmay not apply to you.GARMIN retains the exclusive right to repair or replacethe product or offer a full refund of the purchase price atits sole discretion. SUCH REMEDY SHALL BE YOURSOLE AND EXCLUSIVE REMEDY FOR ANY BREACHOF WARRANTY.To obtain warranty service, contact your local GARMINauthorized Service Center. For assistance in locating aService Center near you, call GARMIN CustomerService at one of the numbers shown below.

GARMIN International1200 East 151st StreetOlathe, Kansas 66062, U.S.A.Toll free: 1-800-800-1020Phone: 1-913-397-8200FAX: 1-913-397-0836

GARMIN (Europe) Ltd.Unit 5, The QuadrangleAbbey Park Industrial EstateRomsey, SO51 9AQ, U.K.Phone: 44-1794-519944FAX: 44-1794-519222Visit our web site at: www.garmin.com

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Cessna Single Engine Piston Aircraft, 2625 S. Hoover Rd. Wichita, Kansas 67215 Telefax: 316.517.2772