FRIDAY   |   March 7, 2008   
This document is published for the purpose of providing general information for the evaluation of design, performance and equipment of the Cessna Skyhawk SP. Should more information be required, please contact:

Cessna Aircraft Company
Single Engine Piston Aircraft
2625 S. Hoover Rd.
Wichita, Kansas 67215

This document supersedes all previous Specification and Description documents and describes only the Skyhawk Model 172S, its powerplant and equipment.

Also included are the warranties applicable to the Skyhawk Model 172S aircraft, the Textron Lycoming IO-360-L2A engine, the McCauley propeller and the OEM-installed Bendix/King and Garmin avionics.

In the event of any conflict or discrepancy between this document and the basic purchase agreement, the basic purchase agreement language shall govern.

Due to the time span between the date of this Specification and Description and the scheduled delivery date of the aircraft, Cessna reserves the right to revise the "Specification" whenever occasioned by product improvements, government regulations or other good cause.

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