Installation of the Hartzell Model HC-C2YR-IN/NG8302-7 Propeller in accordance with Hartzell Owner's Manual, Document Number 145 61-00-45, Revision 20, dated April 2021, or later FAA approved revision.

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Limitations and Conditions:

1) The installer must determine whether this design change is compatible with previously approved modifications.

2) For Instruction for Continued Airworthiness refer to Hartzell Owner's Manual, Document Number 145 61-00-45, Revision 20, dated April 2021, or later FAA approved /accepted revision.  

3) Aircraft must previously or concurrently be equipped with a Lycoming O-360-A1A, O-360-AID, or IO-360-M1B under a separate FAA approval. 

4) Aircraft must be configured with a tail wheel/conventional landing gear under separate FAA approval.

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This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

 

Date of application: November 18, 2021 
Date issuance: April 19, 2022

General Aviation Concepts
3033 Taxilane A
North Pole, AK 99705