STC SA1043SW

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SA1043SW Quantum Swiss LLC 1000 Brickell Avenue, Suite 201 Miami, FL 33131 Part 23* the Federal Aviation Regulations A13CE Cessna 177 Installation of Lycoming O-360-A1A, O-360-A3A, O-360-A1F, O-360-A1F6 and Hartzell Constant Propeller Model HC-C2YK-1B/7666A-2 in accordance with Air Mod Engineering Drawing 68020CS (21 pages).

See continuation sheet on page 3 of 3.

November 15, 1968 May 16, 1989; March 24, 1999; July 15, 2009; July 12, 2022 March 17, 1969 January 26, 2010 Luke Walker Acting Manager, Denver ACO Branch Compliance and Airworthiness Division 3

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Too (Name and address of transferee):

Date oI transfer:

SA1043SW 3

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1. The following placards are required:

a. Avoid continuous operation between 2000 and 2250 RPM

b. Minimum octane fuel 100/130

2. FAA approved Airplane Flight Manual Supplement, Document AU-AFMS-02, Revision Original, dated January 15, 2010, or later FAA approved revision is required after January 26, 2010.

3. Compatibility of this design change with previously approved modifications must be determined by the installer.

4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of permission.

----------------------------------------------------------END--------------------------------------------------- Date reissued, July 12, 2022 33