STC SA1008SW

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SA1008SW Quantum Swiss LLC 1000 Brickell Avenue, Suite 201 Miami, FL 33131 Part 3 the Civil Air Regulations A13CE Cessna 177 Installation of Lycoming O-360-A1A, O-360-A3A, O-360-A2F, O-360-A4M, O-360-A2A, O-360-A4A, or O-360-A1F engines and Sensenich M76EM8S5-0-60 propeller in accordance with Air Mod Engineering Drawing 68020FP through E.O. "S” dated August 20, 1969, or later FAA approved data.

See continuation sheet on page 3 of 3.

November 15, 1968 March 15, 1999; March 24, 1999; July 15, 2009; July 12, 2022 March 17, 1969 September 8, 2009 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:

SA1008SW 3

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1. The following placards are required:

a. Avoid continuous operation between 2150 and 2350 RPM.

b. Minimum octane fuel 100/130.

2. A copy of this certificate and FAA approved Flight Manual Supplement, Document No. AU-AFMS-01, Revision Original, dated September 4, 2009, or later FAA approved revision must be maintained as part of the permanent records of aircraft modified after September 8, 2009.

3. Compatibility of this design change with previously approved modifications must be determined by 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 that permission.

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