STC SA413CH

SA413CH Pegasus Innovations, LLC 45 Buttercup Loop Belton, TX 76513 Part 3 the Civil Air Regulations.

2A13 New Piper PA-28-140, PA-28-150 and PA-28-151

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

2) The FAA approved Airplane Flight Manual Supplement dated September 8, 1995, or later FAA approved revisions is required.

(Continued on Page 3) 3/18/1995 4/13/1998 8/26/2015 12/1/2020 9/19/1995 11/8/1995 9/9/1996 10/6/1999 for Roy E. Boffo III Deputy Branch Manager Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3 Install Lycoming engine Model O-320-D2A, O-320-D3G or O-320-E2A (modified by STC SE367CH) in accordance with Piper Service Manuals.

(See Type Certificate Data Sheet Number 2A13 for the complete certification basis.)

SA413CH 12/01/20 3

SA413CH 12/01/20 Limitations and Conditions (continued):

3) The modified engine is rated 160 hp @ 2700 rpm take off and maximum continuous operation.

4) Propeller pitch range change to 60” standard, 58” climb, 62” cruise.

5) 100 Octane minimum grade aviation gasoline only.

6) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

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