STC SA02193CH

FAA Form 8110-2 (5/14) Page 1 of

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Title 2A3 Mooney International Corp 165 Al Mooney Road North Kerrville, TX 78028 3 SA02193CH Code of Federal Regulations 23 Power increase to 310 BHP by Installation of Powerlite STC SE02930AT or CMI IO-550N Engine rated at 310 BHP/2700 RPMs and Hartzell Propeller Model PHC-J3YF-1RF/F7693DF(B)-2 propeller in accordance with Installation Instructions, M1029-5, Rev. F, dated 04/17/13 or later FAA approved revision.

Mooney Airplane Company, Inc.

M20R, M20S, M20U

1. This STC is only applicable to aircraft powered by Continental Motors (CMI) IO-550-N engines, or by a CMI IO-550-G engine which has been modified by Powerlite LLC STC SE02930AT, or other approved FAA method to produce 310 horsepower.

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

(Continuation on page 3 of 3) November 6, 2007, February 27, 2015, November 14, 2017 January 28, 2011, May 03, 2013, October 11, 2017 December 10, 2004 December 16, 2005 Jim Grigg Manager, Fort Worth ACO Branch Compliance & Airworthiness Division

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SA02193CH

FAA Form 8110-2 (5/14) Page 3 of

3. The modified aircraft shall be operated in accordance with Minnis Aviation report M1029-12 Airplane Flight Manual Supplement, Revision C, dated 04/17/13 or Mooney International Corp document SUPP0029 Airplane Flight Manual Supplement (AFMS), Revision D dated 11/14/17 or later FAA approved revision.

4. The aircraft shall be maintained in accordance with Report M1029-12, Instructions for Continued Airworthiness, Revision C, dated 04/17/13 or later FAA approved revision.

5. 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.

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SA02193CH