STC SA1305SW

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

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Signature

Title SA1305SW Griggs Aircraft Refinishing, LLC.

172 Runway Road Tunkhannock, PA 18657 Civil Air Regulations.

1. Installation of auxiliary fuel tank according to Drawing 25500 dated 03/15/71, or later FAA approved revision.

2 FAA Approved Airplane Flight Manual Supplement dated April 29, 1971, is required; or Supplement dated February 23, 1977, if non-icing vents are installed at Nayak vent locations.

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual 25525 dated January 21, 1982 to be used in lieu of previous FAA Approved AFM Supplements.

1. Capacity of the tank is 26 gals. For weight and balance plotter see Drawing 25528 dated 3/15/71.

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

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

Gaetano Sciortino Manager New York Aircraft Certification Office Piper PA-31, S/N 31-2 and Up March 5, 2004, June 8, 2015, September 4, 2015, October 15, 2015, June 22, 2016, January 13, 2017 February 23, 1977, January 21, 1982 April 27, 1971 May 10, 1971 A8EA 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SA1305SW