STC SA2277CE

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

Part of the

Signature

Title SA2277CE Griggs Aircraft Refinishing, LLC.

172 Runway Road Tunkhannock, PA 18657 Civil Air Regulations.

1. Installation of Fuel Bladder Cells in wet wing fuel cavities in accordance with the following:

a. Configuration 1: O & N Aircraft Modifications Inc., Installation Drawing List B-400, original release, dated July 30, 1987, revised September 11, 1987, or later FAA Approved revision; Report B-200 Installation Instructions, dated August 14, 1987;

and Report B-300 Maintenance Instructions, dated August 14, 1987.

b. Configuration 2: O & N Installation Drawing List No. B-600, Revision A, dated July 28, 1995, and Report B-300 Maintenance Instructions, dated November 15, 2003.

(See Description of Type Design Change continued on Page 3 of 3)

1. Configuration 3: Configuration 1 is a pre-requisite and must be installed prior to or in conjunction with configuration 3.

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 Mooney M20F, M20J April 4, 1988, March 12, 1997, May 4, 2015, June 8, 2015, October 15, 2015, June 22, 2016, January 13, 2017 September 29, 1995, December 22, 2003 June 13, 1986 September 11, 1987 2A3 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA2277CE

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

3 Date Reissued: January 13, 2017

Description of Type Design Change (continued):

1. c. Configuration 3: O & N Installation Drawing List B-400a, Revision A, dated January 24, 2003, and Report B-300 Maintenance Instructions, dated November 15, 2003.

2. FAA Approved Flight Manual Supplements:

a. Configuration 1: O & N Aircraft Modifications Inc. Airplane Flight Manual Supplement for Mooney Aircraft Models M20F, dated 9/11/87 (up to S/N 700004) or Airplane Flight Manual Supplement for Mooney Aircraft Model M20F and M20J, dated 9/11/87 (M20F S/N 700005 and above).

b. Configuration 2: O & N Flight Manual Supplement No. 14 for Mooney Aircraft Models M20F and M20J, dated 9/29/95 (covers M20F S/N 700005 and above); Supplemental Flight Manual No. 15 for Mooney Aircraft Model M20F (covers S/N 680002 through 700004), dated 9/29/95.

c. Configuration 3: O & N Flight Manual Supplemental No. 73A for Mooney Aircraft Model M20F, dated December 22, 2003 (applicable to M20F S/Ns 660002 through 660004, 670001 through 670363, 670387 through 670482, 670484 through 670539, 680001 through 680206, 690003 through 690090, 690092, 700001 through 700004); Flight Manual Supplemental No. 72A for Mooney Aircraft Models M20F and M20J, dated December 22, 2003 (applicable to M20F S/Ns 700005 through 700061, 700063 through 700066, 700070 through 700072A, 22-0001 and on; M20J S/Ns 24-0002 through 24-2999) are required.

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