STC SA1665NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SAIG65 AM This certificate issued to: General Aviation Modifications, Inc.

2800 Airport Road Ada, OK 74820 Certifies that the change in the type design for the following produot with the limitations and conditions therefor as speoified hereon meets the airworthiness requirement's of Part 3 of the * Federal Aviation I8 egulations. (See Type Certificate Data Sheet No. 1A15 for complete certification basis) Original Product -- Type Certificate Number: 1A15 Make: Piper Model: PA-24-260 Description of Type Design Change:

Installation of a Shadin "Digiflo" (P/N 910501) or "Miniflo" (P/N 912001) series fuel flow indicator system in accordance with FAA sealed CAPCO Report No. 2, dated June 22, 1982, or later FAA approved revision.

Note: Removal of the original pressure fuel flow guage and plumbing is optional for this installation.

Approval of this change in type design applies to the above model aircraft with the following Aveo Lycoming type engines only: 10-540-D4A5, 10-540-N1A5, and 10-540-RIA5. This approval should not be extended to other aireraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will (See Continuation Sheet on Page 3.)

Date of Application: March 6, 1982 Date Reissued: . April 23, 1985; April 12, 1988;

February 28, 2020 Date of Issuance: June 24. 1982 Date Amended: December 12, 1984 FEDERAL AVIATION By Direction of the Administrator (Signature) TOMINISTRATO for Manager, Central Certification Branch Paul (Vu) Nguyen Compliance & Airworthiness Division Aircraft Certification Service (Title)

000. or a years or porn.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA165NM Date of Issuance: June 24, 1982 Date Amended: December 12, 1984 Date Reissued: February 28, 2020 Limitations and Conditions: (Continued):

introduce no adverse effect upon the airworthiness of that aircraft. Aircraft equipped with the Shadin 910501 "Digiflo" or 912001 "Miniflo" fuel flow indicator system must be operated in accordance with FAA Approved Airplane Flight Manual Supplement dated August 6, 1982, or later FAA approved revision. A copy of this Certificate and FAA Approved Airplane Flight Manual Supplement shall be maintained as part of the permanent records for the modified aircraft.

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