STC SA1016NW

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

(See Continuation Sheet Page 3 of 4 Pages) February 1, 1965, and amendments 23-1 and 23-2.

SA1016NW FletchAir, Inc.

103 Turkey Run Lane Comfort, TX 78013 23 the Federal Aviation Regulations A11EA Gulfstream American (Grumman) AA-1 Installation of a Lycoming 0-360-A4M engine, Sensenich 76EM8-0-62 propeller, and AA-5 elevator system in accordance with Maynard C. Crosby photographs 1 through 5.

Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Gulfstream American (Grumman) AA-1, Serial Number AA1-0459, as modified by the installation of a modified lower cowl, landing gear fairing, and AA-5A dorsal fin in accordance with STC Nos. SA809NW, SA810NW, and SA1009NW respectively. A copy of this Certificate and Addendum No.

SA1016NW shall be maintained as part of the permanent records for the modified aircraft.

May 28, 1980 June 9, 2022 August 28, 1980 For Acting Manager, Seattle ACO Branch

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SA1016NW

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 3 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

(See Continuation Sheet Page 4 of 4 Pages) SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA1016NW The conditions and limitations of the original specification apply except as follows:

This Addendum, which is part of Supplemental Type Certificate No. SA1016NW, prescribes the condtions and limitations under which the STC was issued and meets the airworthiness requiements of the Federal Aviation Regulations.

SUPPLEMENTAL TYPE CERTIFICATE: FletchAir, Inc.

1. MODEL AA-1 2PCLM (NORMAL CATEGORY) AS MODIFIED BY STC SA1016NW Engine: Lycoming 0-360-A4M Fuel: 100/130 minimum grade aviation gasoline Engine Limits: For all operators: 2700 rpm (180 Hp) Propeller and Sensenich 76EM8-0-62 Propeller Limits: Diameter: 76" maximum; 76" minimum Static Limits: 230 rpm maximum; 2200 rpm minimum Placards: None C.G. Range: (+78.5) to (+81.0) at 1500 pounds Maximum Weight: 1500 pounds Instrument Markings: Oil Temperature:

245° Oil Inlet (red line) maximum Oil Pressure:

60 to 90 psi (green arc) normal operating range Cylinder Head Temperature (Bayonet Thermcouple):

500°F (red line) maximum SA1016NW

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 4 of 4 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

End NOTE 1: Current weight and balance report including list of equipment in the certified empty weight must be in the aircraft.

NOTE 2: In addition to the Placards and Markings required by Type Certificate Data Sheet A11EA, Note 2, apply the following:

a. Adjacent to the fuel filler cap:

Adjacent to or in close proximity to the aircraft identification plate:

NOTE 3:

With the described engine and propeller installation, performance will be at least equal to or better than that given in the original FAA Approved Airplane Flight Manual for the Grumman American AA-1 airplane.

SUPPLEMENTAL TYPE CERTIFICATE ADDENDUM NO. SA1016NW SA1016NW