STC SA1195NW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate /14/70 Number: SA1195NN This certificate issued to: Fletchair, InC.

7786 Braniff Street Houston, Texas 77061 Purl 23 ofithe Federal Aviation Regulations: , February 1, 1965, amended by 23-1 through 23-8.

Original Product - Type-bertificate Numben: ALGEA Make: Gulfstream American Murkel: AA -5B Descriplion/Sype Resign shange: Installation of Sensenich 76EM8S10-0-60 through - 65 propellers on a Lycoming 0-360-A4K engine in accordance with Ameromod Corporation Installation Instruction No. AM 130.

Limilalind and bendilions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the BA part or the dannent reco, for the nobi er aver fe, be paye o naintained airworthiness of that aircraft.

as part of the permanent records Datindaide saht top ring datusch is the hasis for approval shall reuin in effect until sur and conditions rendered, suspended, revcked, or a lormination date is sherwise es tablished by the Administrater of the Federal Aviation Administration Dale applicatim: January 8, 1981 Jule missed: January 13, 1986; June 14, 1991 Galesfissuance: March 30, 1981 • June 14, 1991 FEDERAL NUTATION divinistrater нонг Acting Mgr., Special Certification Branch COMINISTRATD Seattle Aircraft Certification Office (Title)

47.

FAA FoR 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1195NW Limitations and Conditions: (Continued) Limitations and Conditions: of the original specification apply except as follows:

the conditions and limitations under which the Sic was issued and meets the prescribes the conditions and limitations under which the airworthiness requirements of the Federal Aviation Regulation 23.

Supplemental Type Certificate HOLDER: FLETCHAIR, INC.

1. MODEL AA-5B 4PCLM (NORMAL/UTILITY CATEGORY) AS MODIFIED BY STC SA1195NW Engine: Lycoming 0-360-A4K (Same as TCDS A16EA) Fuel: 100/300 minimum galions seable gasoline Capacity:

Engine Limits: For all operations: 2700 rpm (180 Hp) Propeller and Propeller Limits: Sensate 75EMg maximum reminin Diameter: minimum Placards: None C. G. Range: Same as Type Certificate Data Sheet No. A16EA Maximum Weight: 2400 pounds (Same as TCDS A16EA) Instrument Markings: Oil Temperature:

245• F Oil Inlet (Red Line) Oil Pressure:

60 to 90 psi (Green Arc) Cyl foder Heed Limperature (Bayonet Thermocouples) NOTE 1: Current weight and balance report including a 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 AlEA, Note 2, apply the following:

In full view of the pilot on the instrument panel:

NOTICE AIRCRAFT MODIFIED BY SENSENICH 76EM8SIO-0 SERIES PROPELLER IN ACCORDANCE WITH STC SA1195NW NOTE 3:

to or better FAA Approved Airplane Flight

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