STC SA1028NW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1028NW This certificate issued to: Flightcraft, Inc.

Certifies that the change in the type design for the filliving freduct with the linitations and conditions therefer as specified heran muts the aimerthiness requirements f Part 3 of the Civil Air Regulations.

Original Product - Sype tortificate Number: 3A15 Make: Beech Model: A36TС Detect 15 as assetted system in borince waft fightcraft, Inc. photographs 1 through 8. This installation requires the rerouting of the right hand rudder control cable as per Flightcraft, Inc. Sketch No. 1 and photograph No. 6.

See "Continuation Sheet" Page 3 Limitatin und fendiline Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Beech A36TC, Serial Number EA-117 only. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.

Date of Application: September 18, 1980 Dude missued:

Date of Issuance: September 25, 1980 Date Amended: October 10, 1980 FEDERAL AVIATION Thales Gehredu (Signature ) TOMI NISTRATO Chief, Engineering and Manufacturing Branch (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Amended October 10, 1980 Number: SA1028N4 Description of Type Design Change: (continued):

NOTE: This aircraft will be operated in the Standard (Utility)/Restricted Category (Aerial Photography). While in Restricted Category, the Operating Limitations, dated September 25, 1980, and FAR 91.39 are applicable. A placard is to be placed on the instrument panel in full view of the pilot which reads:

CAUTION

TO OPERATE IN THE STANDARD AIR-

WORTHINESS CATEGORY, CAMERA SYS-

TEMS MUST BE REMOVED AND COVEF

PLATES MUST BE INSTALLED BEFORE FLIGHT

- END -

FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3PAGES C FAA AC 73-2651