STC SA908NW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA908NK This certificate issued to: Terry I. Myers Purt 04 of the CIVI] Air Regulations.

Original Product - Type bertificate Number: A-696 Make: Taylorcraft Model: BC12-D graphs numbers 1 through 3.

Limilalins andbendilins: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Taylorcraft BC12-D, Serial Number 7624 only. A copy of this Certificate and Addendum Number SA908NW shall he maintained as part of the permanent records for the modified aircraft.

Date of Application: December 1, 1978 Date Reissued:

Date of Issuance: March 25, 1980 Date Amended:

FEDERAL AVIATION Charla Citihroder (Signature) TO MINISTRATO Chief, Engineering and Manufacturing Branch (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) March 25, 1980 Number: SA908NW Supplemental Type Certificate ADDENDUM NO. SA908NW The conditions and limitations of Type Certificate Data Sheet Number A-696 apply except where superseded by the following:

Regulations. prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Civil Air Supplemental Type Certificate Data Sheet, which is part of STC SA908NW, Supplemental Type Certificate HOLDER: Terry L. Myers I. TAYLORCRAFT BC12-D (LANDPLANE-NORMAL CATEGORY) AS MODIFIED BY STC SA908NW Engine: Continental A-65-8 (converted to -14) Engine Limits: 75 Hp @ 2675 rpm Fuel: 80/87 octane aviation gasoline Propeller: McCauley 1A90/CF7040 Propeller Limits: 85 Hp @ 2800 rpm *All else is the same as Type Certificate Data Sheet A-696.

- END - FAA FORM 8110-2-1 (10-69)

PAGE 3 OF 3 PAGES C FAA AC 73-2651