STC SA2-1136

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2-1136 This certificate issued to: Signature Flight Support Corporation, a Delaware Corporation 7511 Lemmon Avenue, Hangar C Dallas, TX 75209 Certifies that the change in the type design for the following product with the limitations and conditions therofor as specified hereon meet's the airvorthiness requirement's of Part 42 of the CiVi1 Aix Regulations.

Original Product Type Certificate Number: 723 Make: Lockheed Model: 18 Description of Type Design Change:

Installed a Lear, Inc. rotary electric actuator No. 164EK in the carburetor air control valve linkage as per EAS Drawings #342565 and #342332 dated March 22, 1961, or later FAA approved revision.

Note: This actuator to be installed on aircraft modified in accordance with STC SA4-149.

Compatibility of this modification with other previously approved modifications must be determined by the installer.

Date of Application: March 22, 1961 Date Reissued: 7/10/92; 12/21/98; 8/31/00 Date of Issuance: March 23, 1961 Date Amended: May 26, 1982 Rev. 2 FEDERAL AVIATION y direction Administrator (Signature) S. Frances Cox TOMNISTRATIO Manager, Special Certification Office, Southwest Region (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type).

(Address of grantor) (Number and street) (City, Stake, and ZIP code) Extent of Authority (if licensing agreement): - Date of Transfer:

Signature of grantor (In ink):

FAA AC 69-5536