STC SA1081SO

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Added Notes at Surrender:

Future unsafe conditions existing in the product can Number: SA108150 result in an airworthiness directive requiring correction of the unsafe condition before further flight. If there is no entity to comply-with-14 CFR This certificate issued to: Aeronautical Engineers, INC. 21,99(a), Required design changes, the existence of an unsafe condition might result in permanently grounding of the dircraf

2. Replacement parts might not be available in the future.

Certifies that the change in the type design for the following product with the limita therefor as specified hereon meets the airvorthiness requivements of Part Regulations.

Original Product -TypeCertificate Number: 4A22 Make: Lockheed STC Surrender processed Model: L-788C Approval by: Лан Suns elvin Taylor, ATL ACO Manager Description of Type Design Change: Make: 0/12/2007 Increase in zero fuel weight from 86,000 sated May 8, 1978 for later FAA ARE A ne in accordance with Aeronautical Engineer Drawing f2169, Keris todified Limitations and Conditions: to Lockneed Model L- fool Tannes this aproval sintant be extended to stally airplanes.

airplanes of this model on which other previously approved moditications are incorporated unless determined by the installer that the interrelationship between thi any of those other previously approved modifications will produce no advers fect upon the airworthiness of that airplane. This determination should include consideration of significant changes in weight distribution such as an the Liked disposable weist fathe fusettshall continued de Paid u supporting data us Federal Aviation Administration .

Date of Application: February 23, 1978 Date Reissued:

Date of Issuance: June 14, 1979 Date Amended:

TATION By Direction of the Administrator N. 1. Ірок W. S. Thomas, (Signalure) Acting Chief, OMIN Engineering and Manufacturing Branch Flight Standards Division (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA1081SO Limitations and Conditions: (Continued):

Airplane Flight Manual Supplement dated June 14, 1979, and Aeronautiçal Engineers, SURRENDER Inc., Report No. R-362-1, L-188 Weight and Balance Report dated November 15, 1974, are required parts of this Supplemental Type Certif Issued: June 14, 1979 JEND.

FAA FORM 8110-2-1 (10-69) PAGE 2 OF 2 PAGES FAA AC 72-4435