STC SA4-1629

Part * of the * Federal Aviation R egulations. (See page 3 of 3 for complete certification base).

Original Product --Type Certificate N umber :

Installation of Wing Tip Fuel Tanks in accordance with J. L., Osborne Installation Instruction Instructions as listed on AML No. SA4-1629, or later FAA approved revision and Master Drawing List (MDL) No. T-68, dated January 14, 1965, or later FAA approved revisions.

This STC has been determined to be a non acoustic change in accordance with § 21.93(b) when incorporated on the G36 model airplanes.

Limitations and Conditions: The approval of the change in type design applies to the basic airplane of the specified model that is otherwise unmodified. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. See Continuation Sheet on Page 3.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

General Aviation Modifications, Inc.

2800 Airport Road Ada, OK 74820 **See attached FAA Approved Model List (AML) M ake : * No. SA4-1629 for list of approved airplane models M odel : * and applicable airworthiness regulations.

Date reissued : 11/10/1969; 02/02/19 71; 09/17/1987;

9/29/2009; 2/07/2020 Date amended : 12/26/1961; 03/12/1963; 01/23/1962;

01/27/1965; 12/14/1983; 04/23/1992; 04/17/2008

B y direction of the A dministrator

(Signature) Monica Nemecek Manager, Airframe & Administrative Section Chicago ACO Branch

(Title)

Date of application : September 24, 1961

Date of issuance : November 9, 1961

FAA FORM 8110-2-1(10-69) PAGE 2 of 3 PAGES

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 of type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

N umber SA4-1629 Date of issuance: November 9, 1961 Date Amended : April 17, 2008 Date Reissued: February 7, 2020

Limitations and Conditions ( Continued):

The Wing Tip Fuel Direct Engine Feed System is applicable to all eligible aircraft (items 1.1 through 1.21) listed in Item Section of the AML. The Wing Tip Tank Fuel Transfer System is applicable to all eligible aircraft (items 2.1 through

2.11) listed in Item Section of the AML with two 40 U.S gallon main fuel tanks only.

A copy of this certificate and AML No. SA4-1629 dated April 23, 1992, or later FAA approved revision, must be maintained as part of the permanent records of the modified aircraft.

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