STC SA4061WE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA406 INE This certificate issued to: Monte L. Zema Purt 04 of the CiviL AiT Regulations. See page 3 for complete certification basis.

Original Product - Type Gertificate Number: A-766 Make: Swift (Globe) Model: GC- 1B Installation of dual control sticks in accordance with an FAA sealed copy of Chuck Lischer Aircraft Drawing No. SDS-101, dated August 7, 1979, or later FAA approved revision and either Chuck Lischer Aircraft Installation Instructions No.

SDS-101, dated November 7, 1984, or later FAA approved revision, or Custom Swift Modification Instructions No. SDS-101, Revision "A", dated February 15, 1984, or later FAA approved revision.

Limitations and Conditions: . Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, must be maintained as part of the permanent records for the modified aircraft.

Date of Application: September 15, 1978 Date Reissued: January 19, 1983; August 30, 1983 Date of Issuance: November 20, 1979 Date Amended: March 28, 1984

FEDERAL AVIATION ( Signature) TENNIS RAIDS Acting Manager, Seattle Aircraft Certification Office (Title) 47 FAA FORM 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 11/20/79 (I) (Continuation Sheet) 01/19/83 (R) 08/30/83 (R) Number: SA406 1ME 03/28/84 (A) Eligibility:

This alternation meets the flight characteristics requirements with engines of up to 150 hp. that were installed using the engine mount approved by STC SA2-1007 (thrust line inclined 226° downward).

Required Equipment:

In addition to the equipment applicable and required by Aircraft Specification No. A-766, the equipment specified by Chuck Lischer Aircraft Drawing No. SDS-101, Swift Dual Stick Control System, dated August 7, 1979, or later FAA approved revision, must be installed as a result of the incorporation of this STC.

Certification Basis:

Part 04 of the Civil Air Regulations effective November 1, 1943 plus Amendments 04-1 thru 04-5 inclusive. Under provisions of CAR 04.00 (1), the applicant was permitted to use the requirements of FAR 23 effective February 1, 1965 plus Amendments 23-1 thru 23-22 for the complete structural substantiation.

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FAA FORM B110-2-1 (10-69) PAGE 3 OF 3 PAGES