# STC SA02052LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aeroplane Factory, United States
- Description: Installation of an electrical trim system for the horizontal stabilizer.
- Applied: June 12, 2003
- Status date: June 15, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-766](https://openairdocs.org/tcds/A-766)
- Certificate PDF: https://openairdocs.org/files/sha256/34/3b/343bf156497379aaa3296d9b007b6630a6c2b4e30f07b069e0b981ae72cacad7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2F801AC47BA0F2E68625730D005137B6.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02052LA

## ADs that name it (0)

None.

## Approved models (1)

- Swift Museum Foundation Inc. GC-1B ([TCDS A-766](https://openairdocs.org/tcds/A-766))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to Aeroplane Factory 885 Taildragger Road Gardnerville, Nevada 89410

Part 4a* of the Civil Air Regulations. *Certification basis is set forth in Type Certificate Data Sheet A-766 Original Product Type Certificate Number :

A-766 Globe GC-1B Description of Type Design Change: Installation of an electrical trim system for the horizontal stabilizer, in accordance with the Aeroplane Factory Master Drawing List, No. 603-100, Revision G, dated November 10, 2006, or later FAA approved revision. Maintain and operate in accordance with Instructions for Continued Airworthiness for the Aeroplane Factory Electric Trim Installed on the Swift GC-1B, No. ICA-Trim, Revision C, dated February 26, 2004, and Airplane Flight Manual Supplement for the Aeroplane Factory Electric Trim System installed on the Globe Swift, No. FMS-Trim, Revision IR, dated June 13, 2007 or later FAA approved revisions.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted aircraft models only. A copy of this STC must be included in the permanent records of the modified aircraft. 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.

Date of application : June 12, 2003

Date of issuance : June 15, 2007

Original signed by Gregory S. Dilibero ( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office ( Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- June 15, 2007: Issued, Current. [certificate](https://openairdocs.org/files/sha256/34/3b/343bf156497379aaa3296d9b007b6630a6c2b4e30f07b069e0b981ae72cacad7)

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