What it approves
Installation of wing leading edge stall strips
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may 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 wing leading edge stall strips in accordance with the Aeroplane Factory Master Drawing List, No. 507-001, Revision A, dated April 23, 2008, or later FAA approved revision. Operate in accordance with Supplemental Airplane Flight Manual for the Aeroplane Factory Machined Stall Strips installed on the Globe Swift, No. 507-002, Revision IR, dated May16, 2008 or later FAA approved revisions.
Limitations and Conditions: This installation requires that the wing leading edge slots remain operational.
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 13, 2007
Date of issuance : July 8, 2008
( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office ( Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Swift Museum Foundation Inc. | GC-1B | A-766 |