What it approves
Installation of Alpha Omega Suspension System in place of original bungees or bungees and hydasorbs.
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.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate 14 CFR 21.120) FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3 Number: SA02214AK This certificate issued to:
Installation of Alpha Omega Suspension System in place of original bungees, or bungees and hydasorbs, in accordance with Alpha Omega Suspension System Master Drawing List BAR-18DL-1, Revision F, dated October 21, 2005, and Installation Instructions and Operations and Maintenance Instructions BAR18A-1, Revision E, dated October 21, 2005, or later FAA approved revision. Instructions for Continued Airworthiness are contained in the Installation Instructions and Operation and Maintenance Instructions BAR18A-1, Revision E, dated October 21, 2005, or later FAA approved revision.
Piper PA-18 series only: Installations restricted to S/N 18-3771 and S/N 18-3781 and subsequent when equipped with 5/16 bolt cabane V assembly P/N 30602-7.
Burl’s Aircraft, LLC P.O. Box 671487 Chugiak, AK 99567-1487 Original Product Type Certificate Number: * Make: * Model: * See FAA Approved Model List (AML) No. SA02214AK, dated August 18, 2005, for a list of approved airplane models and applicable airworthiness regulations.
Date of application: May 07, 2001 Date of issuance: May 26, 2004 Date reissued: March 18, 2022 Date amended: November 15, 2005 By direction of the Administrator Signature:
August A. Asay Title: Manager, Anchorage ACO Branch Part * of the * Regulations.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3
(Continuation Sheet) Number: SA02214AK
Date of application: May 07, 2001 Date of issuance: May 26, 2004 Date reissued: March 18, 2022 Date amended: November 15, 2005
Limitations and Conditions: (continued):
This STC is compatible with 3-inch extended main landing gear installed in accordance with STC SA02152AK or STC SA02175AK.
Compatibility of this design change with previously approved modifications must be determined by the installer.
The BAR18-2 AOSS Unit is a lower initial stiffness version of the BAR18 unit and is interchangeable on eligible aircraft with a gross weight above 1500 lb. Mixing the BAR18 and the BAR18-2 units on the same aircraft is not approved.
-END-
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3
Number: SA02214AK
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02214AK
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 25
| Make | Model | Data sheet |
|---|---|---|
| FS 2001 Corp. | J5A (Army L-4F) | A-725 |
| FS 2001 Corp. | J5B (Army L-4G) | A-725 |
| FS 2001 Corp. | J5C | A-725 |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 18, 2022 | Reissued, current | CertificateApproved model list |
| November 15, 2005 | Amended, earlier issue | CertificateSA02214AKAML |