What it approves
Fabrication of Airframes Alaska LLC Heavy Duty Standard Length or 3-inch Extended Main Landing Gear
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.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3
Number: SA02175AK This certificate issued to:
(Continued on Page 3 of 3)
Airframes Alaska, LLC 81 East Commercial Drive Palmer, AK 99645
Type Certificate Number: 1A2
Make: Piper
Model: PA-18, PA-18S, PA-18 “105” (Special), PA-18S “105”(Special), PA-18A, PA-18 “125” (Army L-21A), PA-18S “125”, PA-18AS “125”, PA-18 "135" (Army L-21B), PA-18A “135”, PA-18S “135”, PA-18AS “135, PA-18 “150”, PA-18A “150”, PA-18S “150”, PA-18AS “150”
Date of application: February 23, 2001
Date of issuance: May 14, 2001 Date reissued: January 16, 2008
Date amended: January 7, 2013;
March 14, 2023 By direction of the Administrator
August A. Asay Title: Manager, Anchorage ACO Branch
Part 3 of the Civil Air Regulations.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3
Number: SA02175AK
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02175AK
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3
(Continuation Sheet) Date of application: February 23, 2001 Date of issuance: May 14, 2001 Date reissued: January 16, 2008 Date amended: January 7, 2013, March 14, 2023
Number: SA02175AK
(Continuance from Page 1 of 3)
Fabrication of Airframes Alaska, LLC steel “Heavy Duty” Standard Length or 3-inch Extended Main Landing Gear, in accordance with Airframes Alaska LLC Master Data List, Document No.
MDL-AI-01-01, Revision B, dated November 17, 2012, and installation in accordance with USAF T.O. 1L-21A-2, Sections 2-81 through 2-88, Main Landing Gear, revised October 14, 1955, or later FAA approved revisions.
- or - Fabrication of Titanium Main Landing Gear, in accordance with Airframes Alaska LLC Master Data List Document No. MDL-AI-01-02, Revision C, dated November 10, 2022, and installation in accordance with Installation Instructions and Instructions for Continued Airworthiness, PA-18 Series Titanium Landing Gear, revision B, dated March 14, 2023, or later FAA approved revisions.
1) The installer must determine whether the design change is compatible with previously approved modifications.
2) The steel gear is a direct replacement part, and the FAA has determined no Instructions for Continued Airworthiness are required. 14 CFR Part 43 is adequate to ensure continued airworthiness of the steel landing gear modification.
3) Maintain the titanium 3-inch Extended Main Landing Gear in accordance with Airframes Alaska Installation Instructions and Instructions for Continued Airworthiness, PA-18 Series Titanium Landing Gear, revision B, dated March 14, 2023, or later FAA approved revisions.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 16
| Make | Model | Data sheet |
|---|---|---|
| Piper Aircraft Inc. | PA-18 | 1A2 |
| Piper Aircraft Inc. | PA-18-105 (Special) | 1A2 |
| Piper Aircraft Inc. | PA-18-125 (Army L-21A) | 1A2 |
Every issue · 4
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| March 14, 2023 | Amended, current | Certificate |
| January 7, 2013 | Amended, earlier issue | Certificate |
| January 16, 2008 | Reissued, earlier issue | Certificate |
| May 14, 2001 | Issued, earlier issue | Certificate |