STC SA02262AK

Supplemental type certificate · Northern Airframes LLC

Holder
Northern Airframes LLC · United States
Status
Current · Reissued
Status date
January 16, 2008
Applied
May 6, 2005
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDS1A2

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Manufacture weld-on float fittings in accordance with Airframes, Inc., Master Drawing List AF591078, Revision A, dated November 24, 2005, or later FAA approved revision. Install in accordance with Installation Instructions II591078, Revision O, dated February 22, 2006, or later FAA approved revision. Maintain in accordance with Instructions for Continued Airworthiness ICA591078, Revision O, dated November 28, 2005, or later FAA accepted revision

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 Northern Airframes, LLC.

20130 Birchwood Loop Spur Road Chugiak, AK 99567

Part 23 of the Federal Aviation Regulations

Original Product — Type Certificate Number: 1A2 Make: The New Piper Aircraft, Inc.

PA-18, PA-18S, PA-18 “105”, PA-18S “105”, PA-18A, PA-18 ”125”, PA-18S “125”, PA-18AS “125”, PA-18 “135”, PA-18A “135”, PA-18S “135”, PA-18AS “135”, PA-18 “150”, PA-18A “150”, PA-18S “150”, PA-18AS “150”

Description of Type Design Change: Manufacture weld-on float fittings in accordance with Airframes, Inc., Master Drawing List AF591078, Revision A, dated November 24, 2005, or later FAA approved revision. Install in accordance with Installation Instructions II591078, Revision O, dated February 22, 2006, or later FAA approved revision.

Maintain in accordance with Instructions for Continued Airworthiness ICA591078, Revision O, dated November 28, 2005, or later FAA accepted revision

Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed above only.

This approval should not be extended to other aircraft of these models 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 record 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: May 6, 2005 Date reissued: January 16, 2008 Date of issuance: March 1, 2006 Date amended:

( Signature) Gregory J. Holt Manager, Anchorage 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.

No AD in this release names this STC

Approved models · 16

MakeModelData sheet
The New Piper Aircraft Inc.PA-181A2
The New Piper Aircraft Inc.PA-18-105 (Special)1A2
The New Piper Aircraft Inc.PA-18-125 (Army L-21A)1A2
See all 16 models

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
January 16, 2008Reissued, currentCertificate
March 1, 2006Issued, earlier issueCertificate