# STC SA02292LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aero Transporte S.A. Dearborn and Flint Aviation Co. S.A., United States
- Description: Fuselage life limit extension.
- Applied: February 23, 2008
- Status date: March 24, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A23SO](https://openairdocs.org/tcds/A23SO)
- Certificate PDF: https://openairdocs.org/files/sha256/74/43/7443b72c2ddff31fedf1aa5fe25539e400526d27216f9f63f5a16d92acfce231
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C5A66BD80C78099B862576F80073225A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02292LA

## ADs that name it (0)

None.

## Approved models (1)

- Piper Aircraft Inc. PA-42 ([TCDS A23SO](https://openairdocs.org/tcds/A23SO))

## 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 Aero Transporte S. A., Dearborn and Flint Aviation Co. S.A.

1519 New Garden Rd. Apt 2A Greensboro, NC 27410 Part 23* of the Federal Aviation Regulations. *Certification basis is set forth Type Certificate Data Sheet Original Product Type Certificate Number :

A23SO Piper Aircraft, Inc.

PA-42 Description of Type Design Change: Fuselage life limit extension in accordance with the airworthiness limitations section of ATSC, Dearborn and Flint Aviation Co. Instructions For continued Airworthiness Report No ATSARD-2, Revision Level “A” dated March 16, 2010 or later FAA Approved Revisions to the airworthiness limitations section.

Limitations and Conditions: The revised airworthiness limitations only apply to the serial numbers listed in the airworthiness limitations section of ATSC, Dearborn and Flint Aviation Co. report No. ATSARD-2 when operated by Aero Transporte S. A. 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 airplane model series 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 : February 23, 2008

Date of issuance : March 24, 2010

( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office ( Title)

NOTE:

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Number (STC No.)

Number SA0xxxxLA Certification Basis:

## Every issue (1)

- March 24, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/74/43/7443b72c2ddff31fedf1aa5fe25539e400526d27216f9f63f5a16d92acfce231)

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