# STC SA01359AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerial Banners Mods LLC, United States
- Description: Installation of wing forward spar fuselage attachment assembly reinforcement.
- Applied: January 3, 1997
- Status date: May 20, 2014
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A10](https://openairdocs.org/tcds/2A10), [TCDS 2A8](https://openairdocs.org/tcds/2A8)
- Certificate PDF: https://openairdocs.org/files/sha256/74/ef/74ef41bf386caf6a2bde14638a746969482c808b13f03ed65b976248cb45a511
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D2570FEA33F2257C86257D510052262C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01359AT

## ADs that name it (0)

None.

## Approved models (2)

- Lavia Argentina S.A. (Laviasa) PA-25 ([TCDS 2A10](https://openairdocs.org/tcds/2A10))
- Lavia Argentina S.A. (Laviasa) PA-25 ([TCDS 2A8](https://openairdocs.org/tcds/2A8))

## 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.

FAA Form 8110-2 (5/14) Page 1 of 2

Number: SA01359AT

This certificate issued to: Aerial Banners Mods LLC 601 SW 77th Way Pembroke Pines, FL 33023

Part 3of the Civil Air Regulations for Normal Category aircraft and of Part 8 of the Civil Aeronautics Manuals for Restricted Category aircraft.

Original Product – Type Certificate Number: 2A8 (Normal Category) and 2A10 (Restricted Category) Make: Piper Model: PA-25

Installation of the wing forward spar fuselage attachment assembly reinforcement in accordance with The STC Solution, Inc. Installation Instructions, Document Number ST2548AT-A-INST, Revision A, dated March 3, 1997, or later FAA approved revision.

The STC Solution, Inc., Maintenance Instructions, Document Number ST2548AT-A-MT, Revision A, dated March 3, 1997, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.

Date of Application: January 03, 1997 Date Reissued: May 20, 2014 Date of Issuance: May 05, 1997 Date Amended:

Signature

Title Melvin D. Taylor Manager, ACE-115A Atlanta Aircraft Certification Office

FAA Form 8110-2 (5/14) Page 2 of 2

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (1)

- May 20, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/74/ef/74ef41bf386caf6a2bde14638a746969482c808b13f03ed65b976248cb45a511)

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