# STC SA2522NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: GE Engine Services-Corporate Aviation Inc.
DBA Garrett Aviation Services, United States
- Description: Reinforcement of baggage compartment bulkhead and installation of a restraint net at F.S. 539.750 as specified by associated placards required to be installed in the cargo compartment.
- Applied: January 23, 1984
- Status date: July 30, 2003
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA)
- Certificate PDF: https://openairdocs.org/files/sha256/15/43/1543fbe5ce3daf2bcfd6943f430547ee83305d84cc251f199fa3ede498cceb59
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D86EC31E420DD12F86257505007BA248.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2522NM

## ADs that name it (0)

None.

## Approved models (3)

- Gulfstream Aerospace Corporation G-1159 ([TCDS A12EA](https://openairdocs.org/tcds/A12EA))
- Gulfstream Aerospace Corporation G-1159A ([TCDS A12EA](https://openairdocs.org/tcds/A12EA))
- Gulfstream Aerospace Corporation G-1159B ([TCDS A12EA](https://openairdocs.org/tcds/A12EA))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2522NM This certificate issued to: GE ENGINE SERVICES - CORPORATE AVIATION, INC.

DBA GARRETT AVIATION SERVICES 6201 WEST IMPERIAL HIGHWAY LOS ANGELES, CA 90045 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 4b of the Civil Air Regulations. December 31, 1953 Original Product Type Certificate Number: A12EA Make: Gulfstream Model: G-1159, G-1159A, G-1159B Description of Type Design Change: Reinforcement of Baggage Compartment Bulkhead and installation of a restraint net at F.S. 539.750, as specified by associated placards required to be installed in the cargo compartment, CAE report No. AIN-20 January 3, 1984 and sealed master drawing list Rev. J August 28, 1984 or later revisions approved by the FAA.

Limitations and Conditions: 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 introduce no adverse effect upon the airworthiness of that 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. A copy of this STC must be included in the permanent records of the modified aircraft.

Date of Application: January 23, 1984 Date Reissued: December 20, 1994, July 30, 2003 Date of Issuance: October 4, 1984 Date Amended:

FEDERAL AVIATION By direction of the Administrator Мии с Kuck (Signature) * cucting fer Manager, Technical & Administrative Support TOMINSTRATOS Staff, Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- July 30, 2003: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/15/43/1543fbe5ce3daf2bcfd6943f430547ee83305d84cc251f199fa3ede498cceb59)

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