# STC SA5867NM

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Installation of Bendix/King traffic alert and collision avoidance system(TCAS II).
- Applied: September 17, 1992
- Status date: June 19, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA)
- Certificate PDF: https://openairdocs.org/files/sha256/64/3d/643dbba13d51bc914cc018921e2c3b1f6805b3fe34e21e2d905fa0e7a17f2bf6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1BD9D71CFB49669C862575EC0067C6DB.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5867NM

## 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: SA5867NM This certificate issued to: Hollingsead International SURRENDERED Certificate 2226 Goodyear Avenue Ventura, CA 93003 on - 6-19-09 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereen meets the airworthiness requirement's of Part *25 of the * Federal Aviation Regulalions. *Certification basis is set forth in Type Certification Data Sheet.

Original Product Type Certificate Number : A12EA Abake Gulfstream

•Abodel G-1159, G-1159A, G-1159B Description of Type Design Change: Installation of Bendix King Traffic Alert and Collision avoidance System (TCAS II) in accordance with FAA approved Hollingsead International Master Drawing List 10883, Revision "N/C", dated November 19, 1992, or later FAA approved revision, For appropriate FAA approved Airplane Flight Manual supplement refer to associated section of the Hollingsead International Master Drawing List.

Limitations and Conditions: 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 affects upon airworthiness of the 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: September 17, 1992 Late reirmed : December 3, 1998; April 25, 2002 May 7, 2007 Date of Issuance: December 11, 1992 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Calta K. W00 (Signature) TOMINSTRATO Los Angeles Aircraft Certification Office Manager, Technical & Administrative Support Staff

FAR Form 8110-2 (10-68) Page 1 of 2

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP Code) from (Name of grantor) (Print or type).

(Address of grantor)_ (Number and street) (City, State, and ZIP Code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

* U.S. GPO 1987-763-289 Page 2 of 2

## Every issue (2)

- June 19, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/64/3d/643dbba13d51bc914cc018921e2c3b1f6805b3fe34e21e2d905fa0e7a17f2bf6)
- May 7, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/39/ca/39cae95243c5df4e545a8f027061c705a81b53b520bc3e5fb27af7ca7f477794)

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