# STC SA982SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Associated Air Center, Inc. - c/o CT Corporation System, USA
- Description: Installation of Collins FD109F and FD109H Flight Director Systems
- Applied: August 15, 1968
- Status date: January 29, 2018
- Product: Aircraft, Large Airplane
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA)
- Certificate PDF: https://openairdocs.org/files/sha256/38/06/3806b25c66841aea5eb1e811ebd87fbed80301102ee9e635ef68e37f49b792b5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156229710120230425161214.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA982SW

## ADs that name it (0)

None.

## Approved models (1)

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

## 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 (8/13) Page 1 Number:

Part of the Federal Av iation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

By direction of the Administrator Signature Title SA982SW Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 4b A12EA Grumman G-1159 Installation of Collins FD109F and FD109H Flight Director Systems in accordance with Drawings List 19113-1159, Sheets 1 and 2, dated October 13, 1968; or installation of FD109F and FD109H Flight Director Systems with INS coupling as an acceptable option to the basic flight directors when installed in accordance with Drawing List 19208-1159 dated May 30, 1969;

or installation of FD109Y/Z Flight Director Systems with INS coupling when installed in accordance with Drawing List 19208-1159, as revised May 16, 1972.

1. FAA Approved Flight Manual Supplements are required as follows: (a) Two Supplements dated 12/3/1968 with installation according to STC dated 12/3/1968; (b) Two Supplements dated 6/25/1969 when Revision 1 dated 6/25/1969 of this STC is incorporated; (c) Supplement dated 9/18/1972, when Revision 2 of this STC is incorporated.

2. STC's SA946SW and SA983SW must be incorporated with this STC if operation in vertical modes and altitude hold is desired.

3. STC SA945SW must be incorporated concurrently when Revision 1 or Revision 2 of this STC is installed.

Certification Basis of this STC refers to Part 4b of the Civil Air Regulations (CAR 4b).

8/15/1968 12/3/1968 6/25/1969; 9/18/1972 1/29/2018 Jose Mora-Vargas ODA Administrator ODA-710437-SW

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SA982SW

## Every issue (1)

- January 29, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/38/06/3806b25c66841aea5eb1e811ebd87fbed80301102ee9e635ef68e37f49b792b5)

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