# STC SA1838NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: ELDEC Corporation, United States
- Description: Installation of Eldec Corporation9-45599901 Mass Fuel Flow Indicating System and any one of the optional 9-455999-02, -03, -04 totalizer indicator kits.
- Applied: November 1, 1982
- Status date: August 22, 1983
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A12EA](https://openairdocs.org/tcds/A12EA)
- Certificate PDF: https://openairdocs.org/files/sha256/74/86/74864d408f55f99b613a43c096f56860a7d740fa0693823f87dd872b66d88752
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DF95C416015FB33A85256CC10083D16B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1838NM

## ADs that name it (0)

None.

## Approved models (2)

- Gulfstream Aerospace Corporation G-1159 ([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: SA18388M This certificate issued to: Eldec Corporation Part 4b of the Civil Air Regulations. See Type Certificate Data Sheet No. AI2BA for complete certification Original Product Type tientificate Namber: A12EA Make: Gulfstream American (Grumman) Model:

G-1159, G-1159B Description of Type Design Change: Installation of Eldec Corporation 9-455999-01 Mass Fuel Flow Indicating System and any one of the optional 9-455999-02, -03, -04 Totalizer Indicator Kits in accordance with FAA sealed Eldec Corporation ID/PL 9-455999-01, Rev. No. 3, dated 1-26-83, ID/PL 9-455999-02, Rev. No. 2, dated 2-4-83, ID/PL 9-455999-03, Rev. No. 2, dated 2-4-83, ID/PL 9-455999-04, Rev.

Eldec Corporation FAA approved Airplane Flight Manual Supplement, Document No.

Jillo-and Cented February 24, 1983 is required. The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other aircraft of these models 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.

February 24, 1983 August 22, 1983 FEDERAL ATTATION By Direction of the Administrator ele C. Davis (Signature ) PAINIST AT T actigSupervisor, Aireraft Nodification Section 47

## Every issue (1)

- August 22, 1983: Amended, Current. [certificate](https://openairdocs.org/files/sha256/74/86/74864d408f55f99b613a43c096f56860a7d740fa0693823f87dd872b66d88752)

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