# STC SA1042EA

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Northrop Grumman Comm Aircraft Div, United States
- Description: Installation of a hydraulically actuated target type thrust reverser system.
- Applied: February 14, 1974
- Status date: April 28, 1998
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A33EU](https://openairdocs.org/tcds/A33EU)
- Certificate PDF: https://openairdocs.org/files/sha256/b9/c5/b9c56a3dc08f6e77391cc61b79119ea55cffa8e02e024f8c1ab08302a39cdf8b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3AD15D56271087C285256CC10080DCC3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1042EA

## ADs that name it (0)

None.

## Approved models (1)

- Avions Marcel Dassault - Breguet Aviation Falcon 10 ([TCDS A33EU](https://openairdocs.org/tcds/A33EU))

## 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: SA1042EA This certificate issued to: Northrop Grumman Commercial Aircraft Division Post Office Box 9015 Stuart, Florida 34995-9015 Part 23/36 of the Federal Aviation Poegulations Original Product - Typs Certifioats Number: АЗЗЕО Make: Avions Marcel Dassault - Breguet Aviation Model: Falcon 10 Description of Type Design Change:

Installation of a hydraulically actuated target type thrust reverser system in accordance with Grumman Aerospace Corporation Installation Drawing No. C43B21000 and Master Drawing Index F10A-5-ACTR-MI Revision AJ dated November 4, Installation Instructions No. PMFJC-MA76-6 Revision G dated January 11, 1983..

1. AiResearch engine models TFE731-2 or -3 modified in accordance with STC SE1040EA, amended June 30, 1983, or November 17, 1987, prior to or concurrent with this modification are required with this installation.

2. This installation is approved for ground use only up to a maximum reverse thrust with fuel control computer in "ON" mode. The trust reversers are limited to 20,000 flight hours. (See Continuation Sheet, Page 2)

Date Reissued: November 10, 1997 Date of Application: February 14, 1974 Date Amended: 2/11/77, 5/31/77, 7/11/78, Dato fisuanos: November 8, 1976 10/1/81, 6/30/83, 11/17/87 By Direction of the Administrator FEDERAL AVIATION (Signaptre) Anthony Socias Manager, Airframe and Propulsion Branch TOMINSTRATO New York Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1042EA Limitations and Conditions: (Continued):

3. Grumman Aerospace Corporation Flight Manual Supplement No. 1, PMFJC-MA76-4, Revision 7, FAA approved October 20, 1987, to the Falcon 10 Airplane Flight Manual is required with this installation.

4. Engine must be equipped with AiResearch bypass inner segment (air-cooler fairing) P/N 3072751-1 which has a life limit of 20,000 hours.

5. Grumman Aerospace Corporation Falcon 10 Maintenance Manual Supplement PMFJC-MA76-1, Revision 10, dated September 1987, and System Maintenance and Overhaul Manual with Illustrated Parts Lists for Thrust Reverser Model No. F10A Document No. PMEJC-MA76-2, Revision 8, dated January 1983, are required for this installation.

6. Grumman Aerospace Corporation Flacon 10 Inspection Schedule is included in Falcon 10 Maintenance Manual Supplement PMFJC-MA76-1, Revision 10, dated September 1987.

7. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

8. 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.

NOTE: This installation incorporates multiple thrust reverser door locking devices, and automatic throttle retarder system, emergency stow switches and visual and aural warning indicators.

FAA Form 8110-2-1 (10-69) Page 2 of 2

## Every issue (1)

- April 28, 1998: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b9/c5/b9c56a3dc08f6e77391cc61b79119ea55cffa8e02e024f8c1ab08302a39cdf8b)

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