# STC SA7078NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Teledyne Controls, United States
- Description: Requirements for the installation of Teledyne Controls' Optical Quick Access Recorder (OQAR)
- Applied: August 26, 1993
- Status date: October 4, 2012
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/29/ad/29ad77d48057a6b7db66c25225831184284f2449b8127376096080c9853d4437
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1CE3619F76E57F7C86257AA800590658.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA7078NM

## ADs that name it (0)

None.

## Approved models (4)

- The Boeing Company 737-200 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-400 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-500 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## 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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate This certificate has been reissued to replace the original certificate reported as lost.

This Certificate issued to Teledyne Controls 501 Continental Boulevard El Segundo, CA 90245 Part 25* of the Federal Aviation Regulations.

*for certification basis see TCDS A16WE Original Product Type Certificate Number :

A16WE

Boeing

737-200, -300, -400, -500 Series Description of Type Design Change: Requirements for the installation of Teledyne Controls’ Optical Quick Access Recorder (OQAR) in accordance with FAA A pproved Teledyne Controls’ Master Drawing List No. MDL 2248000-737, Revision B, da ted April 19, 1994, or later FAA approved revisions. To determine which configurations of the OQAR have been approved, refer to the appropriate appendixes in the FAA Approved Master Data List.

Limitations and Conditions: This installation should not be inco rporated in any aircraft unless it is determined that the interrelationship between this in stallation and any previously approved configuration will not introduce any adverse effect upon the airworthin ess of the aircraft. Refer to the appropriate appendixes in the FAA Approved Mast er Data List for any other limitations. If the holder agrees to permit another person to use this certificate to alte r the product, the holder shall give the other person written evidence of that permission.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: August 26, 1993

Date of issuance: April 22, 1994

Date reissued: November 14, 1994, October 4, 2012

( Signature) Haifa Haj-Eid Supervisor, Technical and Administrative Support Staff Los Angeles Aircraft Certification Office ( Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

## Every issue (1)

- October 4, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/29/ad/29ad77d48057a6b7db66c25225831184284f2449b8127376096080c9853d4437)

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