# STC ST00132LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Teledyne Controls, United States
- Description: Requirements for the installation of Teledyne Controls  Digital Flight Data Management Unit (DFDMU)
- Applied: March 23, 1993
- Status date: October 4, 2012
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU)
- Certificate PDF: https://openairdocs.org/files/sha256/7a/3b/7a3b668b428898a805d89977b4c2ac90af366a482b97eb2ff5fcdbf361ce4eb1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/335207E20292BA3586257AA90044A11F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00132LA

## ADs that name it (0)

None.

## Approved models (8)

- Airbus A310-203 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-204 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-221 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-222 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-304 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-322 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-324 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310-325 ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))

## 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.

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 A35EU Original Product Type Certificate Number :

A35EU Airbus Industries A310-200, -300 Series Description of Type Design Change: Requirements for the installation of Teledyne Controls’ Digital Flight Data Management Unit (DFDMU) are contained in th e Teledyne Controls’ Master Data List for the installation of the Teledyne Controls DFDM U 2241000 on the Airbus A310 series aircraft, MDL2241000-A310, Rev. “IR”, dated July 25, 1995, or la ter FAA approved revisions. To determine which configuration(s) of the DFDMU have been a pproved, 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: March 23, 1993

Date of issuance: November 2, 1995

Date reissued: 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/sha256/7a/3b/7a3b668b428898a805d89977b4c2ac90af366a482b97eb2ff5fcdbf361ce4eb1)

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