# STC SA5835NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Teledyne Controls, United States
- Description: Installation of Teledyne Controls  Digital Flight Data Acquisition Unit
- Applied: March 9, 1992
- Status date: October 4, 2012
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A35EU](https://openairdocs.org/tcds/A35EU)
- Certificate PDF: https://openairdocs.org/files/sha256/6b/09/6b090f667e42a104335fa4cc595a2ffebba30c5a6b1937aa0288c89648ca566f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7C9C7C05B82EB59486257AA8004B3196.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5835NM

## ADs that name it (0)

None.

## Approved models (2)

- Airbus A310 200 Series ([TCDS A35EU](https://openairdocs.org/tcds/A35EU))
- Airbus A310 300 Series ([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

A310, model 200/300 Series Description of Type Design Change: Installation of Teledyne Controls’ Digital Flight Data Acquisition Unit in accordance with the FAA Approved Master Da ta List Drawing No. MDL 2227000-310, Revision IR, dated August 12, 1992, or later FAA approved revisions.

Limitations and Conditions: The approval of this change in t ype design applies only to the above-list model only. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft . If the holder agrees to permit another person to use this certificate to alter the pr oduct, 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 9, 1992

Date of issuance: September 9, 1992

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/sha256/6b/09/6b090f667e42a104335fa4cc595a2ffebba30c5a6b1937aa0288c89648ca566f)

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