# STC SA829EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aerosonic Corporation, United States
- Description: Installation of Teledyne Avionics Auto Throttle System No. SL104A100-1.
- Applied: February 4, 1970
- Status date: August 14, 2007
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A7EU](https://openairdocs.org/tcds/A7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/2c/81/2c81cdfe1c765517945bea1d88294691f40144a142a7db050c308a677fb286c5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CAF62B4BAE8EBC61862573D2005A9A00.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA829EA

## ADs that name it (0)

None.

## Approved models (3)

- Dassault-Aviation Fan Jet Falcon ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Fan Jet Falcon Series C ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Fan Jet Falcon Series D ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))

## 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.

Number SA829EA This certificate issued to Aerosonic Corporation 1212 North Hercules Avenue Clearwater, FL 33765

Part 4b of the Civil Air Regulations.

Original Product Type Certificate Number: A7EU

Make: Dassault Aviation

Model: Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D Description of Type Design Change:

Installation of Teledyne Avionics Auto Throttle System No. SL104A100-1 in accordance with data listed in Teledyne Avionics Drawing List No. D5392 Revision A, dated October 22, 1970.

1. Teledyne Avionics FAA Approved Airplane Flight Manual Supplement No. 2, dated October 26, 1979, is required with this installation.

2. Aircraft must have incorporated Avions Marcell Dassault Service Bulletin No. 155 (performance Kit) and the modifications of STC SA1137SW prior to or simultaneously with this installation.

3. Additional limitations are contained in the Limitations Section of the aforementioned A.F.M.S.

4. The Installer must determine whether this design change is compatible with previously approved modifications.

5. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Date of application: February 4, 1970

Date of issuance: June 19, 1970 Date reissued: January 7, 1972, July 1, 1976, March 8, 1993, August 14, 2007 Revision 2 Date amended: August 25, 1970, October 26, 1970

( Signature) Anthony Socias Manager New York Aircraft Certification Office

( Title)

## Every issue (1)

- August 14, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2c/81/2c81cdfe1c765517945bea1d88294691f40144a142a7db050c308a677fb286c5)

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