# STC SA7121SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Falcon Jet Corporation, United States
- Description: Installation of the Collins dual EFIS-85C(13/14) electronic flight instrument system.
- Applied: September 15, 1987
- Status date: May 17, 1990
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A33EU](https://openairdocs.org/tcds/A33EU)
- Certificate PDF: https://openairdocs.org/files/sha256/8a/81/8a815ee02919658ba058380595e7f2ab9b70dd75245454ca71578af241efd7a0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/87350DCA21329CE485256CC20056A18A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA7121SW-D

## 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

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.

Hratri j&cua of 3amca Bepartmcnt of (Transportation —federal 2toiation Administration Supplemental t:jipe Certificate

• "taufa-fi-f^nA ta*- SA7121SW-D Falcon Jet Corporation P.O. Box 967 Little Rock, Arkansas 72203 A^rf-e^^fnji^^Ae'jij^i^^ 25 Federal Aviation A33EU Avions Marcel Dassault - Breguet Aviation Falcon 10 Installation of the Collins Dual EFIS-85C( 13/14) Electronic Flight Instrument System in accordance with Drawing List Report Number FlO-01031, Revision J dated 9-22-88, or later FAA approved revision.

See page 2.

Mf^ *S][amtmA&a£0t*4i6 September 15, 1987 November 4, 1987 ^ ———— ^, 1-21-88; 6-6-88; 10-6-88;

5-17-90 Rev. 4

• tA Joeeph A. Sevart (Title)

This certificate may b* trantfemd in actardana with FAR 21.47.

FAA FOIM »l 10-J (10-*«)

Unitrd £tatu of ©epartmcnt of 'Cransportation— Jfederal SDiation administration Supplemental TCgpe Certificate(Continuation £heet) SA7121SW-D Rev. 4 Limitations and Conditions

1) FAA Approved Airplane Flight Manual Supplement, Report Number 35480-3 dated November 4, 1987, or later FAA approved revision, is required for EFIS-85C

(13).

2) FAA Approved Airplane Flight Manual Supplement, Report Number 35480-4, Rev.

A dated May 17, 1990, or later FAA approved revison, is required for EFIS-85C(14).

3) Compatibility of this modification with other previously approved modifications must be determined by the installer.

4) This STC utilizes STC SA1815CE, reissued December 7, 1982, as a Certification Basis of Compliance.

i1 i <,,Krnf:nn uj this certificate, is punishable by a jine oj nnt exceeding Si,000, or imprisonment not exceeding 3 venrs, m />'il A A FORM 8110-2-1 (1O-69) This ceriijicate may be Iranfjerrrd in accordanci iril/i 1-AR ^'l.-t PAGE 2 OF 2 PAGES

## Every issue (1)

- May 17, 1990: Amended, Current. [certificate](https://openairdocs.org/files/sha256/8a/81/8a815ee02919658ba058380595e7f2ab9b70dd75245454ca71578af241efd7a0)

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