# STC SA7072SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Falcon Jet Corporation, United States
- Description: Installation of the Bendix EFS-10 electronic flight instrument system.
- Applied: June 16, 1986
- Status date: September 30, 1987
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A46EU](https://openairdocs.org/tcds/A46EU)
- Certificate PDF: https://openairdocs.org/files/sha256/1e/3a/1e3a88d15e60e0dceac9567533ba445f485dab48b2b51ce463778b72308014ce
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/46B60674663CA7AE85256CC20056A124.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA7072SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Dassault-Aviation Mystere-Falcon 50 ([TCDS A46EU](https://openairdocs.org/tcds/A46EU))

## 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&tara Department of Transportation — federal 2toiation administration Supplemental 'Cgpe Certificate tSuvmvev*' SA7072SW-D Falcon Jet Corporation P.O. Box 967 Little Rock, Arkansas 72203 naf"ls 25 y^ Federal Aviation . sltat<ta/j A46EU Avions Marcel Dassault-Breguet Aviation Mystere - Falcon 50 _£4&tv«fi&(>n 4>f'Z!yfie>-j4AAam- T^Aanae* :

Installation of the Bendix EFS-10 Electronic Flight Instrument System in accordance with Drawing List Report Number F50-01114, Revision E dated 3-25-87, or later FAA approved revision.

See page 2.

rrnrivrm-if rtcriy^rnnVri; rrtTrrrrn; rr a fcrmtnaticn (fa/r tA fmtmilt* cm&~»: June 16, 1986 ^.4 ^^tl^- January 6, 1987 _^>- ff-Tr-V^v 4/21/87; 9/30/87 Rev. 2 S&~^IJoseph" A.' DAS8SW COORDINATOR __ _ L ^-l ^^__ aUtration of this certifieatt is punitkablt by a fine of not txcttding I/,000, or imfmsonmtnt not txcttding 3ytars, or both.

Tkii arttjttftt mty W trtntjtm^ m utar^uta with FAR 21.47.

ttnitrd 3tatu of amtrira Bcpartment of transportation— federal atriation administration Supplemental ITjipe Certificate(Continuation £heet) SA7072SW-D (Revision 2) Limitations and Conditions:

1) FAA Approved Airplane Flight Manual Supplement, Report No. 35827-1, Revision A dated September 30, 1987, is required when this system is interfaced with an FCS-90 Flight Control System.

2) FAA Approved Airplane Flight Manual Supplement, Report No. 35827-2, dated April 21, 1987 is required when this system is interfaced with an APS-85 Autopilot System.

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

.IM ^Iteration nf this certificate is punishable by a fine of not exceeding Sl,000, or imprisonment not exceeding 3 fears, or b^t^ ~AA FORM aiio-2-1 (10-69) This ctrlifica.lt may bi transferred in accordance wilh I'AR .'! ^~ PAGE 2 OF 2 PAGES

1 INSTRUCTIONS: The transferendowment beiow may be used to notify the appropriate FAA Regional Office of the tranifer of thU Supplemenul Type Certificate.

The FAA will reissue the certiSca.c in the name of the iransferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of Iransferee).

from (Name of grantor) (Print or type).

(Address of grantor) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- September 30, 1987: Amended, Current. [certificate](https://openairdocs.org/files/sha256/1e/3a/1e3a88d15e60e0dceac9567533ba445f485dab48b2b51ce463778b72308014ce)

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