# STC SA7038SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Falcon Jet Corporation, United States
- Description: Installation of Honeywell inertial reference system.
- Applied: July 25, 1986
- Status date: June 14, 1993
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A46EU](https://openairdocs.org/tcds/A46EU)
- Certificate PDF: https://openairdocs.org/files/sha256/61/db/61dbbbd62cf0baf3cf32acaecef0366ceda131be280aafcd1e7df75d10ba5d88
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/06220D99441AB0F885256CC20056A0DE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA7038SW-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

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA7038SW-D This certificate issued to: Falcon Jet Corporation P.O. Box 967 Little Rock, Arkansas 72203 Part 25 of the Federal Aviation Regulations:

Original Product - Type bertificate Number: A46EU Make: Dassault Aviation Model: Mystere - Falcon 50 Description of Type Design Change:

Installation of the Honeywell Inertial Reference System in accordance with Drawing List Report No. F50-01088, Revision AJ dated 5-3-93, or later FAA approved revision.

See Page 2.

Date of Application: JUly 25, 1986 Date Reissued:

Date of Issuance: August 28, 1986 Date Amended: See page 2. 6-18-87, 8-26-87, 9-16-87 (Rev. 12) EDERAL AVIATION By Direction of the Administrator Enden Si. Boersma Andrew A. Boersmalignature) DAS8SW COORDINATOR (Title) 47 FAA FORM 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA7038SW-D Revision 12 Date Amended: 10-27-87, 10-21-88, 11-17-88, 1-6-92, 4-1-92, 4-23-92, 7-24-92, 4-27-93, 6-14-93.

One of the following FAA Approved Airplane Flight Manual Supplements is required.

a) Report Number 35541-2 Revision B, dated 6-16-87 or later FAA approved revision, when the F50-01088-503 installation is utilized.

b) Report Number 35541-3 dated 8-7-87 or later FAA approved revision, when the F50-01088-503 installation is utilized including Lasertrak NDU.

c) Report Number 35541-4 dated 9-16-87 or later FAA approved revision, when the F50-01088-505 installation is utilized thru revison status "y".

d) Report Number 35541-5 Revision B, dated 1-6-92 or later FAA approved revision, when the F50-01088-505 installation is utilized at revision status "AA" or later.

e) Report Number 35541-6 Revision A, dated 4-27-93 or later FAA approved revision, when the F50-01088-507 installation is utilized.

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

3) This STC utilizes STC SA5754SW, issued July 20, 1984, as a certification basis of compliance.

000, or imprisonment not exceeding 3 years. or hath FAA FORM 81102-1 (10-69) This certificate may be transferred in accordance with LAR 21.t7

**PAGE OF PAGES**

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP code) Exent of Authority (if licensing agreement) :

Signature of grantor (In ink) :

## Every issue (1)

- June 14, 1993: Amended, Current. [certificate](https://openairdocs.org/files/sha256/61/db/61dbbbd62cf0baf3cf32acaecef0366ceda131be280aafcd1e7df75d10ba5d88)

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