# STC SA7299SW-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Dassault Falcon Jet, United States
- Description: Installation of the No. 2 emergency power supply system.
- Applied: September 17, 1990
- Status date: July 15, 1996
- 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/a0/66/a066ea824f0dd34746cfa72208acd4055a8db90c58d59238de817021f5ab279d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F38345C3EACA3B7885256CC20056A295.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA7299SW-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.

Btpartmeitt of transportation— fttoal 2ttriation administration Supplemental ¥gpe Certificate U7299SW-D Dassault Falcon Jet P.O. Box 967 Little Rack, Arkansas 72203 jA&^u*we>i^^^ 25 ^j£e, Federal Aviation A46EU Dassault Aviation ////. Mysterc - Falcon 50 Installation of the No. 2 Emergency Power Supply System in accordance with Drawing List Report No. F50-OW16, Revision M dated 3-30-96, or later FAA approved revision.

See Page 2.

da^j^ / / / // '.4&?<??u>zxWi^?t/.^u&^x*£i#»<<£«<^.^4£z^!^^ & ' September 17, 1990 ».- February 7,1991 QLt.*^*^: 7-12-93,7-15-96 Rev. 2 A—tA A j AD (Siputun)Andrew A. Boersma DAS8SW COORDINATOR (TitU)

This certificate may bt transferred in accordance with FAR 21.47.

FAA Fot» S M 0-2 (10-68)

Btpartmm ef Transportatiwi-jfttoal atfetim adnfnfstntin Supplemental *Cgpe Certificate(Continuation gtect) SA7299SW-D Revision 2 Limitations and Conditions:

1) FAA Approved Airplane Flight Manual Supplement Report Number 35263-2, Revision A dated 7-12-93 or later FAA approved revision, is reauired when the F50-01016-505 installation is utilized.

2) FAA Approved Airplane Flight Manual Supplement Report No. 35263-3, dated July 15, 1996 or later FAA approved revision, is reauired what the F50-01016-507 installation is utilized.

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

4) This STC utilizes STC SA4573SW, issued 12-21-81, as a certification basis of compliance.

5) Periodic Maintenance Testing of the PS-855 Power Supply is reauired in accordance with J.E. T.

Installation Manual 24-30-06.

'-H Any alteration of this etrtifaatt is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

rAA FOMM •no*l (M4I) TV* t*t$utt my fc tratufirrid M tctmiattt witk FAR 21.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, Xlale, and <7P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) ( Cilr. Stale, and ^IP rode I Extent of Authority (if licensing agreement): _ Date of Transfer:.

Signature of grantor (In ink):__

## Every issue (1)

- July 15, 1996: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a0/66/a066ea824f0dd34746cfa72208acd4055a8db90c58d59238de817021f5ab279d)

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