# STC SA1851WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rogerson ATS, United States
- Description: Installation of a single point pressure fueling system.
- Applied: March 29, 1967
- Status date: April 19, 1991
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A7EU](https://openairdocs.org/tcds/A7EU)
- Certificate PDF: https://openairdocs.org/files/sha256/07/0d/070d50f66a755fc141f8d86372c8180997c82cb5dadaf5f238827b645e78254d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/61316208FC1A83EE862572AA00486475.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1851WE

## ADs that name it (1)

- [AD 82-18-09](https://openairdocs.org/ad/82-18-09): Refueling System · Single point pressure fueling system (Rogerson ATS STC SA1851WE or 4 others). Effective Oct 4, 1982. Named in the applicability

## Approved models (6)

- 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))
- Dassault-Aviation Fan Jet Falcon Series E ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Mystere-Falcon 20 - C5 ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Mystere-Falcon 20 - D5 ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))
- Dassault-Aviation Mystere-Falcon 20 - E5 ([TCDS A7EU](https://openairdocs.org/tcds/A7EU))

## What the certificate says

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

05/23/06 TUE 13:51 FAX 562 627 5210 FAA LAACO 2ND FLR WEST 4008 *niced Scotce of Stacie Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1851WE This certificate issued to: 16940 Von Karman Avenue Rogerson ATS Irvine, California 92606 Certifies that the change in the type design for the following preduct with tho limitations unsh conditions shonfon as specified heren meets the airwanthiness requinments of Port Ab* of the Civil Air Regulalions. * certification basis as set forth in Type Certificate Data Sheet ATU.

Original Product _Izype Cortificate Number: ATEV Мако: Dassault/Sud Merdal: **See Page 3 Description of Type Design Change:

Installation of a single point pressure fueling system in accordance with FAA sealed Aircraft Tank Service, Inc., Summary Drawing No. 2554, Revision "G" or later FAA approved Revision.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

January 10, 1969 Sole eeceeded: April 6, 1971; June 16, 1977;

FEDERA Ay divestion of the SIde sinistrali mov (Signature ) June 20, 1989 PHINISTRATOR a Manager, Los Angeles Aircraft Certification Office (Title)

FAA FORM 8 1 10-2 (10-48) Page 1 of 3

05/23/06 TUE 13:52 FAX 562 627 5210 FAA LAACO 2ND FLR WEST Z1007 Ented States of Slanica

• 01/10/69 Department of Transportation Federal Aviation Administration (K) 06/20/89; Supplemental Type Certificate 04/19/91 (A) 04/06/71; (Contination Sheet) 06/20/89 06/16/77; Number: SA1851WE Model: **Fan Jet Falcon, Fan Jet Falcon Series C, Fan Jet Falcon Series D, Fan Jet Falcon Series E, Mystere Falcon 20-C5, Mystere Falcon 20-D5 and Mystere Falcon 20-E5.

**FAA FORM 8110-7-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (1)

- April 19, 1991: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/07/0d/070d50f66a755fc141f8d86372c8180997c82cb5dadaf5f238827b645e78254d)

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