# STC SA1132WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Rogerson ATS, United States
- Description: Installation of an underwing pressure refueling system and fuel level indicator
- Applied: November 29, 1965
- Status date: April 12, 1991
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 6A6](https://openairdocs.org/tcds/6A6)
- Certificate PDF: https://openairdocs.org/files/sha256/bd/57/bd57cf35945396793181e90546c54383f8794ffb604b523c89841677033c5bc0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9179CB00ECEE240A86257A36004DADF1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1132WE

## ADs that name it (1)

- [AD 67-33-03](https://openairdocs.org/ad/67-33-03): Pressure Fueling Valves · Kelowna Flightcraft R & D 240 Series, 340 and 440 with STC SA1054WE or 3 others. Effective Oct 3, 1972. Named in the applicability

## Approved models (2)

- Kelowna Flightcraft R & D Ltd. 340 ([TCDS 6A6](https://openairdocs.org/tcds/6A6))
- Kelowna Flightcraft R & D Ltd. 440 ([TCDS 6A6](https://openairdocs.org/tcds/6A6))

## 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: SA1132WE This certificate issued to: ROGERSON ATS Part Ab of the Civil Aviation Reguitations.

Original Product -Type Certificate Numben: 6A6 Make: General Dynamics Model: 340 and 440 Description of Type Design Change:

Installation of an underwing pressure refueling system and fuel level indicator in accordance with either FAA approved Aircraft Tank Service Drawing No. 2361, Revision D dated July 19, 1968, or Aftermarket Technologies Master Drawing List MDL 236100, Revision N/C dated January 31, 1987, or later FAA approved revision.

This approval should not be extended to other specific airplanes of these models 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 airplane.

Date of Application: November 29, 1965 Date Reissued: April 6, 1987; April 12, 1991 Date of Issuance: January 13, 1966 Jate unended: April 6, 1987; April 7, 1987 FEDERAL AVIATION By Direction of the Administrator Apon, sen Sharlen *MINISTRATIO por Manager, Los Angeles Aircraft Certification Office (Title ) 47 FAA FORM 8110-2 (10-68)

## Every issue (1)

- April 12, 1991: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/bd/57/bd57cf35945396793181e90546c54383f8794ffb604b523c89841677033c5bc0)

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