# STC SA3454WE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Mission Avn Fellowship, United States
- Description: Installation of an emergency fuel system.
- Applied: July 22, 1976
- Status date: February 7, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/21/eb/21ebf4f632712a9f265ebd48d51217b5a1739406f519d0639a61f9c14074496c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7AFAF1797554310085256CC2000A983E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3454WE

## ADs that name it (0)

None.

## Approved models (4)

- The Cessna Aircraft Company TU206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- The Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- The Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- The Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## What the certificate says

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

United States of America Supplemental Type Certificate Department of Transportation Federal Aviation Administration SA7249WE Number: SA3454N This certificate issued to: Mission Aviation Fellowship Part 3* of the CIVI1 Air Regulatims: *Certification basis is set forth on Type Certificate Data Sheet A4CE, Revision 21 Original Product - Type Berlificate Number: A4 CE Make: Cessna Model: U206F, U206G Description of Type Design Change: TU206F, TU206G Installation of an emergency fuel system in accordance with Mission Aviation Fellowship Drawing List 508A-000, Revision "D" or later sealed revisions, Supplemental Type Certificate SE80WE or SE88WE are required as part of this installation. FAA-approved Mission Aviation Fellowship Airplane Flight Manual dated February 7, 1978, or later FAA-approved revision is also required as part of this installation.

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: JUly 22, 1976 Date Reissued:

Date of Issuance: September 12, 1977 Dalcumended: November 2, 1977; Feb. 7, 1978 FEDERAL AVIATION By Direction of the Administrator (Signglure) Chief, Aircraft Engineering Division (Title)

## Every issue (1)

- February 7, 1978: Amended, Current. [certificate](https://openairdocs.org/files/sha256/21/eb/21ebf4f632712a9f265ebd48d51217b5a1739406f519d0639a61f9c14074496c)

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