# STC SA1467NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Theodore E Deusner Jr, United States
- Description: Installation of a new instrument panel and associated wiring
- Applied: March 18, 1981
- Status date: August 26, 1982
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A-799](https://openairdocs.org/tcds/A-799)
- Certificate PDF: https://openairdocs.org/files/sha256/b8/8b/b88b13bafd8f7054a98482b483208e308bec1a640ffb629e9cd5f814b63d5cbe
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E98A1F8C1986DA3386257A14006CED4C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1467NM

## ADs that name it (0)

None.

## Approved models (3)

- Cessna Aircraft Company 170 ([TCDS A-799](https://openairdocs.org/tcds/A-799))
- Cessna Aircraft Company 170A ([TCDS A-799](https://openairdocs.org/tcds/A-799))
- Cessna Aircraft Company 170B ([TCDS A-799](https://openairdocs.org/tcds/A-799))

## What the certificate says

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

Manited Starcs of Smerica Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A1467NM Tris coolificute, issued le Theodore E. Deusner, Jr.

Certifies that the change in the type design fer the fillewing praduct with the limitations and conditions thereferas specified heren mats the wireshines nquiremente if Part 03 & 3 / the CIVIT Air Pegulations:

Original Product - TypeCertificate Number: A-799 Alute: Cessna Mixtel: 170 Series LescriptinyLypeLign thunge: Installation of a new instrument panel and associated wiring in accordance with Theodore E. Deusner, Ur. Assembly Instructions and Master List No. 1050.

tinute undendins. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircrait of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate shall be maintained as part of the permanent records for the modified aircraft.

Date of Application: March 18, 1981 Lute reisued:

Tate sf insunce: March 5, 1982 Jalamended: august 26,1952 FEDERAL AVIATION Donel M Pedinsan clion of the Sidministraten TOMINISTAT STION citin [ Chief, Seattle Area Aircraft Certification Office, ANM-100S (Signature ) (Title)

47.

**FAA FORM 5110-2 (10-68)**

## Every issue (1)

- August 26, 1982: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b8/8b/b88b13bafd8f7054a98482b483208e308bec1a640ffb629e9cd5f814b63d5cbe)

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