# STC SA02376AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Stoots Aviation David S. Stoots, United States
- Description: Replacement of tricycle landing gear with conventional (tail-wheel) landing gear
- Applied: December 12, 2005
- Status date: December 12, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17)
- Certificate PDF: https://openairdocs.org/files/sha256/9a/d7/9ad715c506bab7a397decdb5163c547660247af9947088950f4e266b554330a9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9862ADC83950D1AC8625780600576454.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02376AK

## ADs that name it (0)

None.

## Approved models (7)

- Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 175 ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175A ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175B ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175C ([TCDS 3A17](https://openairdocs.org/tcds/3A17))

## 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.

This certificate issued to Stoots Aviation David A. Stoots 3686 University Ave Fairbanks, AK 99709

Part 3 of the Civil Air Regulations

Original Product — Type Certificate Number: 3A12 3A17 Make: Cessna Cessna Model : 172, 172A, 172B 175, 175A, 175B, 175C

Description of Type Design Change: Replacement of tricycle landing gear with conventional (tailwheel) landing gear in accordance with Stoots Aviation Master Drawing List DSA 172/175-1, Revision A, dated October 12, 2010, or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. For Instructions for Continued Airworthiness, reference Stoots Aviation Instructions for Continued Airworthiness DSA-172-175 ICA, Revision IR, dated September 3, 2010, or later FAA accepted revisions.

3. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: December 12, 2005 Date reissued:

Date of issuance: December 2, 2010 Date amended:

( Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

( Title)

## Every issue (1)

- December 12, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/9a/d7/9ad715c506bab7a397decdb5163c547660247af9947088950f4e266b554330a9)

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