# STC SA03139AT

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Rawson Rod, United States
- Description: Conversion of Cessna Models 182, 182A, 182B, 182C, and 182D from a Tricycle Landing Gear (nose wheel) to a Conventional Landing Gear (tail wheel) configuration.
- Applied: April 4, 2005
- Status date: August 18, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/d8/f4/d8f400ef2f613abdbfc135c647bf497840cd718801dddb4297df2b5dc9f5cdbb
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/75543856B75840B4862571FD0058BDB7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03139AT

## ADs that name it (0)

None.

## Approved models (5)

- The Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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.

FAA FORM 8110-2(10-68) PAGE 1 of 1 PAGES Number SA03139AT This certificate issued to Rod Rawson PO Box 1242 Anna Maria, FL 34216

Part 3 of the Civil Air Regulations.

Original Product--Type Certificate Number : 3A13 Make : Cessna Model : 182 , A, B, C, D

Conversion of Cessna Models 182, 182A, 182B, 182C, and 182D from a Tricycle Landing Gear (nose wheel) to a Conventional Landing Gear (tail wheel) configuration in accordance with Michael Stohler Installation Instructions, Report RS-180, “Tail Wheel Modification Procedure”, dated April 2, 2005, or later FAA approved revision.

Limitations and Conditions: Michael Stohler Report RS-182, “Instructions for Continued Airworthiness”, dated April 2, 2005, is a required part of this STC. The compatibility of this design change with other previously approved modifications must be determined by the installer. If the holder of this STC 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 : April 04, 2005

Date of issuance : August 18, 2005 Date reissued :

( Signature) Melvin D. Taylor Manager, ACE-115A Atlanta Aircraft Certification Office

(Title)

## Every issue (1)

- August 18, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d8/f4/d8f400ef2f613abdbfc135c647bf497840cd718801dddb4297df2b5dc9f5cdbb)

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