# STC SA3113WE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Thermal Aircraft Company, United States
- Description: Installation of flap gap fairing.
- Applied: September 6, 1975
- Status date: December 29, 1983
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/4f/52/4f52370ad5e88e6ccd27204d5f85ff03ea3cb0e474b9c14b0287b275b3e46f12
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A3FA2BEED01436CC85256CC2000A93FC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3113WE

## ADs that name it (0)

None.

## Approved models (19)

- 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))
- The Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company R182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company T182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company TR182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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 SA3113WE This certificate issued to: Thermal Aircraft Company Part 3 of the CiVil Air Engine Indud fye betiale Mitication basis. Regulalions, dated Nov. 1, 1949. *Refer to Type Certificate Data Sheet No. 3A13 for a Cessna Model: 182, 182A thru H, J thru N, P & Q, Description of Type Design Change: T182, R182, TR182 Installation of flap gap fairing in accordance with Thermal Aircraft Company Drawing No. 5 dated September 6, 1975.

Thermal Aircraft Company Drawings No. 2, 3, and 4 (September 6, 1975) contain production data for this assembly.

Limitations and Conditions: The approval of this change in type design applies basically to the above listed aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of Application: September 6, 1975 Date Reissued:

Date of Issuance: December 15, 1975 Jale mended August 22, 1977; December 29, 1983 EDERAL AVIATION By Direction of the Administrator OMINIS Supervisor, Aircraft Modification Section ames A (Signature) ruge 47

## Every issue (1)

- December 29, 1983: Amended, Current. [certificate](https://openairdocs.org/files/sha256/4f/52/4f52370ad5e88e6ccd27204d5f85ff03ea3cb0e474b9c14b0287b275b3e46f12)

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