# STC SA1021SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Peterson Aircraft Repair, United States
- Description: Installation of flap on switch on control wheel.
- Applied: April 9, 1969
- Status date: September 16, 1977
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS A6CE](https://openairdocs.org/tcds/A6CE)
- Certificate PDF: https://openairdocs.org/files/sha256/52/b2/52b2cc18124ac0a92cf073a300680fada195004046f3eebd636dd92a46ef07d6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F20CD94CCF833E1286257D3F006E88FF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1021SW

## ADs that name it (0)

None.

## Approved models (25)

- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 210-5 (205) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210-5A (205A) ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210C ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210D ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210E ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 337 ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company 337A ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company 337B ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company 337C ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company 337D ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company T337B ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company T337C ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company T337D ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- Cessna Aircraft Company U206 ([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 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA102154 This certificate issued to: Peterson Aircraft Repair 5104 Rector Fort Worth, Texas 76133 Part 3 of the CIVIL AIx Regulations:

Original Product -TypeCertificate: Number: 3A13, 3A21, A4CE, AGCE Make: Cessna Model: See Limitations and Conditions Description of Type Design Change: Installation of flap up switch on control wheel in accordance with drawings called out for the specific models on Flap Up Installation Data Requirement Sheet" dated April 8, 1969, and MASA Drawing No. 9000 dated April 16, 1973.

Limitations and Conditions: This modification is approved for the following models:

Cessna 182E, 182F, 182G, 182H, 182K, 182L, 182M; 206, P206, U206, 210C, 210D, 210E, 210F, 210G (205) 210-5, (205A) 210-5A; 337, 337A, 337B, T337B, 337C, T337C, 337D, T337D. This modification is also eligible on the following Wren Model: 460H, 460J, 460K, 460L, and 460M.

Date of Application: Apr11 9, 1969 Dule rissued: 3/20/70; 5/11/72; 5/14/73;

3/1/74; 1/10/75; 2/28/75; 9/16/77 Date of Issuance: April 16, 1969 Date Amended: Revision 7 FEDERAL AVIATION ти .

(Signature) TMINISTRATO Don P. Watson Chief, Engineering and Manufacturing Branch (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee) - (Naber and street) (City, State, and ZIP code ) from (Name of grantor) (Print or type) (Address of grantox) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement) Date of Transfer:

Signature of grantor (In ink):.

* U.S. GOVERNMENT PRINTING OFFICE: 1977 - 772-889

## Every issue (1)

- September 16, 1977: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/52/b2/52b2cc18124ac0a92cf073a300680fada195004046f3eebd636dd92a46ef07d6)

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