# STC SA403SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Peterson Jeffrey Todd, United States
- Description: Full span double slotted flaps, drooped wing leading edge, aileron actuated drag plates, Robertson U.L.S. nose control system, increased elevator aerodynamic balance, and relocated pilot head.
- Applied: March 12, 1963
- Status date: December 20, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/cb/11/cb11e1c156a0da5d4689181fc2c6a72756366d8f2bf9dccf5f7ff8b79258e811
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E8ACF62A8637FD8985256CC2000C605A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA403SW

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- The Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## What the certificate says

The certificate has no text we could read; open the PDF to read it.

## Every issue (1)

- December 20, 1984: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/cb/11/cb11e1c156a0da5d4689181fc2c6a72756366d8f2bf9dccf5f7ff8b79258e811)

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