# STC SA1493CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aircraft Development Co, United States
- Description: Installation of flap and aileron gap seals.
- Applied: April 20, 1979
- Status date: February 24, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- Certificate PDF: https://openairdocs.org/files/sha256/1c/4d/1c4de7d418b135cea99d0336349c966d6c7619fde3639072c7402ac3a199871f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CD4D41626764766A86256FE200709DCB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1493CE

## ADs that name it (0)

None.

## Approved models (11)

- The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))

## 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.

1220 Red Oak Ct.

Troy, MO 63367

Part 3 of the Civil Air Regulations.

Original Product--Type Certificate Number : 5A6 Make :

Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K

Description of Type Design Change: Installation of flap and aileron gap seals per Aircraft Development Co. Drawing Lists 114-1 and 115-1 stamped "FAA Approved" with a date of April 18, 1979, or later.

Compatibility of this design change with previously approved modifications must be determined by the installer.

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 : April 20, 1979

Date of issuance : May 21, 1979 Date reissued : January 27, 1993; January 30, 1996

Date amended : February 24, 2005

Original signed by: Dan Withers

( Signature) Dan Withers Program Manager Wichita Aircraft Certification Office

(Title)

## Every issue (1)

- February 24, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/1c/4d/1c4de7d418b135cea99d0336349c966d6c7619fde3639072c7402ac3a199871f)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
