# STC SA00147SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aeronautical Testing Service Inc., United States
- Description: Installation of vortex generators mounted on the wings and (optional) 'split flaps' mounted on lower trailing edge of the inboard 'stub' wing.
- Applied: September 22, 1994
- Status date: May 29, 1996
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A9CE](https://openairdocs.org/tcds/A9CE)
- Certificate PDF: https://openairdocs.org/files/sha256/ec/ce/ecce2f760cc64514b452e1cc4197c475a80946043615e0203612ecff98a45972
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/98455888F780A18E85256CC1007DC7D9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00147SE

## ADs that name it (0)

None.

## Approved models (3)

- Cessna Aircraft Company 188B ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company A188B ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))
- Cessna Aircraft Company T188C ([TCDS A9CE](https://openairdocs.org/tcds/A9CE))

## What the certificate says

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

## Every issue (1)

- May 29, 1996: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ec/ce/ecce2f760cc64514b452e1cc4197c475a80946043615e0203612ecff98a45972)

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