# STC SA1605SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Micro AeroDynamics Inc, United States
- Description: Removal of cowl flaps and associated components.
- Applied: August 25, 1983
- Status date: February 13, 1995
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A7CE](https://openairdocs.org/tcds/A7CE)
- Certificate PDF: https://openairdocs.org/files/sha256/12/6f/126fc7932575b61718875e7469b219452e643c8f0316dcd7e0f326fd6fd76b2b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EFC92C23D432B75985256CC100821446.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1605SO

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 411 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- February 13, 1995: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/12/6f/126fc7932575b61718875e7469b219452e643c8f0316dcd7e0f326fd6fd76b2b)

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