# STC SA00018SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aerocet Inc, United States
- Description: Fabrication of interchangeable float attachment gear parts.
- Applied: July 15, 1993
- Status date: October 20, 1993
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/db/37/db377b175820c968dd5226ffdbcb4ea0728b0c40c6780ab51b8104a898c8532d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2AC65F9154740D9485256CC1007DC711.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00018SE

## ADs that name it (0)

None.

## Approved models (19)

- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TP206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206G ([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.

Sie Beek United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA00018SE This certificate issued to: Aerocet, Inc.

Port 3 of the CIVIl Air Regulations: * Original Product Type ortifical Number: A4CE Make:

Model: Cessna Putachin Fear Parts hagordance wric FAn Approved he icet Master Drawing list No. Fabrication of Aerocet interchangeable Lication , Aeroet interchangeable float A 35-10011, dated July 15, 1993, or later FAA Approved revision. The installation considerations noted on page 3 of this SIC should be observed during the interchange process.

Limitations and Conditions: Approval of this change in type design applies to only those Cessna Model airplanes which were previously equipped with either factory installed Edo Model 582-3430 floats, or Edo Model 696-3500 floats installed in accordance with STC No. SA439NW. Refer to Aerocet Parts Application List No. A-10008 dated July 15, 1993, or later FAA Approved revision, for a listing of which float gear parts may be interchanged on each airplane/float combination, except that (see Continuation Sheet, page 3) 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number 5A000185E Limitations and Conditions: (continued) the Edo 696-3500 floats are not approved for installation on Cessna Model U206G airplanes (S/N's U20606921 and up), or any Cessna Model TU206G airplanes under STC No.

SA439NW. This approval should not be extended to airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and Continuation Sheet No. SA00018SE must be maintained as part of the permanent records for the modified aircraft.

- Many changes are known to have been made to some airplane float installations over the years. Thus, the installer should verify that the replaced parts are approximately identical to the Aerocet interchangeable parts. A dimensional comparison of float fittings and struts would be a good check.

- Install all interchangeable float attachment gear parts using existing float hardware following standard marine corrosion prevention measures. Replace all damaged and worn parts.

- Assess all existing float damage and corrosion for continuing airworthiness.

- Re-install water rudder rigging in an FAA Approved manner.

Re-install passenger step assemblies in an FAA Approved manner.

= END - 17

**PAGE OF PAGES FAA AC 82 03579**

## Every issue (1)

- October 20, 1993: Issued, Current. [certificate](https://openairdocs.org/files/sha256/db/37/db377b175820c968dd5226ffdbcb4ea0728b0c40c6780ab51b8104a898c8532d)

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