# STC SA3651NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: EDO Corporation, United States
- Description: Installation of Edo 696-3500 amphibious floats. (TU206G AMPHIBIAN)
- Applied: February 21, 1984
- Status date: February 26, 1992
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/51/9c/519c476b2a43ce8b73a130ab57459d7290fb8950af3de8558f01b2d980eccc49
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A119B51D54A88F8285256CC2000C594A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3651NM

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206 ([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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA3651NM This certificate issued to: Edo Corporation/Kenmore Air Harbor/Soloy Corporation Purt 3 of the CiViL Air Regulations.

Original Product -Type Certificate Number: A4CE Make: Cessna Model: U206 & TU206G Amphibian Description of Type Design Change: Installation of Edo 696-3500 amphibious floats in accordance with Edo Installation Report No. EEC-R-474 and Kenmore Air Harbor Report No. K14439 dated September 3, 1986, or later FAA approved revisions.

Limilatinsand bendilions: Approval of this change in type design applies to the above model aircraft as modified per STC SA2353NM only. This approval should not be extended to aircraft of this model 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 the aircraft.

(Please see Continuation Sheet.)

Dalesapplicatinebruary 21, 1984 Jute wissued:

Date of Issuance: October 10, 1986 Vale unvended: February 26, 1992 FEDERA AVIATION By Direction of the Administrator Senan/alle ( Signature ) CHINIST RAY ON Stewart R. Miller, Assistant Manager Seattle Aircraft Certification Office, ANM-101S (Title )

47.

FEB 2 6 1992 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA3651NM Limitations and Conditions: (Continued) This approval is intended for installation in the above models incorporating the Turbine Pac (Allison 250-C20S) engine STC SE2352NM in accordance with Soloy Corporation STC SA2353NM. A copy of this Certificate, Pilot's Operating Handbook Supplement, dated October 15, 1986, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

NOTE: This approval is extended to those models above modified per Soloy Corporation SIC No. SA2353NM and also modified per the Sierra Industries Inc. STC No.

-END-

**FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES**

## Every issue (1)

- February 26, 1992: Amended, Current. [certificate](https://openairdocs.org/files/sha256/51/9c/519c476b2a43ce8b73a130ab57459d7290fb8950af3de8558f01b2d980eccc49)

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