# STC SA3347NM

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: C & C Aviation, United States
- Description: Use of the Union Aviation portable hand operated rudder and brake model C.
- Applied: March 6, 1986
- Status date: September 30, 1987
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/b5/0a/b50abd7cc1ef4ac5c722d4ad793b807a9065c10b3690f2c7596b0fbf71022686
- Approved model list and other attachments: [AML SA3347NM.pdf](https://openairdocs.org/files/sha256/06/2e/062e2691f1ed6596eed7296a008ca619035b8d4aae5875e4dc16b0af1ed72b31)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0DDB3AC7342BA9B485256CC2000A9720.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3347NM

## ADs that name it (0)

None.

## Approved models (45)

- Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 210F ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210G ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210H ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210J ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210K ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company 210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- 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 P206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T210L ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210M ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company T210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))
- Cessna Aircraft Company TP206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TP206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TP206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TP206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company TP206E ([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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA33478N1M This certificate issued to: C & C AViAtion Certifies that the change in the type design for the following product with the limitations and conditions therefor aspecified hereonneels the airworthiness sequirements of Purt * of the * Pregulations Original Product - Type bertificate Numben: Make: * * *See attached Master Eligibility List (MEL) No. SA3347NM for list of approved airplane models and applicable airworthiness Model: * regulations.

DesriplinType Design hange. spot ted Unen stated table ance with Union er nd brake control, Model Aviation Installation Instructions, dated October 15, 1975. Aircraft may be operated with or without the Model "C" Control installed.

NOTE: This approval requires that Cessna rudder pedal, part No. 1460320-1, be installed in the aircraft.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft 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 upor the airworthiness of that aircraft. A copy of this Certificate, Master Eligibility List, and FAA Flight Manual Supplement dated April 7, 1986, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft

Date of Application: March 6, 1986 Date Reissued:

Date of Issuance: Apri1 7, 1986 Date Amended: November 21, 1986, September 30, 1987 FEDERAL NUTATION Pary direction of the Sldministrater кля Signatures pen TAMINIST RANDO Assistant Manager, Seattle -Aireraft Certifigation Office

47.

### AML SA3347NM.pdf

This is OCR from the scanned FAA attachment. OCR can misread letters and numbers.

Issue Date: November 20, 1986 MEL AMENDMENT DATE 9/30/87 ORIGINAL TYPE CERTIFICATE NUMBER 3A21 A16CE A4 CE FAA Approvedig Manager, Seattle Aircraft Certification Office C & C AVIATION FAA APPROVED MASTER ELIGIBILITY LIST NO. SA3347NM INSTALLATION OF UNION AVIATION HAND CONTROL, MODEL C CERTIFICATION BASIS FOR ALTERATION 5/15/56 2/1/65 5/15/56 Date: September 30, 1987 Page 1 of 1 FOR CAR Part 3, FAR Part 23, CAR Part 3, AIRCRAFT MODEL |P210, 210F thru 210N, T210L thru T210N 1207, I207, 207A, & I207A 206 Series AIRCRAFT MAKE Cessna Cessna Cessna ITEM

## Every issue (1)

- September 30, 1987: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b5/0a/b50abd7cc1ef4ac5c722d4ad793b807a9065c10b3690f2c7596b0fbf71022686), [AML SA3347NM.pdf](https://openairdocs.org/files/sha256/06/2e/062e2691f1ed6596eed7296a008ca619035b8d4aae5875e4dc16b0af1ed72b31)

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