# STC SA01374SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Can-Am Aerospace LLC, United States
- Description: Installation of a remote flap selector lever; manufactured, installed, and maintained
- Applied: September 16, 2003
- Status date: December 31, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- Certificate PDF: https://openairdocs.org/files/sha256/f2/72/f272ecfaa43fbb7844c4efadd0610cc1aa0a289fcd2ae31bb6a26e8fadc9254d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/23C0C0156DCB9F1D862576BF005738FF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01374SE

## ADs that name it (0)

None.

## Approved models (3)

- Viking Air Limited DHC-2 Mk.I ([TCDS A-806](https://openairdocs.org/tcds/A-806))
- Viking Air Limited DHC-2 Mk.II ([TCDS A-806](https://openairdocs.org/tcds/A-806))
- Viking Air Limited DHC-2 Mk.III ([TCDS A-806](https://openairdocs.org/tcds/A-806))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SA01374SE

This certificate, issued to: Can-Am Aerospace, LLC 3101 111th Street SW, Unit B Everett, WA 98204

Part 29 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A-806 Make: De Havilland Model: DHC-2 Beaver

Description of the Type Design Change: Installation of a remote flap selector lever; manufactured, installed, and maintained in accordance with Master Data and Document List No. NW012-AOG-003, Revision NC, dated January 26, 2004, Installation Instructions Report No. AOG-14-002-1, Revision New, dated June 30, 2001, and Maintenance Manual Supplement, MMS-198-03-001, Revision NI, dated June 30, 2001, or later FAA-approved revisions.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft 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 the FAA-approved Airplane Flight Manual Supplement (AFMS), dated February 05, 2004, must be maintained as part of the permanent records for the modified aircraft.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application: September 16, 2003 Date reissued: December 31, 2009 Date of issuance: February 05, 2004 Date amended: June 04, 2004

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Original Signed by Ronald F. May

## Every issue (2)

- December 31, 2009: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f2/72/f272ecfaa43fbb7844c4efadd0610cc1aa0a289fcd2ae31bb6a26e8fadc9254d)
- June 4, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d1/03/d10331ff8f872b6013730b5611576eb42bd2d87c5a84cc63c83460c8363cb7ee)

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