# STC SA02269AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Tailwind Aviation Inc, United States
- Description: Installation of a 6.00-6 type III wheel and 6.00/7.00-6, 6-ply type III tire using a Cessna 310 nose fork and operated as a tail wheel on DHC-2 Series airplanes.
- Applied: November 2, 2004
- Status date: May 4, 2006
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-806](https://openairdocs.org/tcds/A-806)
- Certificate PDF: https://openairdocs.org/files/sha256/7e/ea/7eea2536cff2619ec7fa33da7cd8d308972f56e7ad7e40237eed340b8eeaee5e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F99EA80BB4117FF86257169004EE6A8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02269AK

## 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.

491 Westcove Drive Wasilla, AK 99654

Part 10 of the Civil Air Regulations.

Original Product Type Certificate Number : A-806 Make : Viking Air Limited (Formerly deHavilland, Inc.)

Model : DHC-2 Mk. I, Mk. II, and Mk. III

Description of Type Design Change: Installation of a 6.00-6 type III wheel and 6.00/7.00-6, 6-ply type III tire using a Cessna 310 nose fork and operated as a tail wheel on DHC-2 Series airplanes, in accordance with Tailwind Aviation, Inc., Master Data List MDL-001, Original Issue dated May 4, 2006, or later FAA approved revision.

1. Compatibility of this design change with other previously approved modifications must be determined by the installer. This design change has been shown to be compatible with Alaskan Bushwheel, Inc., STC SA01015SE.

2. A copy of this Certificate must be maintained as part of the permanent record of the modified aircraft.

3. 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.

4. This design change may be incorporated on surplus military Models L-20A, YL-20, and U-6A when the airplane has been converted to Model DHC-2 Mk. I in accordance with the requirements listed in Aircraft Specification No. A-806, Note 4.

Date of application : November 02, 2004

Date of issuance : May 4, 2006 Date reissued :

( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office

(Title)

## Every issue (1)

- May 4, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/7e/ea/7eea2536cff2619ec7fa33da7cd8d308972f56e7ad7e40237eed340b8eeaee5e)

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