# STC SR01639SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Columbia Helicopters Inc, United States
- Description: Installation of a 190 gallon fuel system conversion.
- Applied: November 3, 2005
- Status date: February 2, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1PC](https://openairdocs.org/tcds/H1PC), [TCDS 1H16](https://openairdocs.org/tcds/1H16)
- Certificate PDF: https://openairdocs.org/files/sha256/c0/12/c01253901a3cbd58fd19a516595419a9f5d932377cb1776ec1bf34e75f9fa919
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7372608E6FA76B598625710F00560838.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01639SE

## ADs that name it (0)

None.

## Approved models (3)

- Boeing Defense & Space Group 107-II ([TCDS 1H16](https://openairdocs.org/tcds/1H16))
- Kawasaki Heavy Industries Limited KV107-II ([TCDS H1PC](https://openairdocs.org/tcds/H1PC))
- Kawasaki Heavy Industries Limited KV107-IIA ([TCDS H1PC](https://openairdocs.org/tcds/H1PC))

## 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 SR01639SE This certificate, issued to Columbia Helicopters, Inc.

P.O. Box 3500 Portland, OR 97208-3500 Parts 7&10 of the Civil Aviation Regulations.

Original Product⎯Type Certificate Number: H1PC (CAR 7&10) 1H16 (CAR 7) Make: Kawasaki Boeing Vertol Model: KV107-II, IIA 107-II

Description of the Type Design Change: Installation of a 190 gallon fuel system conversion on the above model rotorcraft in accordance with Columbia Helicopters Inc. Master Drawing List 04-RDE- 1206 Rev. A, dated January 26, 2006.

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 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. This certificate must be maintained as part of the helicopter. The Rotorcraft AEG Accepted Maintenance Manual Supplement C07-2/28-00-01, Rev. 1, dated October 27, 2005 must be maintained as part of the helicopter instructions for continued airworthiness.

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: November 3, 2005 Date reissued:

Date of issuance: February 2, 2006 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- February 2, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c0/12/c01253901a3cbd58fd19a516595419a9f5d932377cb1776ec1bf34e75f9fa919)

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