# STC SR01270SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Columbia Helicopters Inc, United States
- Description: Installation of Load Beam, Hook for Attaching External Load, and Load Cell (Sensor) Indication System.
- Applied: February 5, 2003
- Status date: October 5, 2005
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS 1H16](https://openairdocs.org/tcds/1H16), [TCDS H1PC](https://openairdocs.org/tcds/H1PC)
- Certificate PDF: https://openairdocs.org/files/sha256/78/57/785762b1d3ff81b4af81fc31f38c0278c3f0cd3d8c49572d44956a988a6163ca
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2399AE9021D50D80862570A7004BDD9E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01270SE

## ADs that name it (0)

None.

## Approved models (2)

- 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))

## 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.

United States of America Department of Transportation _ Federal Aviation Administration Supplemental Type Certificate Number SR01270SE This certificate, issued to Columbia Helicopters, Inc.

P.O. Box 3500 Portland, OR 97208 Part 7 and 10 of the Civil Air Regulations.

Original Product⎯Type Certificate Number: H1PC 1H 16 Make: Kawasaki Boeing Model: KV107-II Vertol 107-II Series

Description of the Type Design Change: Installation of Load Beam, Hook for Attaching External Load, and Load Cell (Sensor) Indication System per Columbia Helicopters, Inc. Master Drawing List Document No. 03-RDE-0511, Revision D, dated September 28, 2005 or later Federal Aviation Administration (FAA) approved revision. The modification must be maintained in accordance with Columbia Helicopters, Inc. Maintenance Manual Supplement Document No. C07- 2/25-51-00, Revision 3, dated February 9, 2005 or later FAA accepted revision.

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.

Rotorcraft modified in accordance with this STC must be operated in accordance with a FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS) Columbia Helicopters, Inc. Document No. 05-RDE-0505, Revision IR, dated September 27, 2005 or later FAA approved revision. The FAA approved RFMS is a required part of this STC and must be maintained with a copy of this certificate as part of the permanent records of the modified helicopter. The Maintenance Manual Supplement 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: February 5, 2003 Date reissued:

Date of issuance: January 22, 2004 Date amended: October 5, 2005

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- October 5, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/78/57/785762b1d3ff81b4af81fc31f38c0278c3f0cd3d8c49572d44956a988a6163ca)

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