# STC SH2709NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Comm Corporation, United States
- Description: Installation of an engine driven accessory hydraulic pump and associated hardware.
- Applied: January 4, 1984
- Status date: November 24, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/fd/3f/fd3f45cc981ed4c825cc361bb629c9cbbc3dab7c5c649eabe1d6424ab84074a9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/42A8FA861B0F7EF286257DF7006B9098.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH2709NM

## ADs that name it (0)

None.

## Approved models (2)

- Bell Helicopter Textron Canada Limited 206A ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))
- Bell Helicopter Textron Canada Limited 206B ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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 SH2709NM

Date of application: January 4, 1984 Date reissued: June 16, 1987; November 24, 2014 Date of issuance: May 12, 1986 Date amended: June 23, 1986

Todd Dixon (Signature) Manager, Denver Aircraft Certification Office Denver Aircraft Certification Office (Title)

This certificate, issued to Air Comm Corporation 1575 West 124th Ave Westminster, CO 80234

Part 6 of the Civil Air Regulations.

Original ProductType Certificate Number: H2SW Make: Bell Helicopter Textron Model: 206A, 206B Description of the Type Design Change:

Installation of Engine Driven Accessory Hydraulic Pump and associated hardware in accordance with Air Comm Corporation Drawing List No. DL-206HP, Revision D, dated May 1, 1985, or later FAA approved revision.

1. FAA Approved Flight Manual Supplement, dated May 3, 1985, or later FAA approved revision is required.

2. Approval of this change in type design applies to the model of aircraft listed above only.

3. Compatibility of this design change with previously approved alterations must be determined by the installer.

4. 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.

5. A copy of this certificate and the appropriate flight manual supplement as listed above must be maintained as part of the permanent record for the altered aircraft.

## Every issue (3)

- November 24, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fd/3f/fd3f45cc981ed4c825cc361bb629c9cbbc3dab7c5c649eabe1d6424ab84074a9)
- August 15, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ba/a3/baa30ceefbf6ad0a2d826ce10aa9cf99fb5e984f6c44d179bb6bca0f8a6daa36)
- June 16, 1987: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e9/8a/e98a728e23b56e10e7f22824f4f7b382d1d96ac58174375d4f17b7ae4f5ba6aa)

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