# STC SR01591LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Van Horn Aviation LLC, United States
- Description: Description of Type Design Change:    Installation of main rotor blades, P/N 206B2100-101, in accordance with Van Horn Aviation, L.L.C. Master Document List (MDL), 206B-MDL-001, Revision C, dated February 5, 2004, and Bonded Structures Ltd. Installation and Maintenance Manual, Manual No. VMM-301, Revision N/C, dated February 9, 2004, or later FAA Approved Revisions.
- Applied: July 20, 2001
- Status date: February 27, 2004
- Product: Aircraft, Rotorcraft
- Certification basis: Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/db/65/db65652f5ada32f8f0c0750cf1eee17bc3a39fb79efb43b1f2b6c5557a50c387
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B62D5C181C0A784E86256E75004EC831.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01591LA

## ADs that name it (0)

None.

## Approved models (2)

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

This Certificate issued to Van Horn Aviation, L.L.C.

1000 E. Vista Del Cerro Drive Tempe, Arizona 85281 Part 27* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet H2SW Original Product Type Certificate Number :

H2SW Bell Helicopter Textron 206A, 206B Description of Type Design Change: Installation of main rotor blades, P/N 206B2100-101, in accordance with Van Horn Aviation, L.L.C. Master Document List (MDL), 206B-MDL-001, Revision C, dated February 5, 2004, and Bonded Structures Ltd. Installation and Maintenance Manual, Manual No. VMM- 301, Revision N/C, dated February 9, 2004, or later FAA Approved Revisions.

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted helicopter models only. A copy of this STC must be included in the permanent records of 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 : July 20, 2001

Date of issuance : February 27, 2004

( Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office ( Title)

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- February 27, 2004: Issued, Current. [certificate](https://openairdocs.org/files/sha256/db/65/db65652f5ada32f8f0c0750cf1eee17bc3a39fb79efb43b1f2b6c5557a50c387)

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