# STC SR01692LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Van Horn Aviation LLC, United States
- Description: Installation of an Internal Load Attaching Means.
- Applied: August 2, 2004
- Status date: November 15, 2004
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H9EU](https://openairdocs.org/tcds/H9EU)
- Certificate PDF: https://openairdocs.org/files/sha256/5c/f0/5cf0790fdc4b3e8127637b5cbf17759858406430b5f42d155ffacb4259daf63e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DEAFB52CF8BC37FD862570CA00742CF0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01692LA

## ADs that name it (0)

None.

## Approved models (8)

- Eurocopter France AS-350B ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B2 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350B3 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350BA ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350C ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))
- Eurocopter France AS-350D1 ([TCDS H9EU](https://openairdocs.org/tcds/H9EU))

## 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 Dr.

Tempe, Arizona 85281 Part 27* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet H9EU Original Product Type Certificate Number :

H9EU Eurocopter France AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350C, AS350D, AS350D1 Description of Type Design Change: Installation of an Internal Load Attaching Means in accordance with FAA approved Van Horn Aviation LLC Master Document List No. MDL-123-000, Revision “N/C”, dated November 3, 2004, and FAA approved Van Horn Aviation LLC Rotorcraft Flight Manual Supplement No.

123-121 revision “N/C” dated November 12, 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 airplane model series only. The equipment for which these provisions are intended has not been certified. Additional FAA approval is required for the installation of this equipment and must be evaluated to assure satisfactory compliance with the applicable airworthiness standards. 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 : August 2, 2004

Date of issuance : November 15, 2004

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

## Every issue (1)

- November 15, 2004: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5c/f0/5cf0790fdc4b3e8127637b5cbf17759858406430b5f42d155ffacb4259daf63e)

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