# STC SH6039NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Heli-Support Inc, United States
- Description: Intermixing of main rotor blades of the same part number.
- Applied: July 30, 1992
- Status date: July 29, 2004
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H1IN](https://openairdocs.org/tcds/H1IN)
- Certificate PDF: https://openairdocs.org/files/sha256/ba/82/ba8207691762fec882b4e10e929648036807fbd4fe4f4a19b4f5fb2b75c191a4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E3A82F48FAED3423862574430071586A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH6039NM

## ADs that name it (0)

None.

## Approved models (5)

- Eurocopter France SA.315B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))
- Eurocopter France SA.316B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))
- Eurocopter France SA.316C Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))
- Eurocopter France SA.319B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))
- Eurocopter France SE.3160 Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SH6039NM This certificate issued to: Heli-Support, Inc.

4101 Evans Avenue Cheyenne, WY 82001 Part CAR 6* of the Civil Air Regulations. *(For Certification basis see Type Certificate Data Sheet HIIN) Original Product Type Cerlificate Number: HIIN Make: Aerospatiale Model: SE 3160, SA 316B, SA 315B, SA 319B, SA 316C Alouette IIII Description of Type Design Change: Intermixing of Main Rotor Blades of the same part number for Aerospatiale models listed above in accordance with FAA approved Heli-Support, Inc. Master Document List MDL-HSI-3160-50 Rev. N/C dated June 1, 1993, or later FAA approved revisions.

Limitations and Conditions: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this change and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the 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 30, 1992 Date Reissued: July July 2004 Date of Issuance: July 19, 1993 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Calk K. Woo (Signature) TOMINSTRATO Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- July 29, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ba/82/ba8207691762fec882b4e10e929648036807fbd4fe4f4a19b4f5fb2b75c191a4)

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