# STC SR01022SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Eagle Helicopters Inc, United States
- Description: Fabrication of Eagle Helicopter's Tail Rotor Guard Clamp
- Applied: November 7, 2000
- Status date: November 30, 2001
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H1IN](https://openairdocs.org/tcds/H1IN)
- Certificate PDF: https://openairdocs.org/files/sha256/0d/ce/0dce97cb5c1b0a20552490ab01df6d1934cd52decb6e7a69cc9b610cc75d73c6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33D4C20C2D668D6185256CC20062269F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR01022SE

## ADs that name it (0)

None.

## Approved models (1)

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

## 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.

Number SR01022SE

This certificate, issued to Eagle Hlicopters, Inc.

5311 East Rutter Ave.

Spokane, WA 99212 Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H1IN (SA315B) & 7H1 (SA318C) Make: Eurocopter France Model: SA315B & SA318C

Description of the Type Design Change: Fabrication of Eagle Helicopter’s Tail Rotor Guard Clamp in accordance with Eagle Helicopter’s Master Drawing List No. EH 3130, Revision N/C, dated September 12, 2001, or later FAA approved revision; and installation of this clamp in accordance with Installation Instructions, Report No. EH-3130, Revision A, dated June 4, 2001, or later FAA approved revision. This modification must be maintained in accordance with Instructions for Continued Airworthiness, Report No. EH-3130, Revision A, dated June 4, 2001, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to Eurocopter rotorcraft models listed above only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of the helicopter. A copy of this Certificate and Instruction for Continued Airworthiness must be maintained as part of the permanent record of the modified helicopter.

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: November 7, 2000 Date reissued:

Date of issuance: November 30, 2001 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- November 30, 2001: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0d/ce/0dce97cb5c1b0a20552490ab01df6d1934cd52decb6e7a69cc9b610cc75d73c6)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.