# STC SR02068SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Firehawk Helicopters Inc., United States
- Description: Installation of a modified Sikorsky L/H Step Fairing P/N 70215-02319-043 manufactured and installed.
- Applied: July 30, 2009
- Status date: May 26, 2010
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H3NE](https://openairdocs.org/tcds/H3NE), [TCDS H5NE](https://openairdocs.org/tcds/H5NE)
- Certificate PDF: https://openairdocs.org/files/sha256/6b/4a/6b4ab050d2c9ffdd3a319f3aa180209dae6312843e884354e35af45614ac3911
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DE28388C07CC6AAF8625773D0064A50E.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR02068SE

## ADs that name it (0)

None.

## Approved models (2)

- Sikorsky Aircraft Corporation S-70A ([TCDS H5NE](https://openairdocs.org/tcds/H5NE))
- Sikorsky Aircraft Corporation S-70C ([TCDS H3NE](https://openairdocs.org/tcds/H3NE))

## 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 SR02068SE

This certificate, issued to: Firehawk Helicopters, Inc.

4125 West Wright Street Boise, ID 83705-6533

Part 29 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H5NE H3NE Make: Sikirsky Aircraft Sikorsky Aircraft Model: S-70A S-70C

Description of the Type Design Change: Installation of a modified Sikorsky L/H Step Fairing P/N 70215-02319-043 manufactured and installed in accordance with Firehawk Helicopters, Inc. Master Document List 777-000-100-MDL, Revision B, dated May 10, 2010, or later FAA-approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only.

This approval should not be extended to other rotorcraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. The rotorcraft must be maintained in accordance with the Instructions for Continued Airworthiness (ICA), document number 777-100-ICAW, Revision C, dated December 29, 2009, or later FAA-accepted revision.

A copy of this certificate and the ICA must be maintained as part of the permanent records for the modified rotorcraft.

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, 2009 Date reissued: Xxxxxxx ##, #### Date of issuance: May 26, 2010 Date amended: Xxxxxxx ##, ####

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title) Original Signed by Ronald F. May

## Every issue (1)

- May 26, 2010: Issued, Current. [certificate](https://openairdocs.org/files/sha256/6b/4a/6b4ab050d2c9ffdd3a319f3aa180209dae6312843e884354e35af45614ac3911)

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