# STC SR01472NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Eaton Aerospace, United States
- Description: Installation of Eaton Aerospace/Tedeco Products Zapper pulsed electric chip detector system 1K7707 with Turbomeca Arriel 1S, 1S1, and 2S1 Engines.
- Applied: December 14, 2001
- Status date: May 11, 2006
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H1NE](https://openairdocs.org/tcds/H1NE)
- Certificate PDF: https://openairdocs.org/files/sha256/cf/25/cf25c2f8ec32362acbce2facfc9687cf527246832be5c0fce028627e4a0e5654
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A80B25E2525CCBF88625719500574EE8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01472NY

## ADs that name it (0)

None.

## Approved models (2)

- Sikorsky Aircraft Corporation S-76A ([TCDS H1NE](https://openairdocs.org/tcds/H1NE))
- Sikorsky Aircraft Corporation S-76C ([TCDS H1NE](https://openairdocs.org/tcds/H1NE))

## 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 SR01472NY This certificate issued to Eaton Aerospace 24 East Glenolden Avenue Glenolden, PA 19036-2198

Part 29 of the Federal Aviation Regulations.

Original Product -- Type Certificate Number : H1NE Make : Sikorsky

S-76A, S76C

Installation of Eaton Aerospace/Tedeco Products Zapper pulsed electric chip detector system 1K7707 on Sikorsky Helicopter S-76A and C Models with Turbomeca Arriel 1S, 1S1, 2S1 and 2S2 Engines in accordance with Installation Drawing List IDL 00508, Rev.

B, dated May 11, 2006.

1. For the Sikorsky S-76 helicopters fitted with Arriel 1S and 1S1 engines – the Arriel 1S and 1S1 engines must be equipped with TU 208 and TU 232 prior to the installation of the 1K7707 Zapper System.

2. Eaton Aerospace. Rotorcraft Flight Manual Supplement, Document # FM 00508, Revision 1, FAA approved May 11, 2006 is required with this modification.

3. 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.

4. Compatibility of this design change with previously approved modifications must be determined by the installer.

Date of application : December 14, 2001

Date of issuance : March 8, 2002 Date reissued : March 20, 2002

Date amended : May 11, 2006

( Signature) Anthony Socias Manager New York Aircraft Certification Office

(Title)

## Every issue (1)

- May 11, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/cf/25/cf25c2f8ec32362acbce2facfc9687cf527246832be5c0fce028627e4a0e5654)

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