# STC SR01601NY-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Teledyne Battery Products, United States
- Description: Installation of a Lead Acid Battery (Gill G-6381ES).
- Applied: July 14, 2003
- Status date: October 8, 2004
- 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/ba/c6/bac64478ee0657472bbb5a04d8b797108facbb8a35a5d75f06a018d29d745a51
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5CF359B273EE08F5862570EB00772A54.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR01601NY-D

## 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.

This Certificate issued to Teledyne Continental Motors 840 West Brockton Avenue P. O. Box 7950 Redlands, California 92375 Part 29 of the Federal Aviation Regulations.

H1NE

SIKORSKY S-76A & S76C Description of Type Design Change: Installation of Lead Acid battery (Gill G-6381ES) in accordance with Keystone Helicopter Installation Drawing List IDL00684, No Rev., dated December 23, 2003, or later FAA approved revision.

Limitations and Conditions

1. Keystone Helicopter Corp. FAA Approved Rotorcraft Flight Manual Supplement No. FM00684, No Rev., FAA approved January 7, 2004 or later FAA approved revision, is required with this notification.

2. This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft.

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 : July 14, 2003

Date of issuance : January 7, 2004

Date reissued February 25, 2004; July 15, 2004;

October 8, 2004

( Signature)

Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

## Every issue (1)

- October 8, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ba/c6/bac64478ee0657472bbb5a04d8b797108facbb8a35a5d75f06a018d29d745a51)

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