STC SR00842DE

Supplemental type certificate · Teledyne Battery Products

Holder
Teledyne Battery Products · United States
Status
Current · Issued
Status date
March 7, 2017
Applied
November 29, 2016
Product
Aircraft · Rotorcraft
Certification basis
Part 21
Data sheet
TCDSH88EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of Teledyne Battery Products Gill LT Valve-Regulated Lead-Acid

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00842DE This certificate, issued to: Teledyne Battery Products 840 West Brockton Avenue Redlands, CA 92374 Part 27 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: H88EU Make: Airbus Helicopters Deutschland GmbH Model: EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+ Description of the Type Design Change:

Installation of Teledyne Battery Products Gill LT Valve-Regulated Lead-Acid (LT-VRLA), P/N 7638-44, battery in accordance with Teledyne Battery Products Document No. TD70-8-03, Master Drawing List, Installation of Teledyne Battery Products P/N 7638-44, Revision IR dated 3/4/2017, FAA approved 3/7/2017 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. TD 70-8-02, Revision NC dated 3/3/2017, FAA Accepted 3/7/2017, or later FAA accepted revision are required to be made available at installation. FAA Approved Rotorcraft Flight Manual Supplement, Document No. TD 70-8-01, Revision IR dated 12/1/2016, FAA Approved 3/6/2017, or later FAA approved revision is required for this modification.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(Certification Basis on page 3 of 3) This certificate and the supporting data which is the bases for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of Application: November 29, 2016 Date Reissued:

Date of Issuance: March 7, 2017 Date Amended:

By direction of the Administrator Signature Kreg R. Voorhies Title ODA Administrator, Cert Works ODA(AIR)-833887-NM

FAA Form 8110-2 (5/14) Page 1 of 3

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR00842DE To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

FAA Form 8110-2 (5/14) Page 2 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00842DE Date of Issuance: March 7, 2017 Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Airbus Helicopters EC135 Series Teledyne Battery Products 7638-44 battery installations is as follows:

a. The type certification basis for Airbus Helicopters Deutschland GmbH EC135 Series helicopter is shown on TCDS H88EU for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, November 29, 2016, is based upon 14 CFR Part 27, effective February 1, 1965 plus Amendments 27-1 through 27-31, as defined per the TCDS. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the TCDS Certification Basis (Part 27, Amendments 27-1 through 27-31):

14 CFR Part 27 Sections: 27.301 Amdt. - ; 27.303 Amdt. - ; 27.305(a) Amdt. - ; 27.307(a) Amdt. 27- 26; 27.337(a) Amdt. 27-26; 27.341 Amdt. - ; 27.601(a) Amdt. - ; 27.603 Amdt. 27-16; 27.605(a) Amdt. 27-16; 27.607(a) Amdt. 27-4; 27.609(a) Amdt. - ; 27.611 Amdt. - ; 27.613 Amdt. 27-26;

27.619(b)(1) Amdt. - ; 27.625(a) Amdt. - ; 27.1301 Amdt. - ; 27.1309(a),(b),(d) Amdt. 27-21;

27.1351(a),(b)(1)(i)(ii) Amdt. 27-13; 27.1353(a-e) Amdt. 27-14; 27.1529 Amdt. 27-18; 27.1581 Amdt.

27-14; 27.1585(a) Amdt. 27-21

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

FAA Form 8110-2 (5/14) Page 3 of 3

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 6

MakeModelData sheet
Airbus Helicopters Deutschland GmbHEC135 P1H88EU
Airbus Helicopters Deutschland GmbHEC135 P2H88EU
Airbus Helicopters Deutschland GmbHEC135 P2+H88EU
Airbus Helicopters Deutschland GmbHEC135 T1H88EU
Airbus Helicopters Deutschland GmbHEC135 T2H88EU
Airbus Helicopters Deutschland GmbHEC135 T2+H88EU