STC SR01042SE

Supplemental type certificate · Dart Aerospace USA, Inc.

Holder
Dart Aerospace USA, Inc. · United States
Status
Current · Reissued
Status date
October 17, 2018
Applied
October 23, 2001
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 27
Data sheet
TCDSH88EU

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

What it approves

Fabrication of Dart D135-692-011 Bearpaws

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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SR01042SE

This certificate, issued to Dart Aerospace USA, Inc.

3845 NE 30th Avenue Hillsboro, OR 97124

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+, EC135P3, EC135T3

Description of the Type Design Change: Fabrication of Dart D135-692-011 Bearpaws in accordance with Dart Aerospace USA, Inc. Master Document List No. MDL-D135-692, Revision H, dated June 8, 2017, or later Federal Aviation Administration (FAA) approved revision; and installation of this system in accordance with Installation Instructions Document No. IIN-D135-692, Revision B, dated July 20, 2015, or later FAA-approved revision. This modification must be maintained in accordance with Instructions for Continued Airworthiness, Document No, ICA-D135-692, Revision 1, dated July 20, 2015, or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only, which are equipped with the standard skidtubes, high gear skidtubes, or float skidtubes as defined i n the Installation Instructions. 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 will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate, the Installation Instructions, and the Instructions for Continued Airworthiness must be maintained as part of the permanent record of 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: October 23, 2001 Date reissued: October 28, 2015; October 17, 2018 Date of issuance: January 25, 2002 Date amended: June 27, 2017

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

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 · 8

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
Airbus Helicopters Deutschland GmbHEC135P3H88EU
Airbus Helicopters Deutschland GmbHEC135T3H88EU

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
October 17, 2018Reissued, currentCertificate
June 27, 2017Amended, earlier issueCertificate
October 28, 2015Reissued, earlier issueCertificate
January 25, 2002Issued, earlier issueCertificate