# STC SR02587LA

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of HeliSAS /Autopilot System
- Applied: June 18, 2012
- Status date: April 19, 2016
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU)
- Certificate PDF: https://openairdocs.org/files/sha256/31/e1/31e1963a0eecec7155d0b5d80b256b7fbf159ebc54531dbb34c9f2b0a070a7ef
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F05472915BABB3A586257F9C00698A1C.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR02587LA

## ADs that name it (0)

None.

## Approved models (6)

- Airbus Helicopters Deutschland GmbH EC135 P1 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135 P2 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135 P2+ ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135 T1 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135 T2 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135 T2+ ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))

## 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.

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SR02587LA

This Certificate issued to

Part 27* of the Federal Aviation Regulations.

*14 Code of CFR requirements of Part 27 and Special Condition No. 27-031-SC

Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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.

S-TEC Corporation One S-TEC Way Mineral Wells, TX 76067 H88EU

Airbus Helicopters Deutschland GmbH

EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, EC135T2+ Original Product Type Certificate Number :

(Signature) Manager, Systems and Equipment Branch Los Angeles Aircraft Certification Office

(Title)

Date of application: June 18, 2012

Date of issuance: April 19, 2016

Number SR02587LA

Description of Type Design Change

1. Installation of HeliSAS®/Autopilot System on Airbus Helicopters Deutschland GmbH Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, and EC135T2+ Helicopters in accordance with FAA Approved Master Data List, ST-948-MDL-0001, Revision “D” dated June 22, 2015, or later FAA Approved Revisions.

2. FAA Approved Rotorcraft Flight Manual Supplement ST-948-RFMS-0001, Revision “ - ”, dated April 18, 2016 is required for Airbus Helicopters Deutschland GmbH Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, and EC135T2+ Helicopters, or later FAA approved revisions of this document.

3. Instructions for Continued Airworthiness ST -948-ICA-0001, Revision “A ”, dated June 16, 2015 is required for Airbus Helicopters Deutschland GmbH Model EC135P1, EC135T1, EC135P2, EC135T2, EC135P2+, and EC135T2+ Helicopters, or later FAA approved revisi ons of this document.

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## Every issue (1)

- April 19, 2016: Issued, Current. [certificate](https://openairdocs.org/files/sha256/31/e1/31e1963a0eecec7155d0b5d80b256b7fbf159ebc54531dbb34c9f2b0a070a7ef)

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