# STC SR03277NY

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: ISEI, Le Mercure B, France
- Description: Installation of a HELICOM V2 NUM System for tracking a set of flight and system parameters during operation of the rotorcraft
- Applied: October 10, 2012
- Status date: March 30, 2017
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU)
- Certificate PDF: https://openairdocs.org/files/sha256/c9/0a/c90a10b4b8c2cf07b83e19efde6e11c7d025c6f6784b37ef1f6961e4f117c9e9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/41CB2F1DD48B3A1B862581100050E136.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR03277NY

## ADs that name it (0)

None.

## Approved models (8)

- 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))
- Airbus Helicopters Deutschland GmbH EC135P3 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))
- Airbus Helicopters Deutschland GmbH EC135T3 ([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.

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

Part of the

Signature

Title SR03277NY ISEI 1030 Avenue JR Guillibert Gauthier De La Lauziere 13290 Aix-En-Provence, France Federal Aviation Regulations.

1. Installation of Flight Data Monitoring System in accordance with ISEI Installation Manual N7-EC135 V2-HV2 NUM E-B-03 dated November 18, 2015 or later EASA approved revisions.

2. Aircraft will be operated in accordance with ISEI Rotocraft Flight Manual Supplement N11-EC135 V2-HV2 NUM-E-A-02 Rev 2, dated November 18, 2105 or later EASA approved revisions.

3. Maintenance in accordance with Instruction for Continued Airworthiness N8-EC135 V2-HV2 NUM-E-B-02 Rev 3, dated November 18, 2105 or later EASA approved revisions.

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 the certificate to alter the product, the holder shall give the other person written evidence of that permission.

Gaetano Sciortino Manager New York Aircraft Certification Office Airbus Helicopters Deutschland EC135 P2+, EC135 T1, EC135 T2, EC135 T2+, EC135 P1, EC135 P2, EC135 T3, EC135 P3 March 30, 2017 October 10, 2012 May 8, 2013 IMPORT H88EU 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SR03277NY

## Every issue (2)

- March 30, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c9/0a/c90a10b4b8c2cf07b83e19efde6e11c7d025c6f6784b37ef1f6961e4f117c9e9)
- May 8, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/7a/6c/7a6c472e8b0254783b46d3bdd7458bcba4bfa293448d2b6c9d5cb696cb4ace3d)

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