# STC SR03794NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: ECMS Aviation Systems GmbH, Germany
- Description: Installation of External Load Attachment Device EAD03
- Applied: February 3, 2016
- Status date: August 26, 2016
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/58/55/58550d9601b9831d842215fe442415cb3afa598c27b4b58b55a1fe1f56deeddc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/06265765B5B9F74986258061005630F2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR03794NY

## ADs that name it (0)

None.

## Approved models (2)

- Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 D-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))

## 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 SR03794NY ECMS Aviation Systems GmbH Hirschmann-Ring 28 71726 Benningen

GERMANY Federal Aviation Regulations.

1. Installation of External Load Attachment Device EAD03 in accordance with Master Document List for EAD03, Revision 1, dated November 16, 2015 or later EASA approved revisions.

2. ECMS Aviation Systems GmbH Flight Manual Supplement for External Load System EAD03, Original Issue, dated May 1, 2015 or later EASA approved revisions is required for this modification.

1. "Lifetime Limitations" Section 11 of ECMS Aviation Systems GmbH Component Maintenance Manual (CMM) for External Load System EAD03, Original Issue, dated August 6, 2016 or later EASA approved revisions is required for this modification.

2. The aircraft must be operated in accordance with the “Limitations” section of ECMS Aviation Systems GmbH Flight Manual Supplement for External Load System EAD03, Original Issue, dated May 1, 2015 or later EASA approved revisions.

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

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

Raymond H. Reinhardt Acting Manager, New York Aircraft Certification Office Airbus Helicopters Deutchland GmbH (AHD) MBB-BK 117 C-2, MBB-BK 117 C-2E, MBB-BK 117 D-2 February 3, 2016 August 26, 2016 IMPORT H13EU 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SR03794NY

## Every issue (1)

- August 26, 2016: Issued, Current. [certificate](https://openairdocs.org/files/sha256/58/55/58550d9601b9831d842215fe442415cb3afa598c27b4b58b55a1fe1f56deeddc)

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