# STC SR00109RD

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: HeliMods Pty Ltd, Australia
- Description: Installation of the Powered Stretcher System
- Applied: February 11, 2020
- Status date: September 17, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/7e/23/7e239220620e6c36b8f71fb742025e7c3f2e89cedff7cc9e165ca9eece3c3078
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B890763B3D84450B862585EE006364DE.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00109RD

## ADs that name it (0)

None.

## Approved models (3)

- Airbus Helicopters Deutschland GmbH MBB-BK 117 C-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- 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 This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title H13EU Helimods Pty Ltd ACN 32 101 040448 Cnr Pathfinder Drive & Henebery Place Caloundra West, QLD 4551 3 SR00109RD Code of Federal Regulations29 Installation of the Powered Stretcher System in accordance with the Powered Stretcher System Install Procedures E5045-1039035 Revision 01 dated May 02, 2018 or later FAA approved revisions.

Continuation on page 3 of 3 Airbus Helicopters Deutschland GmbH MBB-BK117 C-1, C-2, and D-2

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

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.

3) A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

4) Aircraft with this STC embodied must be maintained in accordance with the Instructions for Continued Airworthiness E5065-1039025 Revision 1 dated August 24, 2018 and E5070-1039020 Revision 1 dated May 13, 2018 or later FAA accepted revisions.

February 11, 2020 September 17, 2020 IMPORT Jorge Castillo Manager, Rotorcraft Standards Branch

JORGE R CASTILLO Digitally signed by JORGE R

CASTILLO Date: 2020.09.21 09:30:18 -05'00'

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SR00109RD

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

3 Date of issuance: September 17, 2020 Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this STC is as follows:

14 CFR § 29 effective February 1, 1965 plus amendments 29-1 through 29-51 for the following regulations: 29.29, 29.251,

29.301, 29.303, 29.305, 29.307, 29.337, 29.341, 29.351, 29.471-, 29.479, 29.561, 29.601, 29.603, 29.605, 29.609, 29.611, 29.613,

29.619, 29.625, 29.783(e), 29.785(k), 29.803, 29.807, 29.811, 29.813, 29.815, 29.853, 29.1301, 29.1307, 29.1309, 29.1351, 29.1353,

29.1355, 29.1357, 29.1359, 29.1413(b), 29.1501, 29.1529, 29.1557, 29.1581, 29.1583, 29.1585, 29.1589 An Equivalent Level of Safety finding has been made for 14 CFR 29.561(b)(3), Emergency Landing Conditions as documented in ELOS Memo ST04307RD-R-C-01 --------------------------------------------------------------------------------------END-------------------------------------------------------------------------------- SR00109RD

## Every issue (1)

- September 17, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/7e/23/7e239220620e6c36b8f71fb742025e7c3f2e89cedff7cc9e165ca9eece3c3078)

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