# STC SR04510NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Ultimate Aerostructures, Canada
- Description: Installation of the Fuel Filler Port Protective Plate
- Applied: May 4, 2020
- Status date: June 24, 2020
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/84/64/846498d3fd198ca8d852122daf836f864fb27909c01bfc6081a7c6af05f6d879
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/70ADC7861AF91FA0862585EB003C0585.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR04510NY

## ADs that name it (0)

None.

## Approved models (1)

- Airbus Helicopters Deutschland GmbH MBB-BK 117 B-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 Timothy J. Hadsall Acting Manager New York ACO Branch IMPORT SR04510NY Ultimate Aerostructures 613-10301 104 Street NW Edmonton, Alberta Canada T5J 1B9 29 Federal Aviation Regulations.

**H13EU MBB-BK 117 B-2**

1. Installation of the Fuel Filler Port Protective Plate must be in accordance with Transport Canada Civil Aviation (TCCA) approved Ultimate Aerostructures (ULTAero) Engineering Order UA404-EO, Revision IR, dated July 31, 2017, or later TCCA approved revisions.

2. Maintenance of the Fuel Filler Port Protective Plate must be in accordance with TCCA accepted ULTAero Instructions for Continued Airworthiness UA404-ICA, Revision IR, dated July 31, 2017, or later TCCA accepted revisions.

3. Definition of the Type Design Change can be found in TCCA approved ULTAero Master Data List UA404-MDL, Revision IR, dated July 31, 2017, or later TCCA 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 this certificate to alter a product, the holder must give the other person written evidence of that permission.

Airbus Helicopters Deutschland GmbH May 4, 2020 June 24, 2020 2

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

To (Name and address of transferee)

From (Name and address of grantor)

2 SR04510NY

## Every issue (1)

- June 24, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/84/64/846498d3fd198ca8d852122daf836f864fb27909c01bfc6081a7c6af05f6d879)

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