# STC SH5519SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: The NORDAM Group LLC, United States
- Description: Modification of crew door sliding window.
- Applied: August 22, 1983
- Status date: April 1, 2019
- 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/ba/d2/bad208d8e6c93bae6ec7f79e96924a308811a7afbcf86ddbaac6ce0130930259
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FD4AD400387FC2CF862586C3004F2D19.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SH5519SW

## ADs that name it (0)

None.

## Approved models (6)

- Airbus Helicopters Deutschland GmbH MBB-BK 117 A-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 A-3 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 A-4 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 B-1 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 B-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU))
- Airbus Helicopters Deutschland GmbH MBB-BK 117 C-1 ([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 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SH5519SW The NORDAM Group LLC 6910 N. Whirlpool Tulsa, OK 74117 Part 29 the Federal Aviation Regulations H13EU AIRBUS HELICOPTERS DEUTSCHLAND GmbH (AHD) MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK 117 C-1 Modification of crew door sliding window in accordance with Drawing M-BK117-24100 dated June 29, 1983, E.O. No. 1 dated September 2, 1983, and E.O. No. 2 dated September 13, 1983, or later FAA approved revison.

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

August 22, 1983 1/1/97; 9/20/99; 4/1/2019 August 23, 1983 January 17, 2002; Rev. 1 Jim Grigg Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service 2

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SH5519SW 2

## Every issue (1)

- April 1, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ba/d2/bad208d8e6c93bae6ec7f79e96924a308811a7afbcf86ddbaac6ce0130930259)

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