# STC SR02567SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Airwork (NZ) Limited, New Zealand
- Description: Installation of an Inlet Particle Separator
- Applied: January 8, 2016
- Status date: December 27, 2017
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/00/e4/00e402168ba3e74a4325f0a8971adaf78552c4ff79d898ded80bdaa933dc8647
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7EF31DB4913A94ED86258218004F677E.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR02567SE

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SR02567SE

This certificate, issued to Airwork NZ Ltd.

487 Airfield Road, Ardmore Airport Auckland, PO Box 72 516, Papakura 2244, New Zealand

Part 29 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H13EU Make: Airbus Helicopters Deutschland GmbH (AHD) Model: MBB-BK 117 B-2

Description of the Type Design Change: Installation of an Inlet Particle Separator in accordance with Airwork (NZ) Limited Installation Instructions STC.AW.3022 II, Revision 5, dated June 22, 2016, or later Federal Aviation Administration (FAA) approved revision. Maintained in accordance with Airwork (NZ) Limited Instructions for Continued Airworthiness (ICA) Document STC.AW.3046 Instructions for Continued Airworthiness , Issue 4, dated April 19, 2017, or later FAA-accepted revision. Operated in accordance with Airwork (NZ) Limited Rotorcraft Flight Manual Supplement (RFMS) STC.AW.3046 FMS, Revision 3, dated November 30, 2016.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only.

The FAA has determined that this modification is compatible with STC SR03386NY. This approval should not be extended to other rotorcraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate, the ICA, and the RFMS must be maintained as part of the permanent records for the modified rotorcraft.

Certification Basis: Title 14 Code of Federal Regulations part 29 effective February 1, 1965, plus Amendments 29-1 through 29-16, with the following exceptions: 29.45 (29-24), 29.59 (29-24), 29.67 (29-26), 29.75 (29-17),

29.77 (29-24), 29.79 (29-21), 29.141 (29-21), 29.143 (29-24), 29.1045 (29-26), 29.1047 (29-26), 29.1309 (29-53),

29.1359 (29-42), and 29.1587 (29-24).

Date of application: January 8, 2016 Date reissued: December 27, 2017 Date of issuance: September 29, 2017 Date amended:

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (2)

- December 27, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/00/e4/00e402168ba3e74a4325f0a8971adaf78552c4ff79d898ded80bdaa933dc8647)
- September 29, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/06/d6/06d61f77da36d71bfdfd07a4082a2cb54fa2b003e9b130bcf06a408dca678655)

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