# STC SR03386NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aerospace Design and Certification, Ltd., United Kingdom
- Description: The installation of Honeywell International Inc. s (Model #LTS101-850B-2) engines
- Applied: August 20, 2012
- Status date: April 16, 2014
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU)
- Certificate PDF: https://openairdocs.org/files/sha256/88/87/88871bb15a39fa23e57ea84ee6eb5c2381f2d7dbf13d1e4c02d18763b6dc6b5b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F83733E06FD0743886257D080072E0CD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR03386NY

## 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.

This certificate issued to

Part 29 of the Federal Aviation Regulations.

Original Product -- Type Certificate Number : H13EU

1. The installation of Honeywell International Inc.’s (Model #LTS101-850B-2) engines within Airbus Helicopter Deutschland GMBH’s (Model #MBB-BK117 B-2) helicopter to be done in accordance with AERODAC’s Master Data List, Job #JN216 Form #ADC17, Task: (1), Issue 2, Rev. -, Approved for Release on February 29, 2012, or later EASA approved revision.

2. Operation must be in accordance with Rotorcraft Flight Manual Supplement, Job #JN216, Form #ADC29, Task: (1), Issue 1, Rev -, dated May 3, 2012, or later EASA accepted revision and Rotorcraft Flight Manual Supplement – Category A Operations, Job #JN216, Form# ADC29, Task (2), Issue 1, Rev. -, dated May 3, 2012, or later EASA accepted revision.

3. Maintenance must be in accordance with and AERODAC’s Instructions for Continued Airworthiness, Job #JN216, Form #ADC54-29, Task (1), Issue 2, Rev. -, dated March 3, 2014 or later EASA accepted revision.

1. The Airworthiness Limitation must be in accordance with and AERODAC’s Instructions for Continued Airworthiness, Job #JN216, Form #ADC54-29, Task (1), Issue 2, Rev. -, dated March 3, 2014 or later EASA accepted revision.

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

3. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other pe rson written evidence of that permission.

Aerospace Design and Certification Limited (T/A AERODAC) Stone Building Paddockhurst Road RH10 4SF Turners Hill United Kingdom Make : Airbus Helicopters Deutschland GMBH Model: MBB-BK 117 B-2 Date of application : August 20, 2012

Date of issuance : April 16, 2014

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SR03386NY Date of Issuance: April 16, 2014 Certification Basis

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification to the Airbus Helicopter Deutschland GMBH, Model MBB-BK117 B-2 Series is as follows:

a. The type certification basis for the Airbus Helicopter Deutschland GMBH, Model MBB-BK117 B-2 Series as shown on the TCDS H13EU for parts not changed or not affected by the change.

b. The type certification basis for the Airbus Helicopter Deutschland GMBH, Model MBB-BK117 B-2 Series as shown on the TCDS H13EU for parts changed or affected by the change with the following exemptions:

• Compliance with 14 CFR §§ 29.672, 29.1329, & 29.1587 at Amendment 29-24.

…END…

## Every issue (1)

- April 16, 2014: Issued, Current. [certificate](https://openairdocs.org/files/sha256/88/87/88871bb15a39fa23e57ea84ee6eb5c2381f2d7dbf13d1e4c02d18763b6dc6b5b)

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