STC SR11332DS

SR11332DS Airbus Helicopters, Inc.

2701 N. Forum Drive Grand Prairie, TX 75052-7099 27 Code of Federal Regulations H9EU Airbus Helicopters AS350B3

1. Configurations 35A82-1681-01 and 35A82-1681-02 aircraft are limited to Post OP-4962 aircraft or AS350B3 aircraft with AHI STC SR11189DS installed.

2. Configuration 35A82-1681-03 is limited to post ECP 07.20207 aircraft with AHI STC SR11353DS installed. ---See continuation sheet 3--- 1/2/20 7/22/20 3/12/26 9/14/23 4/27/21 Michael R. Giambrocco, ODA-700097-SW ODA Lead administrator 3 Installation of 2nd Garmin GDU 1060 Display and optional L3 ESI-500 in accordance with Airbus Helicopters, Inc. Master Drawing List (MDL) 350A82-1924 Rev. B dated 06/26/2020 or later ODA approved revision.

SR11332DS 03/12/26 3

SR11332DS 03/12/26 Description of Type Design Change (continued from sheet 1):

350A82-1681-01: Rotorcraft Flight Manual Supplement (RFMS) 350FMS-570, Rev IR dated 7/22/2020 or later ODA approved revision is required and Instructions for Continued Airworthiness (ICA) 350MMS-074 Rev. IR dated 06/29/2020 or later ODA or AED accepted revision is required.

350A82-1681-02: Rotorcraft Flight Manual Supplement (RFMS) 350FMS-578, Rev IR dated 04/27/2021 or later ODA approved revision is required and Instructions for Continued Airworthiness (ICA) 350MMS-074 Rev. IR dated 06/29/2020 or later ODA or AED accepted revision is required.

350A82-1681-03: Rotorcraft Flight Manual Supplement (RFMS) 350FMS-578, Rev IR dated 04/27/2021 or later ODA approved revision is required and Instructions for Continued Airworthiness (ICA) 350MMS-074 Rev. B dated 3/10/2026 or later ODA or AED accepted revision is required.

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 is the same as TCDS H9EU, Rev 23, 11/18/2014, with the following exceptions: 27.610 Amdt 27-37, 27.773 Amdt 27-50, 27.1323 Amdt 27-13, and

27.1545 Amdt 27-16

Limitations and Conditions (continued from sheet 1):

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

4. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

5. Additional limitations may be detailed in the Rotorcraft Flight Manual Supplement(s).

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