STC SR11333DS

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Part of .

SR11333DS Airbus Helicopters, Inc.

2701 N. Forum Drive Grand Prairie, Texas 75052-7099 27 Code of Federal Regulations H9EU Airbus Helicopters AS350B3 Installation of a FLIR UltraForce 350-HD Surveillance System in accordance with Master Drawing List 350A82-1914 Rev. A dated 3/15/2021 or later ODA approved revision. Rotorcraft Flight Manual Supplement 350FMS-562 Rev. A dated 04/15/2021 or later ODA approved revision is required and Instructions for Continued Airworthiness 350MMS-061 Rev. IR dated 3/26/2021 or later ODA or AEG accepted revision is required.

1. This STC is limited to Airbus Helicopters AS350 B3 Post Post AMS 07-3439 with high skid gear.

2. With this STC installed, reduce VNE power-off by 10 knots, with a minimum of 65 knots.

---See continuation sheet 3--- 09/15/2020 04/15/2021 Gina Gonzales ODA Lead Administrator ODA-70097-SW 3

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SR11333DS 3

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

SR11333DS Description of Type Design Change (continued from sheet 1):

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 except for the following:

• 14 CFR 27.2 at Amendment 27-37

• 14 CFR 27.173 at Amendment 27-44

• 14 CFR 27.175 at Amendment 27-44

• 14 CFR 27.177 at Amendment 27-44

• 14 CFR 27.562(a1)(c5) at Amendment 27-25

• 14 CFR 27.773 at Amendment 27-50

• 14 CFR 27.1323 at Amendment 27-13

Note: 27.562 is not part of the original certification basis for this aircraft. The AHI ODA has elected to find limited compliance due to the density of the interior completion.

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.

---END--- The latest effective date of this STC is 04/15/2021.

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

SR11333DS 3

FAA Form 8110-2 (10/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

SR11333DS 3