STC SR00133DE

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

(See Continuation Sheet Page 3 of 3 Pages) Page 1 of 3 SR00133DE Dart Aerospace USA, Inc 3845 NE 30th Avenue Hillsboro, OR 97124 Part 27 the Federal Aviation Regulations H11EU Airbus Helicopters AS355E, AS355F, AS355F1, AS355F2, AS355N Installation of External Pod and Camera Mount per Paravion Technology, Inc. Drawing List Report Number DL-355CM-100, Revision NC, FAA approved November 21, 1994, or later FAA approved revision.

May 18, 1993 November 16, 2023 November 28, 1994 for Manager, West Certification Branch

1. This approval is for the pod and mount only. The camera and monitor must be separately FAA approved as noted in the Installation Instructions.

2. FAA approved Rotorcraft Flight Manaul Supplement, dated November 28, 1994, or later approved revision is required.

3. Paravion Technology, Inc. Report Number PR-355CM-900M, "Camera Mount Installation Instructions" dated June 27, 1994, or later revision is a required part of this Installation.

4. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

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

Page 2 of 3 SR00133DE

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

End Page 3 of 3 Limitations and Conditions Continued:

SR00133DE

5. The installation describes 2 different mount locations, a right side or left side. No configuration combinations are allowed, only one mount location per installation is allowed.

6. A copy of this Certificate, Continuation Sheet, and FAA Rotorcraft Flight Manual Supplement, dated November 28, 1994, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

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