STC SR00063DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00063DE

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 1 of 3

Part 6 of the Civil Air Regulations.

Installation of Inframetrics IRTV-445G Infrared Imaging System in accordance with Paravion Technology Master Drawing List DL-F28IR-100, dated September 7, 1993, FAA approved October 27, 1993 or later FAA approved revision.

1. FAA approved Rotorcraft Flight Manual Supplement dated November 3, 1993, or later FAA approved revision is required.

2. The cockpit video monitor installation must be FAA approved.

3. Paravion Technology, Inc. Report No. PR-F28IR-900M, "Inframetrics IRTV-445G System Installation Instructions" dated September 7, 1993, or later-revision is a required part of this installation.

This certificate and the supporting data which is the basis for ap proval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

This certificate issued to: Dart Aerospace Company 3845 NE 30th Avenue Hillsboro, OR 97124 Original Product Type Certificate Number: H1CE Make: The Enstrom Helicopter Corporation Model: F-28, F-28A, F-28C, F-28F, 280, 280C, 280F, 280FX Date of Application: January 27, 1992 Date Reissued: December 22, 2023 Date of Issuance: November 3, 1993 Date Amended:

Title: for Gregory S. DiLibero Aviation Safety Manager, West Certification Branch, AIR-770 Aircraft Certification Service

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00063DE

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 3

F rom (Name and address of grantor):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR00063DE

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 3 of 3

4. This approval should not be extended to aircraft 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 the aircraft.

5. A copy of this Certificate, Continuation Sheet, and FAA Rotorcraft Flight Manual Supplement dated November 3, 1993, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.