PMA Details TG3844012-3

Part Number: TG3844012-3
Part Name: Second Stage Stator
Replaced Part Number: 3844012-3
Approval basis: Test and Computations per 14 CFR § 21.303
Models: Airbus (Honeywell GTCP331-250 auxiliary power units as installed on: A310, A300-600),Boeing (Honeywell GTC331-200 series auxiliary power units as installed on 757-200, -300, 767-200, -300)
Holder: Triumph Engineering Services Inc
Holder number: undefined
Address: 4246 East Wood Street Suite 560 Phoenix AZ (United States)
Office: Phoenix AZ FAA Office Tel: (480) 419-0330

Certificat: FAA