PMA Details TG3844038-4

Part Number: TG3844038-4
Part Name: Turbine Nozzle First Stage
Replaced Part Number: 3844038-4
Approval basis: Test and Computations per 14 CFR § 21.303
Models: Airbus (A310 series, A300-600 with Honeywell GTCP331-250 auxiliary power units installed on),Boeing (757-200, -200CB, -200PF, -300, -300F, 767-200, -300, -300F with Honeywell GTCP331-200 series auxiliary power units installed on)
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