PMA Details 23072654AL

Part Number: 23072654AL
Part Name: Nozzle Assembly, Turbine - 2nd Stage
Replaced Part Number: 23031938
Approval basis: Test and Computation per 14 CFR § 21.303 Dwg No 23072654AL Rev I/R Date 5/7/02, or later FAA approved revisions
Models: Rolls-Royce (250-B17, B17B, B17C, B17D, B17E, B17F, B17F/1, B17F/2, C20, C20B, C20C, C20F, C20J, C20R, C20R/1, C20R/2, C20R/4, C20S, C20W)
Holder: Timken Alcor Aerospace Technologies Inc
Holder number: PQ2203NM
Address: 3110 North Oakland Mesa AZ (United States)
Office: Phoenix AZ FAA Office Tel: (480) 419-0330

Certificat: FAA