PMA Details E23072654-UC

Part Number: E23072654-UC
Part Name: Nozzle Assembly, Turbine C20 2nd Stage
Replaced Part Number: 23072654, 23074472
Approval basis: Test & Computations per 14 CFR § 21.303 DWG No E23072654-UC Rev B Date 1/28/03, or later FAA approved revisions
Models: Rolls-Royce (250-C20B, C20C, C20F, C20J, C20R, C20R/1, C20R/2, C20R/4)
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