Airbus P/N 3840223-4E

묘사: Blade, Turbine, 1st Stage

airbus 모델

• Honeywell GTCP131-9[A] GTCP131-9[B] GTCP131-9[D] as installed on MD-90

All applicable aircraft models:

Airbus (Honeywell GTCP131-9[A] GTCP131-9[B] GTCP131-9[D] as installed on Model A319-111, 112, 113, 114, 115, 131, 132,-133 Model A320-111, 211, 212, 214, 231, 232, 233 Model A321-111, 112, 131, 211, 231) Boeing (Honeywell GTCP131-9[A] GTCP131-9[B] GTCP131-9[D] as installed on 737-600, 700, 800, 900) McDonnell Douglas (Honeywell GTCP131-9[A] GTCP131-9[B] GTCP131-9[D] as installed on MD-90)