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ENGINE LIMITS
ITT Temp (°C)
Start ........................................................................................................................ 1000° C
Takeoff / Max Continuous ........................................................................................ 800° C
Cruise Climb / Normal Cruise ................................................................................... 770° C
Transient .................................................................................................................... 850° C
MENU RETURN King Air B200 & B200C Pro Line 21
Revision 1.1 FOR TRAINING PURPOSES ONLY L-12A
