充分考虑除冰/防冰液污染对起飞性能和失速特性的影响，并采取适当的补偿措施：减小载重、减小起飞速度.

ON THE EXTERNAL POWER (EXT PWR) PANEL, WHEN THE "AVAIL" AND ＇NOT IN USE" LIGHTS ARE ILLUMINATED:

THE ATTENDANT INDICATION PANEL (AIP) IS LOCATED:

THE COCKPIT SLIDING WINDOWS CAN BE OPERATED FROM THE:

THE ENGINE FIRE EXTINGUISHING SYSTEM IS SUPPLIED BY:

WHEN AN APU FIRE OCCURS ON GROUND:

THE MOVEMENTS OF THE PRIMARY FLIGHT CONTROL SURFACES ARE MANAGED BY:

THE ENGINE DRIVEN PUMPS (EDPs) NORMALLY PRESSURIZE:

THE YELLOW HYDRAULIC SYSTEM IS NORMALLY PRESSURIZED BY:

THE COMPLETE PROBE HEAT SYSTEM INCLUDES:

THE WING LEADING EDGE ANTI-ICED SECTIONS ARE: