除冰/防冰后应当清除空气动力感应区域和空腔内聚集或者残存的除冰/防冰液，可不清洁风挡玻璃上的除冰/防冰液痕迹 .

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:

THE ELECTRONIC INSTRUMENT SYSTEM (EIS) INCLUDE:

THE EIS COMPRISES SEVERAL SYSTEM COMPUTERS, THESE COMPUTERS ARE: