A220- Landing Gear and Brakes

Question 1

The landing gear is electrically controlled and hydraulically actuated by which hydraulic system?

Answer 1

HYD system 1

Question 2

The nosewheel steering system uses which hydraulic system?

Answer 2

HYD system 2

Question 3

The “GEAR” aural warning cannot be muted if the landing gear is not down and locked, and Radio Altitude is less than _________ ft AGL, with the
slat/flap lever set to a landing position or both thrust levers set to approach idle

Answer 3

*1000 ft AGL,

Question 4

AUTOBRAKE rotary switch
RTO — During takeoff, autobrakes activate to bring the aircraft to a maximum performance stop when thrust levers are brought to idle and the aircraft speed is greater than ________ kts.

Answer 4

60 kt

Question 5

The steering tiller can move the nosewheel up to ________ degrees in either direction. The maximum steering angle decreases as speed increases.

Answer 5

80 degrees

Question 6

When the rudder pedals are used, regardless of speed, the nosewheel steering can be moved to a maximum of ________ degrees in either direction.

Answer 6

9 degrees