LANDO NORRIX

What happens when the landing gear lever is in OFF position. Landing gear extend. Landing gear retract. Hydraulic system pressure removed. Landing gear is inoperative.

Landing gear is supplied by?. Hydraulic A. Hydraulic B. PTU. STANDBY only.

Normal Brake is supplied by?. Hydraulic A. Hydraulic B. PTU. STANDBY only.

Alternate Brake is supplied by?. Hydraulic A. Hydraulic B. PTU. STANDBY only.

AutoBrake is supply by?. Hydraulic A. Hydraulic B. PTU. STANDBY only.

Antiskid is supplied by?. Hydraulic A. Hydraulic B. Normal brake and Alternate Brake. STANDBY only.

Autobrake is not intiated when?. if rejected prior 80 knots. if rejected prior 88 knots. if rejected prior 82 knots.

Landing autobrake setting may be selected after touchdown prior to decelerating 30 Kts: False. True.

Airborne, No 1 engine RPM bellow limit, Landing gear lever UP position, either main landing gear is not UP and LOCKED. Are conditions to operate: PTU. STS. Landing gear transfer valve.

With the manual extension access door open, the landing gear can be retracted?. True. False.

How can the Landing gear be retracted?. SYSTEM B. SYSTEM A. Manually. All of them. System A and B.

Nose Wheel Steering is normally operated by?. SYSTEM A. SYSTEM B.

Autobrake disarm actions are: Apply manual brake pressure of 750 PSI. Moving speed brake lever to the down detent. Advancing the forward thrust levers. All of them.

If we loose NORMAL and ALT BRAKE how can we stop the airplane?. Using STANDBY SYSTEM. Using the Accumulator. PTU. Alternate brake.

A fault in parking brake system may cause the. ANTI SKID INOP light to illuminate. Landing gear light illuminate. Autobrake disarm light illuminate. brake pressure to drop.