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During descent, the pressurization descent mode is activated when
Aircraft descends 0.25 psi below the selected FLT ALT
Aircraft descends 0.50 psi below the selected LAND ALT
Aircraft descends 0.25 psi below the selected LAND ALT
Aircraft descends 0.50 psi below the selected FLT ALT
Two independent radio altimeters provide radio altitude to the respective FCC's. With one radio altimeter inoperative
autopilot continues to command the aircraft down to minimums
autopilot disconnects two seconds after LOC and GS capture
autopilot disconnects as soon as the failure is detected
nothing out of the ordinary will occur
Blue illumination of APU GEN OFF BUS means
APU is running and powering transfer busses
APU is not running
APU is running
APU is running but not powering transfer busses
Yaw damper inputs (main or standby) can be overridden
By either trim or rudder pedals inputs
By rudder pedals inputs but not trim inputs
Only when the yaw damper switch is off
By trim inputs but not rudder pedals inputs
If the nose gear steering lockout pin is not installed for pushback or towing, then...
System B HYDRAULIC PUMPS must be switched off
System A HYDRAULIC PUMPS must be switched off
System A HYDRAULIC ELEC PUMP may be switched on
System B HYDRAULIC PUMPS must be switched on
Illumination of the STANDBY POWER OFF lights indicates
AC standby bus unpowered
DC bus 1 unpowered
Hot battery bus unpowered
DC bus 2 unpowered
On the ground, for primary ATC communication
Always use no. 1 VHF radio
Monitor the VHF radio connected to the lower antenna
Always use the no.2 VHF radio
No. 1 VHF for outbound and no. 2 VHF for inbound flights
The FMC Alerting Message INSUFFICIENT FUEL means:
You will not reach your destination before running out of fu
You will have less than 900kg (2000lbs) of fuel at the DEST
The APU is running out of fuel
It is necessary to increase the thrust setting
For landing, what is maximum fuel imbalance between No 1 and No 2 main tanks?
553 Kgs
653 Kgs
726 kgs
453 Kgs
What is the maximum authorised thrust reduction below any certified rating?
20%
35%
25%
10%
The APU may be used as a pneumatic source up to:
17,000 feet
10,000 feet
25,000 feet
41,000 feet
The number of flight spoilers located on each wing are:
2
3
4
6
The amber LOW PRESSURE Light for the No 1 Engine Driven Hydraulic Pump illuminates. What should you do?
Start the Elec pump
Monitor System A and B pressures
Position the pump switch to OFF
Select STBY RUD with FLT CONTROL switch A
What could cause the amber ANTISKID INOP Light to illuminate?
System B pressure is low
Brake accumulator pressure is in the red band
AUTO BRAKE select switch OFF
A fault in the parking brake system
The Predictive Windshear alerts are available:
Automatically below 2300 feet RA
When TERR switch on EFIS control panel is pressed
Automatically below 1200 feet RA
When WPT switch on EFIS control panel is pressed
With ENGINE START switch in OFF, automatic ignition will occur:
If ENG ANTI-ICE is selected ON
If N2 is between 57% and 50%
Will never occur
If N1 is between 57% and 50%
