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