Exam Questions Flashcards
Illumination of amber AUTO SLAT FAIL light that can be reset, during recall indicates:
Failure of a single stall management yaw damper (SMYD) computer
The hydraulic brake pressure indicator displays accumulator nitrogen pre-charge pressure of 1000 psi and:
Brake pressure from hydraulic system B if it is greater than 1000 psi
On which CDU page is the ground speed displayed?
POS REF page 2
One of the purposes of the FMC FIX INFO page is to:
Create a new waypoint at the intersection of the active route with a radial or distance from a known fix
Once activated, the APU DC operated fuel pump operates automatically until:
An AC fuel pump pressurises the manifold
Electrical power to start the APU comes from:
The No 1 transfer bus if available if AC power is not available, battery power is used
A DUCT OVERHEAT light only will cause:
The temperature mix valves to drive full cold
Cruising at FL370. The motorised Overboard Exhaust valve will open in flight if:
Either pack switches are in HIGH and recirculation fan is OFF
If ON DC on left IRS mode selector unit comes ON steady it means:
The related IRS is operating on DC power from the switched hot battery bus
ZONE TEMP amber light illumination for CONT CAB with master caution indicates:
? A duct temperature overheat
? Failure of both flight deck primary and standby temperature controller
The APU starter cycle may take up to:
120 seconds
In addition to hydraulic system A and B, the rudder can also be powered by the standby hydraulic system through the
Standby Rudder PCU
If the thrust lever(s) are advanced after touchdown:
After 3 seconds in the advanced position the AUTO BRAKE DISARM light will illuminate
The red landing gear indication lights are illuminated under which of the following conditions?
? Landing gear is in disagreement with LANDING GEAR lever position
X Landing gear is not down and locked (with either or both thrust levers retarded to idle, and below 800 feet AGL)
Both
The landing gear configuration warning horn will activate anytime a gear is not down and locked:
With flaps set to 15, one thrust lever at idle and the other at low power setting (below 34 degrees)
L NAV will automatically disengage:
Reaching a route discontinuity
Cargo compartment smoke detection is powered from:
DC bus 1 and DC bus 2
An amber IAS DISAGREE alert in the bottom of the speed tape indicates:
The Captains and First Officers airspeeds disagree by more than 5 KTS for more than 5 seconds
The FMC alerting message RESET MCP ALT means:
Aircraft within 5 NM of the FMC calculated Top of Descent (TOD) point without selecting lower altitude on the MCP
What is the source of electrical power for the engine fuel shutoff valves?
The Battery Bus
How are the Engine Bleed Air valves powered?
They are DC activated and pneumatically operated
Following an unpressurised takeoff, when is the first engine Bleed Switch positioned to ON?
At not less than 400 feet, and prior to 2000 feet above field elevation
On the Audio Control Panel (ACP) the Cabin Call lights comes ON. It will illuminate until:
Remains illuminated for 40 seconds
The AC Standby Bus is powered by:
The AC Transfer Bus No 1 under normal conditions
The Autoslat system:
Drives the slats to FULL EXTEND when TE Flaps 1 through 5 are selected and the aircraft approached a stall
The Predictive Windshear alerts are available:
Automatically below 1200 feet RA
Illumination of the PSEU fault light on the aft overhead panel will indicate:
An overwing exit flight lock fails to disengage on the ground
The ND Wind direction/speed and wind arrow is:
Displayed if wind speed is greater than 6 knots
The right IRS is electrically powered from:
Normally AC Transfer Bus 2 and in an emergency from switched hot battery bus for a maximum of 5 minutes
The left IRS is electrically powered from:
Normally AC Standby bus b in emergency from switched hot battery bus
The supplemental and temporary data bases has storage capacity for:
40 navaids and 6 airports
Do not attempt to make a turn away from an obstacle within:
nose 7.4, wing 5.4
In MANUAL pressurisation mode the outflow valve is driven by?
A motor supplied from DC standby bus
DFDR records for how long, when does it work
25h, operates whenever it has power and either engine is operating
After lift-off, the A/T remains in THR HLD until:
800’
The APU can supply both transfer busses:
on the ground or in the air