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
The right IRS is electrically powered from:
normally AC Transfer Bus 2 - in emergency from switched hot battery bus for a maximum of 5 minutes
What happens to the digital readout of the radio alt when descending below minimums?
The dial and pointer of the radio altimeter flash amber for 3 seconds
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
When does the RAD ALT display a digital readout?
Between 2500ft AGL and 1000ft AGL
While making a no engine bleed air take off and an engine failure occurs, when should the bleed air switches be positioned to ON?
Reaching 1500 feet AGL or until obstacle clearance height is reached
When is the exhaust valve open:
A: On the ground
B: In the air
Open with low differential pressures.
Normally closed, and sent to the FWD cargohold in flight
Open if either pack is in high, and the right recirc fan is off
Spar and engine shutoff valves are controlled by which power-sources?
Spar from the hot battery bus.
Engine from the battery bus
In flight L and R recirculation fans will, when:
a. one pack is high
b. two packs are high
a. left turns off
b. both turn off
On the ground, recirculation fans will when:
a. one pack is high
b. both packs are high
a. both will operate
b. left will turn off
What is the minimum pavement width for a 180 degree turn?
24,1m
Wingtip height above the ground is
6.4m
Do not try to turn away from an obstacle within
a. x meters of wing tip
b. x meters of nose
a. 5.4m
b. 7.4m
Elevator feel system is provided by the elevator feel computer. This computer receives inputs of:
Airspeed and stabiliser position
After a normal take-off, what pitch command can you expect from the F/D?
V2 + 15
As you push the TO/GA switch for an automatic go around, what is the correct FMA announciation? (Thrust : Roll : Pitch)
GA : : TO/GA
During battery start, when does the EEC start to operate?
15%
Does the door need to be open, when operating the airstairs from:
a. inside
b. outside
a. yes
b. no
The wing-span of the 737-800 is:
35.79m
Which is the correct mode on the FMA? Condition: After takeoff, A/P engaged, before flaps up. (Thrust: Roll: Pitch)
N1 : LNAV : MCP SPD
You get TCAS alerts within how many seconds from closest approach for
a. TA
b. RA
a. 40 seconds
b. 25 seconds
Two independent radio altimeters provide radio altitude to the respective FCC’s. With one radio altimeter inoperative:
the autopilot will disconnect two seconds after LOC and GS capture
After flare is armed, with a loss off an RA, what will happen
The AP will hand you back the airplane during the flare
In flight, the Predictive Windshear Warning:
will activate for windshear up to 1.5nm ahead of the aircraft
In what mode will the TCAS automatically show if a TA/RA occurs and the TFC switches are selected OFF?
MAP, CTR MAP, VOR, APP
Switching the CAB/UTIL switch OFF removes all 115v AC from the galley busses and:
left and right recirculation fans
If all TEMPERATURE ZONE SELECTORS (knobs, not switch) are positioned to OFF with both packs operating:
the left pack maintains 24 degrees, the right 18 degrees
during single pack operation, with trim air on, how is zone temp controlled?
same is with dual pack operation
During one pack operation with trim air off, how is the system operated
Attempts to produce air for average of all 3 zones
If CONT CAB temp controller fails (both) what temperature will be provided to the flight deck
The packs will go in independent operation, and the flight deck will get air temperature selected from left pack
Which of these is indicated by the hydraulic Brake Pressure Indicator?
Maximum pressure 3500psi in white
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
Prior to returning to the oil tank engine oil passes through:
the scavenge filter and main engine oil cooler
The FMC Alerting Message INSUFFICIENT FUEL means
ou will have less than 900kg (2000lbs) of fuel at the destination
During descent, the pressurization descent mode is activated when:
Aircraft descends 0.25 psi below the selected FLT ALT
The EMERGENCY EXIT LIGHTS Switch in the ARMED position:
Illuminates all interior and exterior emergency lights if there is a loss of electrical power on DC bus No 1, or AC power has been turned off
A DUCT OVERHEAT light only will cause:
The temperature mix valves to drive full cold
When using halon fire extinguishing in the flight deck:
Both crew must don oxygen masks and set EMER
Minimum in-flight tank fuel temperature is:
3 degrees above the fuel freezing point or -43 degrees, whichever is higher
Manual IRS entries of present position or magnetic heading are normally accomplished on the
POS INIT page or the ISDU
Engine Fuel Flow is measured:
after passing through the engine fuel shutoff valve
In AUTO, the FASTEN BELTS and RETURN TO SEAT signs:
illuminate when flap or gear are extended
TCAS TA Only mode is enabled automatically:
elow 1000ft RA when TA/RA mode is selected
Where are the bleed
trip sensors installed?
Sensors are positioned
on both sides of the
engine bleed air valve.
At or below 28,000 feet the
pressurization controller
maintains a pressure
differential of:
7.45
At or above 37,000 feet the
pressurization controller
maintains a pressure
differential of:
8.35
Between 28,000 feet and 37,000 feet the
pressurization controller
maintains a pressure
differential of:
7.8
When do the ram air
inlet doors move to the
full open position?
On the ground or
during slow flight with
flap not fully retracted
With pack switches set to AUTO, if one pack fails, when does the remaining pack provide high air flow:
only when the aircraft
is in flight, flaps up
Which actions will extinguish the ENG FAIL alert over the EGT indication
- Engine recovers
- engine start lever is moved to CUTOFF
- engine fire warning switch is pulled
The fuel quantity
displayed on the FMC
PROGRESS page is:
total fuel onboard, as
obtained from the fuel
quantity indication
system
A Fuel CONFIG alert is
extinguishes if:
Centre tank quantity
les than 363kg
Amber Fuel IMBAL alert
will remain displayed
until the imbalance is
reduced to:
91kg
What airspeed must be
considered with a wheel
well fire situation?
Extend limit speed of
270k/.82M maximum
When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly:-
there will be a GPWS 'minimums' callout since the callouts are based on the captains minimums selector
When can you expect
the EGPWS ‘five
hundred’ call?
When descending
through 500ft RA
outside 2 dots of the
LLZ
