Written test Flashcards
(50 cards)
During taxi, which part of the aircraft requires the largest turning clearance?
The tail
Cabin zone temperatures can be controlled:
On the flight deck control panel or when transferred to the flight attendant control panel
With the recirculation fan button in the AUTO position, the fans are commanded off…
If the dump button is pressed IN
During normal operations, the conditioned air consists of:
52% fresh air, 48% recirculated air
During normal takeoff with AT armed, the FMA annunciation’s will be:
White TO with the TLA less than 50 degrees
Green TO with the TLA greater than 50 degrees
Hold with speed > 60 kts
Informing the AP/FD of an intended CAT II approach is accomplished by:
Setting RA/BARO to RA and adjusting Min to 80 ft or above
What does the OVRD annunciation on the FMA mean?
Symmetric manual levers commanded by pilot, overriding the autothrottle
What is indicated by the acceleration pointer on the PFD?
Indicated aircraft acceleration and deceleration rate along the flight path
Where is the selected VHF COM indicated?
Audio control panel display will show it
Which of the following procedures is applicable to establish alternative VHF tuning?
With the CCD actuate the VHF box on the PFD and tune the new frequency with the CCD tuning knob
The DC electrical network consists of:
2 DC BUSES, 3 DC ESS BUSES, 2 HOT BATT BUSES, 1 APU BUS, 1 DC GND SERVICE BUS
In the event of total generator loss in flight while the RAT is being deployed, the DC ESS BSES 1 and 2 are supplied with current from?
HOT BATT BUSES 1 and 2
An amber LED light beside the IDG disconnect switch…
Indicates the IDG must be disconnected
Pulling down the engine fire extinguishing handle on the flight deck will:
Close the respective fuel, hydraulic and bleed shutoff valves
In the event of a cargo fire on the ground, the pilot pushes the illuminated fire extinguisher button. This provides:
The high rate bottle to be discharged, while the low rate bottle is armed automatically and must be discharged manually
Which of the following are not driven by Fly-by-Wire system technology
The ailerons only
When the ram air turbine is the only source of power…
The slats and flaps will operate at half speed
What is the priority of the pitch trim switches?
Back up, captain, first officer, FCM
In case of airspeed data loss…
The flight control operation is defaulted to fixed control laws
How are the ailerons controlled and operated?
Hydro-mechanical
When LOW 1 is selected on the fuel control panel:
Fuel cross feed valve opens and AC pump 2 activates
How is overpressure in the integral wing tank prevented?
A pressure relief valve opens
Which power sources are used to drive the three hydraulic systems?
System 1 and 2 are powered by an EDP and backed up by an ACMP, System 3 is powered by an ACMP and backed up by another ACMP
What is the important function of the system 3 accumulator, compared to the accumulators installed for system 1 and 2?
During an electrical emergency, it will provide hydraulic power to associated flight controls
