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SILVER AIRWAYS ATR 72 SYSTEMS EXAM STUDY GUIDE €13,65   In winkelwagen

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SILVER AIRWAYS ATR 72 SYSTEMS EXAM STUDY GUIDE

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  • Vak
  • ATR 72-600
  • Instelling
  • ATR 72-600

SILVER AIRWAYS ATR 72 SYSTEMS EXAM STUDY GUIDE

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  • 8 juli 2024
  • 233
  • 2023/2024
  • Tentamen (uitwerkingen)
  • Vragen en antwoorden
  • ATR 72-600
  • ATR 72-600
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Name: Score:
282 Multiple choice questions
Term
If Blue HYD pressure is below 1500 psi, the label on the SD will be:
Second / cyan
N/W STRG in amber
On ground and in flight
Low pressure (lp)1 of 282
Term
When the HDG button is pushed:
ALT* replaces the current active mode, and the command is to return to the altitude the
aircraft was passing at the time the button was pushed.
HDG SEL replaces the current active mode, and the command is to turn in the shortest
direction to the heading indicated by the heading bug position.
Between DU3 and DU4 below the gear lever.
1. Will illuminate once the panel is open
2. Indicates that battery power is being used
3. Will still drain the battery even if the battery toggle switch is in the OFF position2 of 282
Term
Roll trim is accomplished by changing the neutral position setting of _________ ______ _____ aileron
spring tab (s).
On lower half of the ewd
Only the left aileron spring tab
Engine failure
On ground and in flight3 of 282 Term
A Resolution Advisory is shown by:
In two gearboxes, one on the propeller reduction and the other on the HP spool.
The N/W Steering SW should be selected off and deflection angle is 91 °
A solid red square and indicates that the intruder is within 15 to 35 seconds from the
aircraft.
The engine high pressure compressor4 of 282
Term
The total fuel contained in both wing tanks is ___________ lbs.
deselect the loop from operation.
11025 (Wrong 11,020 lbs)
dc bus 1 and 2
11026 (wrong 11,020 lbs)5 of 282
Term
If NWS is not available ...
The aircraft has to be controlled using differential braking and thrust
HDG SEL replaces the current active mode, and the command is to turn in the shortest
direction to the heading indicated by the heading bug position.
Is driven by the power turbine and drives the ACW Gen, the PVM and Propeller brake for
the Right engine.
By a toggle switch on the Engine Rating Panel6 of 282 Term
Maximum Turning Capability on Ground is predicated on...
ALT* replaces the current active mode, and the command is to return to the altitude the
aircraft was passing at the time the button was pushed.
All are correct:
1. Automation mode and status information.
2. Aircraft flight parameter information.
3. Aircraft navigation information.
BLUE pressure < 1500 psi; prop brake released, gear handle DOWN . Either engine
running.
All are Correct:
maximum steering angle of 60 °
slow continuous turning
approximately idle thrust on all engines
no differential braking7 of 282
Term
In case elevators declutch, how can the elevators be reconnected.
Right actuator controlled tab travel
only in conjunction with the emergency procedure for the FWD SMK Warning.
VHF page with EDIT BOX on VHF 1 STBY Frequency
With the aircraft on ground, gust lock ON and the ELV clutch push button.8 of 282
Term
What is the power source for the LDG?
Forward and aft cargo compartments
On the eng start panel.
Lateral and vertical modes engaged
Electrically controlled and hydraulically powered9 of 282 Term
Condition Levers control the propeller rotation speed by changing the blade angle.
True
False10 of 282
Term
How many hydraulic systems are there on theATR72-600?
Contains the Virtual Control Panel (VCP), used to tune all radios.
2
18
2 and 411 of 282
Term
The hydraulic X Feed valve ___________.
Closes automatically (if open) for a LO LEVEL alert
opens the crossfeed valve and turns on both electrical fuel pumps.
1. Has a rotating cover to prevent accidental use
2. Once pressed, will sound a buzzer continuously in the FD
3. The FD crew has 30 seconds to DENY entrance
4. If the FD Crew does NOT DENY entrance, the door automatically unlocks
At the middle of the instrument panel12 of 282
Term
What are the propeller protections?
On both HSIs on the PFD and on the navigation display of the MFD
CACs to display VOR information on display units
Contains the Virtual Control Panel (VCP), used to tune all radios.
Propeller overspeed, low pitch and hydraulic pressure loss13 of 282

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