System Questions 3 Flashcards
One ILS receiver is combined with one GPS receiver to form a(n):
Multi-Mode Receiver (MMR).
According to the ND, what are VOR 1 and VOR 2 tuned to?
ODI
What information is VOR 2 telling the pilot?
Ground based transmitter failure
What is a red VOR 2 on the ND mean?
VOR 2 Receiver has failed
Which of the following is false?
ADR information is available even though the IR unit’’s rotary knob is switched to OFF.
The SRS (Speed Reference System) is a managed speed relating to what phase of flight?
Takeoff
What is the slowest airspeed that should be flown in the clean configuration?
Green Dot
If you are flying an ILS approach, what must you press on this EFIS panel?
LS pushbutton
You are flying an ILS approach and an amber “ILS” indication is flashing on your PFD. The flashing “ILS” indicates:
An ILS approach has been initiated, but the “LS” button is not pressed.
According to the FMA, the APPR button has been pressed and:
Glideslope and Localizer is armed
What do the arrows on the PFD indicate?
Associated receiver has failed in flight
Based on the FMA, how many Flight Directors are on?
2
Based on the RADIO NAV page:
VOR 1 is manually tuned
The yellow arrow is pointing to the M. This symbol on the ND indicates:
The VOR has been manually tuned
Based on the RADIO NAV, in the CRS field:
A course of 165 has been manually inserted in the Radio Nav page.
Pressing the guarded NAV button:
Inhibits all autotuning capability by the FMGCs.
Based on the ND displaying “R”:
VOR frequency is tuned with the RMP
How do you deselect standby tuning of the RMP?
Deselect the guarded NAV button.
The RADIO NAV page displays navaids tuned by the FMGS or flight crew.
True
On aircraft with operational automatic alignment to GPS position, latitude and longitude entry is not required during FMGS preflight.
True
The FMGS remains in the Go-Around phase until the Activate APPR prompt is selected or:
A new destination is entered.
Normally, the VOR, DME, and ILS receivers are tuned:
Automatically by the FMGC.
Which of the following is true regarding the MCDU during takeoff?
The PM should display the F-PLAN page, while the PF should display the PERF page.
Which of the following regarding the SRS system on takeoff is correct?
During takeoff, SRS is the active vertical mode and commands a pitch attitude to maintain V2+10 knots.
SRS is maintained until acceleration altitude.
At acceleration altitude the Climb phase becomes active and the aircraft accelerates to the climb speed designated on the PERF CLB page.
Shortly after takeoff, LVR CLB flashes in column 1 of the FMA, indicating that:
The thrust reduction altitude entered on the PERF page has been reached.
During taxi for takeoff, ATC revises the departure runway. After correctly updating the departure runway in the FMGS, the scratchpad message CHECK TAKE OFF DATA appears. What does this message indicate?
The V1, VR and V2 speeds should be confirmed against the takeoff data.
In order to clear a hold from the flight plan, you could use the clear prompt, hit the IMM EXIT Prompt or:
Go direct to a waypoint.
The ACARS takeoff data function is available for the:
Active flight plan only.
What power setting does Alpha Floor command?
TOGA
In Direct Law, how is pitch trim controlled?
Manually using the Pitch Trim Wheels.
Which controls are available in Mechanical Back up?
Rudder and THS
Your aircraft is currently in a climb with a nose-up pitch attitude. You are hand-flying the aircraft and both sidesticks are currently in the neutral position. You are asking the flight control computers for:
No change in load factor.
Pitch protections provided in normal law include:
Maneuver protection
Pitch attitude protection
High speed and alpha protection
The A320 cannot be stalled in normal law.
True
Which statement below is true concerning the FACs?
Two FACs control rudder movement for automatic turn coordination, yaw damping, rudder limiting, and rudder trim.
If both sidesticks are moved in the same direction at the same time:
The total demand is never more than what can be realized with full deflection on only one sidestick.
You are hand-flying the aircraft. According to the indications shown:
The CA has pressed and held the left sidestick takeover pb and the right sidestick is making unwanted inputs to the flight control computers.