FG 5.1: On the HUD, the lateral deviation indication of the navigation information indicates:
The left or right FMS cross track with respect to the active leg.
The next leg track.
The LOC (localizer) deviation.
The direct to track symbol.
FG 5.2: During takeoff roll and rotation, which of the next statements is true:
A “pitch target” symbol indicates to the pilot the pitch target to be achieved after rotation.
The FD symbol is displayed on the HUD and PFD.
The shape of the “pitch target” symbol remains unchanged.
The “pitch target” symbol is displayed during the climb phase.
FE 5: F-speeds are:
The recommended speed during approach for flaps extension.
The speeds which ensure that the aircraft speed remains above VLS and VFE.
The minimum recommended speeds for flaps retraction during takeoff.
The recommended speeds during a go-around for flaps extension.
FE 6: What is the VMAX equivalent in clean config?
VREF
VFE
VLE / MLE
VMO / MMO
FM 3: The FMS is able to manage up to … SEC F-PLNs.
3
4
5
2
FM 3: The NAV AP/FD DATA DISAGREE alert advises the flight crew that the following systems can be lost:
AP’s and FD’s only
AP’s, FD’s, PRIM’s and AFS CP
AP’s, FD’s, GADIRUS and AFS CP
AP’s, FD’s and AFS CP
FM 4: About the Temporary (TMPY) F-PLN:
It is a copy of the ACTIVE F-PLN that includes the F-PLN revisions.
Its color is green.
It is a copy of the SEC F-PLN.
It does not need to be confirmed by the crew.
FM 5.1: The Required Time of Arrival (RTA) is:
A lateral revision of the F-PLN.
Not taken into account by the FMS for F-PLN predictions.
A time error value information displayed on the HUD and NTD.
The estimated takeoff time.
FM 5: If the synchronization between both FMS is lost, the mode of operation is:
Dependent.
Independent.
Dual.
Single.
FM 6.1: After the creation of a Flight Plan (F-PLN), the flight crew:
Cannot revise, update or modify it in any case
Can revise it at any time.
Can revise it on ground only.
Can do lateral revisions only.
FM 6: The FMS can manage up to
4 flight plans.
2 flight plans.
3 flight plans.
5 flight plans.
FM 7.1: The lateral revisions are related to the modification of the following parameters:
Required time of arrival.
Altitude.
Speed.
Alternate route.
FM 9: Which of the next formats are interactive?
NTD and FM
PFD
HUD
HUD and PFD
FM 9: One of the Fuel and Load page parameters that can be modifiable are:
The estimated takeoff weight at departure airport (TOW).
The estimated fuel on board (EFOB) at destination.
The estimated trip fuel (TRIP).
The minimum fuel at destination (MIN FUEL AT DEST).
FM 10: The flight plan (F-PLN) defines
The intended vertical trajectory.
The intended lateral and vertical trajectory from the departure to the alternate airport.
The intended lateral trajectory.
The intended lateral and vertical aircraft trajectory from the departure to the destination airport and from the destination to the alternate airport (if any).
FM 10: A click on the “SURLY ERASE ALL” button…
Deletes only the ACTIVE flight plan.
Deletes all user data and switches both FMS off.
Switches only FMC 2 off.
Switches only FMC 1 off.
FM 11: How many phases is the vertical F-PLN divided into?
8
10
6
12
LDG GR/BRK 1: Select the correct statement:
The parking brake is only operative when engines are running.
The blue hydraulic system pressurizes the parking brake accumulator.
The yellow hydraulic system pressurizes the parking brake accumulator.
The parking brake decelerates the aircraft after touchdown or rejected takeoff.
COM 1: The AUDIO MODE sw in the AUDIO MODE panel on the main instrument panel:
Enables to switch between the Manual (MAN) mode, the Automatic Link Establishment (ALE) mode and the ALE AUTOmatic (ALE AUTO) mode.
Enables the flight crew to select between normal and emergency transmission.
Enables the flight crew to select between normal and tactical transmission.
Enables to manually force HF transmissions, mainly for secured transmissions.
COM 2: The Passenger Address (PA) system:
Has three modes of operation: general mode, private mode and emergency mode.
Enables any crewmember to make aural announcements to the passengers.
Enables any passenger to make aural announcements to the flight crew.
Enables secure external communications between the passengers and ground installations or other aircraft.
COM 3: The Emergency Locator Transmitter (ELT):
Cannot be removed from the aircraft
Determines the direction from which an incoming emergency signal is transmitted.
Cannot be manually activated nor manually deactivated.
Transmits an emergency signal over the three international distress frequencies.
NET 1: The Aircraft Multipurpose Access Terminal:
Is located on the right console in the cockpit.
Enables any user to access all data hosted on avionics equipment.
Is only operative on ground.
Enables maintenance and mission data operator interface with the NSS hosted applications.
NET 3.1: If a single IOM fails:
Communication between its connected aircraft systems and both avionics networks is lost.
There is no effect, as the redundant IOM ensures full functionality.
It causes a partial network loss.
There is an ECAM alert on the cockpit.
NET 3.2: The communication, navigation and identification management provides:
Monitoring only.
Control only.
Control, monitoring and interface between CDS and RMP.
Public address management.
NET 4: The loss of two switches on the same network:
Causes a total network loss
The redundancy is degraded.
Has no functional effect.
Causes the loss of interconnected systems.
FUEL 2: Select the correct statement about the vent network:
Any fuel spilled into the surge TKs is then returned to the center TK.
The vent network enables the surge TKs to collect the fuel that may overflow.
Any fuel spilled into the surge TKs is discharged overboard via the overpressure disks.
The vent network enables the transfer of fuel from the center TK to the inner TKs and from the inner TKs to the feed TKs.
FUEL 3.1: Which system controls and monitors the fuel system on ground and in flight?
The Full Authority Digital Engine Control (FADEC).
The Control and Display System (CDS).
The Fuel Quantity and Management System (FQMS).
The Flight Management System (FMS).
FUEL 3.2: The jettison function:
Minimizes the potential of an overweight landing.
Provides protection against fire and explosion.
Enables to collect any fuel spilled into the surge TKs and discharge it overboard via the vent outlets.
Enables to increase the aircraft range and endurance.
FUEL 3.3: According to the FUEL SD:
The standby and the main pumps 3 are OFF.
There is a fuel transfer failure.
The fuel of the FEED TK 3 is not usable.
The engine 3 is OFF.
FUEL 3.4: The aircraft is normally refueled on ground:
Using pressure fueling via the refuelling coupling unit.
Using pressue fueling via the jettison outlets located on the wing trailing edge.
Using pressure fueling via the refuelling point in the upper side of the left inner tank.
Using unpressurized fueling via the refuelling probe.
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