11. OS Question CBT

Question 1

FG 5.1: On the HUD, the lateral deviation indication of the navigation information indicates:

Accepted Answer

The left or right FMS cross track with respect to the active leg.

Answer

The next leg track.

Answer

The LOC (localizer) deviation.

Answer

The direct to track symbol.

Question 2

FG 5.2: During takeoff roll and rotation, which of the next statements is true:

Accepted Answer

A “pitch target” symbol indicates to the pilot the pitch target to be achieved after rotation.

Answer

The FD symbol is displayed on the HUD and PFD.

Answer

The shape of the “pitch target” symbol remains unchanged.

Answer

The “pitch target” symbol is displayed during the climb phase.

Question 3

FE 5: F-speeds are:

Accepted Answer

The recommended speed during approach for flaps extension.

Answer

The speeds which ensure that the aircraft speed remains above VLS and VFE.

Answer

The minimum recommended speeds for flaps retraction during takeoff.

Answer

The recommended speeds during a go-around for flaps extension.

Question 4

FE 6: What is the VMAX equivalent in clean config?

Accepted Answer

VMO / MMO

Answer

VREF

Answer

VFE

Answer

VLE / MLE

Question 5

FM 3: The FMS is able to manage up to … SEC F-PLNs.

Accepted Answer

3

Answer

4

Answer

5

Answer

2

Question 6

FM 3: The NAV AP/FD DATA DISAGREE alert advises the flight crew that the following systems can be lost:

Accepted Answer

AP’s, FD’s and AFS CP

Answer

AP’s and FD’s only

Answer

AP’s, FD’s, PRIM’s and AFS CP

Answer

AP’s, FD’s, GADIRUS and AFS CP

Question 7

FM 4: About the Temporary (TMPY) F-PLN:

Accepted Answer

It is a copy of the ACTIVE F-PLN that includes the F-PLN revisions.

Answer

Its color is green.

Answer

It is a copy of the SEC F-PLN.

Answer

It does not need to be confirmed by the crew.

Question 8

FM 5.1: The Required Time of Arrival (RTA) is:

Accepted Answer

Not taken into account by the FMS for F-PLN predictions.

Answer

A lateral revision of the F-PLN.

Answer

A time error value information displayed on the HUD and NTD.

Answer

The estimated takeoff time.

Question 9

FM 5: If the synchronization between both FMS is lost, the mode of operation is:

Accepted Answer

Independent.

Answer

Dependent.

Answer

Dual.

Answer

Single.

Question 10

FM 6.1: After the creation of a Flight Plan (F-PLN), the flight crew:

Accepted Answer

Can revise it at any time.

Answer

Cannot revise, update or modify it in any case

Answer

Can revise it on ground only.

Answer

Can do lateral revisions only.

Question 11

FM 6: The FMS can manage up to

Accepted Answer

4 flight plans.

Answer

2 flight plans.

Answer

3 flight plans.

Answer

5 flight plans.

Question 12

FM 7.1: The lateral revisions are related to the modification of the following parameters:

Accepted Answer

Alternate route.

Answer

Required time of arrival.

Answer

Altitude.

Answer

Speed.

Question 13

FM 9: Which of the next formats are interactive?

Accepted Answer

NTD and FM

Answer

PFD

Answer

HUD

Answer

HUD and PFD

Question 14

FM 9: One of the Fuel and Load page parameters that can be modifiable are:

Accepted Answer

The minimum fuel at destination (MIN FUEL AT DEST).

Answer

The estimated takeoff weight at departure airport (TOW).

Answer

The estimated fuel on board (EFOB) at destination.

Answer

The estimated trip fuel (TRIP).

Question 15

FM 10: The flight plan (F-PLN) defines

Accepted Answer

The intended lateral and vertical aircraft trajectory from the departure to the destination airport and from the destination to the alternate airport (if any).

Answer

The intended vertical trajectory.

Answer

The intended lateral and vertical trajectory from the departure to the alternate airport.

Answer

The intended lateral trajectory.

Question 16

FM 10: A click on the “SURLY ERASE ALL” button…

Accepted Answer

Deletes all user data and switches both FMS off.

Answer

Deletes only the ACTIVE flight plan.

Answer

Switches only FMC 2 off.

Answer

Switches only FMC 1 off.

Question 17

FM 11: How many phases is the vertical F-PLN divided into?

Accepted Answer

8

Answer

10

Answer

6

Answer

12

Question 18

LDG GR/BRK 1: Select the correct statement:

Accepted Answer

The blue hydraulic system pressurizes the parking brake accumulator.

Answer

The parking brake is only operative when engines are running.

Answer

The yellow hydraulic system pressurizes the parking brake accumulator.

Answer

The parking brake decelerates the aircraft after touchdown or rejected takeoff.

Question 19

COM 1: The AUDIO MODE sw in the AUDIO MODE panel on the main instrument panel:

Accepted Answer

Enables the flight crew to select between normal and tactical transmission.

Answer

Enables to switch between the Manual (MAN) mode, the Automatic Link Establishment (ALE) mode and the ALE AUTOmatic (ALE AUTO) mode.

Answer

Enables the flight crew to select between normal and emergency transmission.

Answer

Enables to manually force HF transmissions, mainly for secured transmissions.

Question 20

COM 2: The Passenger Address (PA) system:

Accepted Answer

Enables any crewmember to make aural announcements to the passengers.

Answer

Has three modes of operation: general mode, private mode and emergency mode.

Answer

Enables any passenger to make aural announcements to the flight crew.

Answer

Enables secure external communications between the passengers and ground installations or other aircraft.

Question 21

COM 3: The Emergency Locator Transmitter (ELT):

Accepted Answer

Transmits an emergency signal over the three international distress frequencies.

Answer

Cannot be removed from the aircraft

Answer

Determines the direction from which an incoming emergency signal is transmitted.

Answer

Cannot be manually activated nor manually deactivated.

Question 22

NET 1: The Aircraft Multipurpose Access Terminal:

Accepted Answer

Enables maintenance and mission data operator interface with the NSS hosted applications.

Answer

Is located on the right console in the cockpit.

Answer

Enables any user to access all data hosted on avionics equipment.

Answer

Is only operative on ground.

Question 23

NET 3.1: If a single IOM fails:

Accepted Answer

There is no effect, as the redundant IOM ensures full functionality.

Answer

Communication between its connected aircraft systems and both avionics networks is lost.

Answer

It causes a partial network loss.

Answer

There is an ECAM alert on the cockpit.

Question 24

NET 3.2: The communication, navigation and identification management provides:

Accepted Answer

Control, monitoring and interface between CDS and RMP.

Answer

Monitoring only.

Answer

Control only.

Answer

Public address management.

Question 25

NET 4: The loss of two switches on the same network:

Accepted Answer

The redundancy is degraded.

Answer

Causes a total network loss

Answer

Has no functional effect.

Answer

Causes the loss of interconnected systems.

Question 26

FUEL 2: Select the correct statement about the vent network:

Accepted Answer

The vent network enables the surge TKs to collect the fuel that may overflow.

Answer

Any fuel spilled into the surge TKs is then returned to the center TK.

Answer

Any fuel spilled into the surge TKs is discharged overboard via the overpressure disks.

Answer

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.

Question 27

FUEL 3.1: Which system controls and monitors the fuel system on ground and in flight?

Accepted Answer

The Fuel Quantity and Management System (FQMS).

Answer

The Full Authority Digital Engine Control (FADEC).

Answer

The Control and Display System (CDS).

Answer

The Flight Management System (FMS).

Question 28

FUEL 3.2: The jettison function:

Accepted Answer

Minimizes the potential of an overweight landing.

Answer

Provides protection against fire and explosion.

Answer

Enables to collect any fuel spilled into the surge TKs and discharge it overboard via the vent outlets.

Answer

Enables to increase the aircraft range and endurance.

Question 29

FUEL 3.3: According to the FUEL SD:

Accepted Answer

The standby and the main pumps 3 are OFF.

Answer

There is a fuel transfer failure.

Answer

The fuel of the FEED TK 3 is not usable.

Answer

The engine 3 is OFF.

Question 30

FUEL 3.4: The aircraft is normally refueled on ground:

Accepted Answer

Using pressure fueling via the refuelling coupling unit.

Answer

Using pressue fueling via the jettison outlets located on the wing trailing edge.

Answer

Using pressure fueling via the refuelling point in the upper side of the left inner tank.

Answer

Using unpressurized fueling via the refuelling probe.

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11. OS Question CBT

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	Erstellt von Jose Antonio Vazquez vor mehr als 3 Jahre