The Flight Management part of the FMGEC includes the following elements :
B.
You are in cruise at FL330 and have on the FCU under the speed window the numbers 280. You can say that :
A.
In the second line on the FMA, What does it mean the ALT mode status in magenta color ?
A.
The aircraft is heavy. The thrust delivered by A/THR is already at MAX CLB thrust (needle to the blue circle on the thrust gage). Is it possible to obtain some additional thrust?
B.
How can clear a discontinuity in your F-PLN ?
B.
ATC cleared you to FL 150. The PF set the new altitude on the FCU. What will happen if he pulls the ALT selection knob knowing the there is a ALT constraint at FL 60 in the FLT PLN ?
A.
ATC cleared you to FL 150. What selections should you make to ensure that the aircraft complies with the lower constraints at FL 60 ?
A.
With regards to the SRS mode, during the takeoff phase :
A.
The FMA displays -FD2 in white in the fifth column :
C.
An AP can be disengaged by :
- using the AP take-over pb of a side stick,
- using the AP pb in the FCU,
- moving a side stick or a rudder pedal beyond a given threshold.
A. True
B. False
A
You are flying an approach in good weather and decide to fly the aircraft manually. After disconnecting the autopilot, what standard technique should you use to disconnect the A/THR?
D.
Selected HDG is active on an intercept heading. What happens if the HDG selector knob is pushed?
A. The aircraft will fly to the next waypoint on the original F-PLN.
B. The aircraft will continue on heading until intercepting the original F-PLN.
C. The aircraft will continue on the selected HDG/TRK.
D. The selection changes from HDG to TRK.
When A/THR is active, thrust levers :
B.
You can disengage the AP by :
or overriding the rudder pedals on ground only.
A.
To display localizer and glide slope indications on the PFD, you need to :
A.
To level off immediately, you should :
A.
To switch from speed to Mach on FCU, you need to :
C.
Select the correct statement regarding the FMA :
B.
MCDU failures are :
C.
Select the true statement regarding the FMA :
C.
Fail annunciator is lighted on the left bottom side of the MCDU 2, MCDU 3 could be used :
C.
The A 330 thrust levers are not only used to supply thrust but also send input to the FMGEC :
C.
If requested information such as GW, CRZ FL, and COST INDEX are not set :
C.
The flight management part of the FMGEC :
A.
On the MCDU, the PERF FACTOR is :
C.
The NAV DATA BASE :
A.
The PERF DATA BASE :
A.
In normal operation, interfacing with the FMGEC is carried out by :
C.
On the MCDU screen, INDEPENDANT OPERATION is displayed in amber and IND amber on the upper part, according to these indications :
B.
On the MCDU screen, PLEASE WAIT is displayed, according to these indications :
B.
On the MCDU upper part, FM 1 amber annunciator is lighted, on the STATUS PAGE, you have INOP " FM1 AP1 ", the FM switching button is in " both on 2 " position ; according to these indications :
A.
MCDU 3 is a stand -by unit able to replacing MCDU one or two :
A.
To select BACK-UP NAV on the MCDU :
A.
According to the MCDU POSITION MONITOR page, the RADIO, and MIX IRS positions are slightly different. This is because :
C.
The MIX IRS position is :
B.
In normal operation, to insert the latitude and the longitude of the departure airport into the 3 IRS, the pilot should :
C.
During descent FMA indicates :
THR IDLE / DES / NAV / BLANK / AP1
Pilot has to follow radar heading, when pulling the HDG pb on FCU, FMA indicates :
C.
On the MCDU upper part, FM 1 amber annunciator is lighted, so FM 1 has failed. Therefore :
C.
In order to manually tune the VOR on RMP, the pilot must :
A.
In order to provide the ECON speed for cruise flight, the pilot must :
B.
AP engaged in ALT CRZ mode, ATHR soft mode consist to :
B.
The flight guidance performs :
C.
The FLIGHT GUIDANCE function displays information on :
A.
The AP function :
C.
In cruise, the FCU shows 300 on the SPD window and --- on the HDG window :
B.
In cruise, the FCU shows 300 on the SPD window and 145 on the HDG window :
C.
The FMA indicates in the first column SPEED in green and A/THR in white in the fifth column. The A/THR is :
A.
The FE part performs GW and CG calculations. These calculation are used :
A.
The crew entry of the ZFW and the CG is :
A.
When performing an autoland, the red AUTO LAND flashing light means :
B.
In case of FMGEC failure, the Flight Director :
B.
During take off, the RUNWAY MODE makes you :
B.
The ROLL OUT mode make you keep the heading of the runway and :
B.
Performing a manual ILS approach (AP off, FD ATHR On), the thrust reduction on landing :
B.
During landing, the IDLE MODE of the A/THR reduce thrust :
A.
MANAGED or SELECTED MODE :
- the Managed Mode is activated when flying under AP
- the Selected Mode is activate when flying manually.
A.
During ILS approach with FD On, when losing the GLIDE signal under LAND MODE, the FD pitch bar :
C.
528. During ILS approach with FD On, when losing the LOC signal under LAND MODE, the FD roll bar :
A.
During normal operation, both FMGEC are working :
C.
You can engage AP :
B.
You can engage both AP :
A.
During approach, the FMGEC target speed is :
C.
The ALT mode is engaged :
A.
During descent, V/S mode has been activated with AP/FD/ATHR On; with selected speed on FCU, the target of AP is :
C.
Flying under NAV MODE, the airplane is reaching a flight plan discontinuity :
A.
During take off, to leave SRS MODE :
C.
During approach (AP/FD ON), the APPR p/b is green on FCU :
C.
Below 400 ft during ILS approach, LAND MODE :
C.
In flight A/THR On, you set the thrust lever to IDLE detent then to CL detent :
B.
In flight, A/THR On, thrust levers in CL detent, pilot disconnects A/THR by pushing
the A/THR p/b on FCU :
B.
In flight A/THR On, thrust levers between CL detent and MCT detent, pilot disconnects A/THR by FCU p/b or A/THR failure occures :
B.
A/THR is armed :
A.
When flying with one engine out, A/THR is active between :
B.
Alpha Floor protection is available :
C.
LVR ASYM on FMA means :
B.
To check accuracy of FMS navigation :
B.
The target speed on PFD is blue when :
C.
On FMA, pilot can read on the fifth column 1FD-. That's mean :
A.
By pushing the APPR p/b on FCU, pilot :
C.
When A/THR is active, by pushing the A/THR p/b on thrust levers :
B.
During descent under OPEN DES mode, pilot selects altitude greater than aircraft altitude :
B.
Below 300 ft LAND mode is active, pilot disconnects AP, FMA becomes :
B.
After take off, NAV mode engaged, CLB mode becomes active :
A.
After start up, to update weight, pilot uses :
A.
DECEL point is :
A.
If approach phase is activated and confirmed on PERF page :
C.
Using " Update function " on PROG page, pilot can modify :
C.
SPD CSTR is a constraint associated to :
A.
The FMA indicates : THR IDLE, DES, NAV and vertical deviation is (VDEV = +500 ft). Pilot wants to increase the rate of descent :
C.
What are the Autopilot functions?
D.
A/THR in white means that A/THR is:
B.
What is the difference between -FD2 and 2FD- on the FMA?
A. 1 inop, 2 engaged. 2 engaged, 1 off.
B. 1 off, 2 engaged. 2 engaged, 1 inop.
B
Can the autopilot be used for a single engine approach and autoland?
A. Yes.
B. No.
A
During the takeoff phase:
B.
On an autoland approach, with both autopilots on, which FMGC is master?
