AIRBUS A320 FCOM DSC-22 AUTO FLIGHT Part3

Question 1

About predictions for the primary flight plan, if the flight crew does not fly the flight plan, the MCDU predictions assume that ?

The "selected" data (selected on the FCU)

You will fly back towards the flight-planned route or you will immediately resume flying the FMGC managed modes

Question 2

About predictions for the primary flight plan, if the flight crew does not fly the managed speed profile, the MCDU predictions assume that you will maintain the selected speed until they reach?

In climb or descent phase, the next speed limit or speed constraint if any, or next phase ; in cruise, the top of descent

Until the decel point or when you activate the approach phase

Until the landing

The last way point of the flight plan

Question 3

To get the energy circle symbol (green arc) on the ND, which represents the required distance to land, find the wrong answer below :

The lateral guidance mode is heading or track

The current FMS flight phase is in cruise, descent or approach

The aircraft is within 180nm of the destination

The lateral guidance mode is in NAV (managed)

Question 4

The predicted time of arrival at the TO WPT which is located in the upper right-hand corner of the ND assumes direct distance from the aircraft position to the TO WPT and assumes ?

Current Ground Speed (GS) will be constant

The speed with the prediction data (average wind or wind ins[...]

Question 5

In case of engine-out (EO), the EO target speed computed by the FMGS during climb is?

Green Dot speed

220 kt or green dot + 10 (whichever is greater)

250 kt

275 kt

Question 6

In case of engine-out (EO), the EO target speed computed by the FMGS during cruise is?

Green Dot speed

220 kt or green dot + 10 (whichever is greater)

250 kt

EO CRZ SPD

Question 7

The recommended maximum altitude (REC MAX) is the lowest of the maximum altitude, which answer is uncorrect?

The aircraft can reach with 0.3 g buffet margin

The aircraft can fly in level flight at MAX CRZ rating

The aircraft can maintain a V/S of 300 ft/min at MAC CLB thrust

The aircraft can fly at a speed higher than Green Dot and lower than VMO/MMO

The aircraft is certified at

The aircraft can turn with a roll of 66°

Question 8

Predictions for alternates are displayed on the ALTERNATES page, if the airway distance is less than 200 nm, for the calculatuion a default cruise FL equal to?

FL 100

FL 180

FL 220

FL 310

Question 9

Entering a PERF factor of +1.5 means that flight operations have evaluated the aircraft fuel deviation as ?

1.5 %

5 %

15 %

50 %

Question 10

The FMGS uses the IDLE factor to adjust the computationf of? (DATA -> A/C STATUS)

The vertical profile during the descent phase (IDLE segment)

The engines when thrust levers are in IDLE

Question 11

On the INIT B page, on the [4L] ALTN/TIME, it displays alternate trip fuel and time, assuming that the aircraft flies at the default cruise flight level and with the Cost Index ?

CI = 0

CI = 15

CI = 35

CI = 99

Question 12

How many waypoints can be created and stored?

Unlimited

Question 13

How many NAVAIDs can be created and stored?

Unlimited

Question 14

How many RUNWAYs can be created and stored?

Unlimited

Question 15

How many ROUTEs can be created and stored?

Question 16

The Speed Reference Sysrem (SRS) mode will be unavailable at takeoff if ?

You do not enter a V1

You do not enter a VR

You do not enter a V2

You do not enter a FLEX

Question 17

During the cockpit preparation, on the PERF takeoff page "TO SPEED TOO LOW" amber message appears on the MCDU scratch pad, what does it means ?

The inserted V1,VR,V2 speeds do not satisfy the existing regulatory conditions regarding VMCG/VMCA and VS1G speeds

The inserted V1,VR,V2 are too low, you should insert higher speeds

Your Indicated Airspeed (IAS) is too low

You have inserted a V1 below 100 knots

Question 18

During the cockpit preparation, on the PERF takeoff page you have inserted the altitude of the ENG OUT ACC (5R), but what happen if after taking off you have an engine-out, what can you expect on the FMA passing the altitude of the engine out acceleration

Lever climb "LVR CLB" Will flash

The aircraft Will start acceleration until climb speed

Nothing special, it is for display only, as a reminder

"ENG OUT ACC" will flash

Question 19

On the PERF APPR Page, F, S, GREEN DOT and VLS speeds are computed by ?

The Flight Warning Computer (FWC)

The Flight Mode Annunciator (FMA)

The Speed Reference System (SRS)

The Flight Management and Guidance System (FMGS) assuming landing weight

Question 20

On the PERF APPR Page, the VLS is the VLS of ?

The actual VLS according the aircraft configuration

The clean comfiguration

The selected LDG CONF (3 or FULL)

Question 21

On the PERF APPR page, The FMGC (Flight Management and Guidance Computer) computes VAPP speed, using the formula ?

VAPP = VLS + 1/3 of the headwind components (limited to VLS +5 as a minimum and VLS +15 as a maximum)*

VAPP = VLS - tower head wind component

VAPP = VLS + tower head wind component

VAPP = VLS + current head wind component

Question 22

On the PERF APPR page, The FMGC (Flight Management and Guidance Computer) computes VLS which is equal to ?

1,05 VS1G of the selected landing configuration (full or 3)

1,13 VS1G of the selected landing configuration (full or 3)

1,23 VS1G of the selected landing configuration (full or 3)

1,3 VS1G of the selected landing configuration (full or 3)

Question 23

On the PERF GO AROUND page you have inserted the altitude of the ENG OUT ACC (5R), but what happen if after going around if you have an engine-out, what can you expect on the (FMA) passing the altitude of the engine out acceleration?

Lever climb "LVR CLB" Will flash

The aircraft Will start acceleration until climb speed

Nothing special, it is for display only, as a reminder

"ENG OUT ACC" will flash

Question 24

On the PROG page, the OPT (optimum) flight level is computed based on?

The current gross weight

The current gross weight and cost index

The current gross weight, cost index and temperature

The current gross weight, cost index, temperature and wind

Question 25

On the PROG page, the REC MAX (recommended maximum ) altitude is computed based on?

The current gross weight

The current gross weight and temperature, and assuming that anti-ice is off*

The current gross weight and cost index

The current gross weight, cost index and temperature

Question 26

On the PROG page, the REC MAX (recommended maximum ) altitude provides the aircraft with?

A 0,3g buffet margin, a minimum rate of climb at MAX CL (maximum climb) thrust and a level flight at MAX CRZ thrust

A 1g buffet margin, a minimum rate of climb at MAX CL (maximum climb) thrust and a level flight at MAX CRZ thrust

A 1,23g buffet margin, a minimum rate of climb at MAX CL (maximum climb) thrust and a level flight at MAX CRZ thrust

A 1,3g buffet margin, a minimum rate of climb at MAX CL (maximum climb) thrust and a level flight at MAX CRZ thrust

Question 27

On the PROG page, the field of REC MAX (recommended maximum ) altitude is limited to?

FL 390

FL 395

FL 398

FL 410

Question 28

On the PROG page, on the line 4 where is BRG/DIST, if you enter on the field an airport, waypoint, navaid, runway, latitude/longitude (LL), place/bearing/distance (PBD), place-bearing/place-bearing (PBX), it shows?

A radio bearing and distance from site to aircraft position

The FMGC computed bearing and distance from site to aircraft position

Question 29

In case of engine out at take off, the SRS (Speed Reference System) mode maintain a speed target as V2, or the current speed if it higher but no more than?

V2 + 5

V2 + 10

V2 + 15

Question 30

In case of engine out during a go around, the dpeed target is VAPP, or the current speed if higher, limited to?

VLS + 15

V2 + 15

VLS + 10

V2 + 10