Examen Sistemas A320

The aircraft has two turbofan engines mounted under the wings.

The aircraft has two high bypass turbofan engines mounted under the wings

The aircraft has two high bypass turbofan engines.

150.

179.

145.

30.2M/95.5Ft

37.0/124.0Ft

34.1M/111.1Ft

Radome, Nose Gear Bay, Air Conditioning Compartment, Main Gear Bay, Tail Cone.

Nose Gear Bay, Air Conditioning Compartment, Main Gear Bay.

Radome, Nose Gear Bay, Air Conditioning Compartment, Main Gear Bay, Cargo Compartments, Tail Cone.

70.2°

75°

80°

2 PACK flow control valves, 2 PACKs.

3 PACK flow control valves, 2 PACKs and Mixing Unit.

2 PACK flow control valves, 2 PACKs and Mixing Unit.

3

5

2

PACK overheating, engine starting, operation of the fire pushbutton and operation of the ditching pushbutton.

Engine starting, operation of the fire and operation of the ditching pushbutton.

Engine starting.

With a ΔP 1.5

With a ΔP 1.0

With a ΔP 8.0

YES

NO

T.O.: When T.O. Power is applied until the Main Landing Gear Struts are DECOMPRESSED.
Landing: When the Main Landing Gear Struts are COMPRESSED until 20s after 70Kts.

T.O.: When T.O. Power is applied until FLAPS are retracted.
Landing: When the Main Landing Gear Struts are COMPRESSED until 70Kts.

T.O.: When T.O. Power is applied until FLAPS are retracted.
Landing: When the Main Landing Gear Struts are COMPRESSED until 20s after 70Kts.

YES

NO

APU Bleed "ON", operation with One PACK.

T.O. Power is applied, APU Bleed "ON", operation with One PACK.

T.O. Power is applied, APU Bleed "ON", operation with One PACK, In-Flight.

The related PACK is lost.

The related PACK is lost, and the hot air pressure-regulating valve and associated trim air valves close.

The related PACK is lost, and the hot air pressure-regulating valve and associated trim air valves open.

4

6

2

2 CPCs, 1 Outflow valve, 1 Control Panel, 2 Safety valves.

1 CPCs, 1 Control Panel, 2 Safety valves.

2 CPCs, 1 Outflow valve, 2 PACKs, 1 Control Panel, 2 Safety valves.

1

2

3

ADIRS

LGCIU

FMGC

70s after landing.

If the operating one fails.

Both.

Ground, T.O., Climb, Cruise, Descent.

Ground, T.O., Climb, Cruise, Descent, Abort.

T.O., Climb, Cruise, Descent.

The outflow valve, the emergency ram air inlet, the avionics ventilation inlet and extract valves closes.

The outflow valve, the avionics ventilation inlet and extract valves, and the pack flow control valves closes.

The outflow valve, the emergency ram air inlet, the avionics ventilation inlet and extract valves, and the pack flow control valves closes.

The Avionics, the Battery, Lavatories and Galleys.

The Avionics, the Battery.

The Avionics, Cockpit and Cabin.

The Avionics Ventilation goes to OPEN CIRCUIT CONFIG.

The Avionics Ventilation goes to CLOSED CIRCUIT CONFIG.

The Avionics Ventilation goes to INTERMEDIATE CIRCUIT CONFIG.

The Ventilation System goes to Closed Circuit Config.

The Ventilation System goes to Open Circuit Config.

The Ventilation System goes to Intermediate Config.

The Ventilation System goes to Closed Circuit Config. But the Extract Fan keeps running.

The Ventilation System goes to Open Circuit Config. But the Blower Fan keeps running.

The Ventilation System goes to Intermediate Config. But the Extract Fan keeps running.

With the Blower and Extract Fans.

With RAM Air.

With a Venturi.

Blower Fan

Extract Fan

2 FMGCs, 2 MCDUs, 1 FCU, 3 FACs

2 FMGCs, 2 MCDUs, 1 FCU, 2 FACs

2 FMGCs, 2 FCU, 2 SECs

Selected, Managed.

Selected, Managed, Flight Directors.

Auto Thrust, Auto Pilot, Selected, Managed.

True

False

True

False

4

2

1

Rudder, Rudder Trim, Yaw Damper, Flight Envelope and Speed functions, Low-Energy Warning and Windshear Detection.

Rudder, Rudder Trim, Yaw Damper, Flight Envelope and Speed functions.

Flight Envelope and Speed functions.

Dual mode, Independent mode, Single mode, Back-up navigation mode.

Dual mode, Independent mode, Single mode.

Dual mode, Single mode.

An average position, based on the 3 IRS.

An average position, based on 2 IRS.

The drift error caused by a faulty IR.

A vector between the MIX IRS and the Radio/GPIRS Position

A vector between the MIX IRS and the Radio Position

A vector between the MIX IRS and the GPIRS Position

IRS-GPS

IRS-DME/DME

IRS-VOR/DME

1

2

4

Nothing

Listen to the Morse Code

Change the Nav-Aid

15min

30sec

10min

Excessive motion, disagreement of position, position not entered.

Alignment fault

GPS PRIMARY LOST

PROG Page

FUEL PRED Page

INIT B Page

1.0 G

0.2 G

0.3 G

V2+10

V2+5

V2+15

When you preselect a HDG

When the LOC signal is available

When the YAW BAR is not available

OPEN CLB/DST

CLB/DST

V/S

At Vmax+4

At Vmax+8

At Vmax

An interrupted tone sounds for 5 s, and the emission is turned off.

Nothing.

An ECAM appears.

Yes

No

Tune the VOR, release the VOR reception knob and press the on voice key.

Tune the VOR, release the VOR reception knob.

Release the VOR reception knob.

Yes

No

Move the Audio Switching Selector to F/O 3

Move the Audio Switching Selector to CAP 3

Computer reset

Pressing the CVR ERASE button for 2 seconds IF the Aircraft is on the ground and Parking Brake ON

Pressing the CVR ERASE button for 2 seconds IF Parking Brake ON

Pressing the CVR ERASE button for 6 seconds IF the Aircraft is on the ground and Parking Brake ON

AC BUS 1

AC BUS 2

EMER GEN

Yes

No

75KVA

90KVA

110KVA

75KVA

90KVA

110KVA

Yes

No

1

2

3

Failure of both AC BUS 1 and 2

Failure of AC BUS 2

Failure of TR 1

10s

8s

15s

No more than 2s

No more than 5s

No more than 3s

1

2

3

1

2

3

1 for both compartments

1 for each compartment

2 for each compartment

2 ELACs, 3 SECs, 2 FACs

3 ELACs, 3 SECs, 2 FACs

1 ELACs, 2 SECs, 1 FACs

Yes

No

Yes

No

They drop 5° (Aileron Droop)

They drop 10° (Aileron Droop)

They drop 3° (Aileron Droop)

Yes

No

Center Tank, Inner Tank, Outet Tank, Ventilation Tank

Center Tank, Inner Tank, Outet Tank

Center Tank, Inner Tank

10m

5m

2m

When the Inner Tank have 750kg

When the Inner Tank have 1000kg

When the Inner Tank have 500kg

Yes

No

Differential pressure greater than 500PSI

Differential pressure greater than 700PSI

Differential pressure greater than 200PSI

Yes

No

3

2

1

3

2

1

200Kts

230Kts

250Kts

OAT

Pitot

TAT

1

2

3

It transfers the failed ECAM DU to the Captain ND

It transfers the failed ECAM DU to the Captain PFD

It transfers the failed ECAM DU to the F/O ND

Blank screen with an Amber "F", distorted display, blank screen with the “INVALID DISPLAY UNIT” message in amber

Blank screen with an Green "F", distorted display, blank screen with the “INVALID DISPLAY UNIT” message in green

Blank screen with an Amber "X", distorted display, blank screen with the “INVALID DISPLAY UNIT” message in amber

STS page automatically comes up

Nothing

An ECAM Caution appears

1. L/G not downlocked and radio height lower than
750 ft and
both engines N1 lower than 75 % (or if engine shut
down N1 of remaining engine lower than 97 %)
or
2. L/G not downlocked and radio height lower than
750 ft and both engines not at T.O. power and
flaps at 1, 2, 3 or FULL
or
3. L/G not downlocked and flaps at 3 or FULL and
both radio altimeters failed

1. L/G not downlocked and radio height lower than
750 ft and
both engines N1 lower than 75 % (or if engine shut
down N1 of remaining engine lower than 97 %)
or
2. L/G not downlocked and radio height lower than
750 ft and both engines not at T.O. power and
flaps at 1, 2, 3 or FULL

1.L/G not downlocked and radio height lower than
750 ft and both engines not at T.O. power and
flaps at 1, 2, 3 or FULL
or
2. L/G not downlocked and flaps at 3 or FULL and
both radio altimeters failed

When the actual deceleration is 80 % of the selected rate

When the Auto Brake is working

At Touchdown