Practice Exam 2

Green

Yes, if the A/SKID & N/W STRG switch is ON

Landing Gear Control Interface Unit (LGCIU) 1 only

Orders are added algebraically

6 deg

Both center tank pumps are failed, or are switched OFF

When the fuel quantity in one wing tank goes below 750 kg

Yes, if CTR TK MODE SEL is set to MAN

When any inner tank fuel reaches 750 kg

Ensures the IDG cooling

An independent air bleed from the high pressure compressor protects each engine nacelle from ice

Low on ground and normal in flight for the windshield; one level for windows

3

Yes, the wing anti icing control valves open for 30 sec only (test sequence)

The FADEC monitors the engine during a manual start and aborts the start on the ground, if the start EGT limit is exceeded before reaching 50% N2

Each FADEC has 2 channels, one of which is active and the other is on standby

Then returns to the tank or fuel pump unit

Both igniters are cut off when N2 reaches approximately 50%

Oil quantity must be at or above 9.5 qt + estimated consumption (max average estimated consumption ~ 0.5 qt/h)

10 min

The maintenance crew uses this p/b to reset the control circuit, after the system has operated

It indicates that the crew set the HI ALT LANDING p/b to ON and in this case the masks drop if the cabin pressure exceeds 16,000 feet

True

Yes

6

Silences the aural fire warning, arms the fire extinguisher squibs, closes the low pressure fuel valve, closes the hydraulic fire shut off valve, closes the engine bleed valve, closes the pack flow control valve, cuts off the FADEC power supply and deactivates the IDG

The system shuts down the APU automatically and discharges extinguishing agent

Two identical gas detection loops (A and B) mounted in parallel and a Fire Detection Unit (FDU)

By pushing the transfer key

Audio Control Panel (ACP)

On the ground when one engine is operating

Flight crew interphone

4

Each escape rope is long enough to reach the ground from any window

White

When normal aircraft electrical power fails, or when DC SHED ESS BUS is lost

Using the rotary switch located beneath the FCU

Position 1 turns on the logo lights and the first set of nav lights, position 2 turn on the logo lights and the second set of nav lights

On the forward attendant control panel

A vacuum generator produces the necessary pressure differential

3 turns clockwise

260 knots

6

Three outboard leading-edge slats of each wing and engine air intakes

The LP and HP fuel valves

N1, N2. EGT and F.F.

1 bottle that can discharge in either compartment

The remaining RMP controls all the transceivers

Flashes when one or both engines are stopped, the slides are disarmed and the cabin differential pressure is more than 2.5 Hpa

Yellow

NO SMOKING light will illuminate when either the landing gear is extended, or flaps/slats are extended (position 1, 2, 3 or FULL)