What is the significance of the circuit breakers on the overhead panel?

They may be operational in the Emergency Electrical Configuration.

What cockpit lighting is available during an emergency electrical situation?

Right side Dome light, main panel flood lights (left two columns only), and the standby compass light.

Which flight control computer will be inoperative with gear extension while in the Emergency Electrical Configuration?
FAC1

The BAT FAULT light will illuminate when:

Charging current increases at an abnormal rate

The emergency generator supplies power as long as:

L/G is UP.

The RAT is connected directly (mechanically) to the Emergency Generator

FALSE

The BATTERY BUS is normally powered by:

DC bus 1 through a DC tie control relay.

On the cockpit overhead panel, there is a three position EMERGENCY EXIT Light switch. What lights are associated with
this switch?
Exit signs, emergency lights, and escape path lighting.

While operating on Emergency Electrical Power with the landing gear lowered which of the following statements is
correct
On the ground at 100 knots, the DC BATTERY BUS automatically reconnects to the batteries allowing APU start.

While operating on Emergency Electrical Power (EMER GEN powering the system, FAC #1 reset) which of the following
control laws are in effect?
ALTERNATE

Which condition will automatically illuminate the escape lights

DC ESS BUS not powered.

While operating on Emergency Electrical Power (EMER GEN powering the system) what should the crew accomplish
prior to lowering the landing gear
Depress the guarded RMP NAV push button and tune the appropriate NAV facility and course for the approach to be
accomplished.

Which busses will be powered after the RAT is extended and the EMER GEN begins producing power?
BATT HOT busses, ESS DC, ESS DC SHED, ESS AC and ESS AC SHED.

Trim air valves are controlled by:

The zone controller.

Aft cargo ventilation is controlled by:

The cargo ventilation controller.

How many outflow valves are there?

One valve with two doors
In case of zone controller primary and secondary channel failure, what temperatures are maintained by pack one and
pack two?
Hot air and trim air valves close and packs deliver air at a fixed temperature (20 deg.C pack 1 and 10 deg.pack2
Cond. Zone regulator fault (primary channel failed):
Cabin zone is at fixed temperature

If a pack controller fails (primary and secondary channel failure), the pack outlet air temperature is controlled by:
ANTI ICE VALVE

During landing run, Ram Air Inlet flaps open when speed is less than
70 kts (after 20 seconds delay)

The temperature of the air that exits the compressor section is displayed above the Pack Flow. It normally displays
green, but displays amber for temperatures over:
230

The trim air valves are _____ controlled by the zone controller
ELECTRICALLY

Nose wheel steering is available when:

Nose gear doors closed

Hand wheel and pedals are operated simultaneously

BSCU transforms these orders into nose wheel steering angle (signals are mathematically added)

Following failure of all 3 ADIRS, is antiskid available?

Yes

How many thrust lever positions are there, and how are they labeled?
There are 6 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE, REV IDLE and MREV.

How do you arm the A/THR in flight?

A/THR switch ON when throttles are not in the engagement mode.

What are the two basic modes of the A/THR system

Variable thrust and fixed speed

During a manual start, how is the start valve opened?

By depressing the ENG MAN START pushbutton‟s on the overhead panel while the ENG MODE selector is out of the
NORM position.

Does the FADEC provide EGT limit protection constantly?

No, EGT limit protection is only available during ground auto starts.

What would happen in flight if the FADEC‟s alternator failed?

The FADEC would now be powered using ship‟s power

You are in the middle of a manual engine start. What are you looking for when you select ENG MASTER 2 ON
The fuel used is reset, both igniters are powered and fuel flow is indicated

During an automatic start, the FADEC controls:

The start valves, igniters, HP and LP fuel valves, and fuel flow
Which steps of a manual start are being taken care of by the FADEC?
Starter valve closure and ignition cut off

APU fire detection is accomplished by:

Two parallel fire detection loops.

The aft cargo compartment smoke detection system consists of:

Four smoke detectors and a two channel smoke detection control unit

In the event a lavatory smoke detector detects smoke

warnings will be generated in the cockpit and in the cabin.

DISCH light on either the engine or APU fire agent switches indicates:
The extinguisher bottle has been discharged

The AFT SMOKE light closes the aft cargo inlet and outlet isolation valves and shuts off the aft cargo extraction fan
TRUE

The APU BLEED FAULT light illuminates amber for an APU:

Bleed leak.

The overheat detection system uses a single loop for

PYLON AND APU

The AUTO position of the X BLEED selector opens the crossbleed if

The APU bleed valve is open.

The X BLEED selector is selected to OPEN or to SHUT

Cooled in a heat exchanger by cooling air bleed from Fan section

An amber flashing IR FAULT light indicates that:

Attitude and heading information may be recovered in ATT mode.

The white IR ALIGN light is flashing. What does this mean?

No present position has been entered and ten minutes has elapsed since the IR was selected ON. An
alignment fault may exist.

What does the LOW ACCURACY message mean?

FMGC position & actual radio position difference exceeds limits.

What information is supplied by the Air Data Modules (ADMs) and displayed on the PFD‟s?
Airspeed, altitude, and backup vertical speed.

If the IR mode rotary selector is selected OFF:

The ADIRU is not energized: AD and IR information is lost.

The DDRMI provides the pilot with:

Bearing only for VOR 1 and VOR 2

The ON BAT light will illuminate amber:

When one or more IR’s are operating on aircraft battery power.
While in flight operating in Normal law, movement of the sidestick and subsequent return to neutral will
command
A load factor proportional to stick deflection, then maintain one G flight corrected for pitch attitude

ADIRU 1 is supplying information to PFD 1, ND 1 and the DDRMI; ADIRU 2 is supplying power to PFD 2 and ND
2.

Which situation will automatically illuminate the escape path lighting?

The loss of power to the DC ESS SHED bus and The loss of power to the AC bus #1

With the EMER EXIT LT selector in the ARM position, if AC bus #1 is unpowered:
The emergency lights and exit signs will illuminate automatically.