When you jack the MLG with two rear tires are deflated and two forward tires are inflated

Replace them before you lift the forward axles

You can lift the forward axles as normal

Put the JACK - WHEEL CHANGE, MAIN/NOSE LANDING GEAR in position on the side where the tires are deflated until the adapter touches the ball pad of the bogie

Towing can be carried out using

Tow bar or towbarless tractor at NLG.

Tow bar or towbarless tractor at MLG(s)

If the passenger/crew doors are fully open and locked and/or the cargo doors are open in the

You can tow the aircraft with certain limited speed

You are not allow to tow the aircraft

You can tow the aircraft with certain limited wind speed

You can tow an aircraft which has deflated tires in these conditions on the NLG

Not more than one deflated tire

Tow the aircraft with a towbar only

You can tow an aircraft which has deflated tires in these conditions on the MLG

Not more than one deflated tire on the same axle

Not more than three deflated tires on both MLGs

When you replace the wheel and tire assembly which has a deflated tire after towing

You must also replace the adjacent wheel and tire assembly on the same axle

You can replace the wheel and tire only

You must also replace the adjacent wheel and tire assembly on the same MLG

When you do pressure Refuel with Automatic Control from the Integrated Refuel Panel

You can enter the Preselected Fuel Quantity (PFQ) through the Flight Management System (FMS).

You cannot enter the Preselected Fuel Quantity (PFQ) through the Flight Management System (FMS).

You can enter the Preselected Fuel Quantity (PFQ) through the Flight Management System (FMS)

During pressure refuel, the maximum refuel pressure is limited to 3.4 BAR(50 PSI)

To prevent from causing damage to the aircraft fuel system

To limit the fuel flow into the tank

To prevent from closing the refuel isolation valve by FQMS

You can use air for the servicing of the tires

Yes, if the oxygen in the tires is not more than 5% of volume

Yes, if maintenance personnel remove the air from the tire(s) and inflate the tire(s) with dry nitrogen

AIRBUS recommends that when you inflate the tires, you use the maximum normal pressure

This is necessary to keep tire inflation to a minimum

This is necessary to keep tire will not be worn on the shoulder

This is necessary to keep tire inflation to a maximum

Procedure when you filling of the Pneumatic Starter

Fill the engine oil at a rate of 4 strokes per minute for up to 9 strokes. Then fill at a rate of 1 stroke per minute until the engine oil starts to spill from the overfill port

Fill the engine oil at a rate of 4 strokes per minute until the oil starts to spill from the overfill port

Fill the engine oil at a rate of 9 stroke per minute until the oil starts to spill from the overfill port

In General case, Wire P/N Identification:

Standard P/N + Wire type code + Wire gauge.

Standard P/N + Code letter for number of cores + Wire gauge

Standard P/N + Wire gauge + Insulation color code

Continuity Test of an Aircraft Wire, you can do Continuity test:

With aircraft wire connected to a grounding point Or with an extension wire.

With aircraft wire connected to a grounding point

What is operation you should not do in storm condition?

Refuel/ defuel operation and use headset to communicate with flight deck from ground connection

Use headset to communicate with flight deck from ground connection

The Trim Air Valve can be manually Positioned and locked

Yes, can be manually positioned and locked 3 positions(Closed, LO, HI Pos)

Yes, Locked 2 positions(Closed, Opened)

Yes, Locked 2 Positions(Closed, LO Position)

For Filling SCS which purpose of the Interconnection Cable to connect between Ground Service Panel and Ground Service Equipment

Set the SCS from Standby to Servicing Mode

Supply Electrical power for SCS

Supply Electrical Power for Ground Service Equipment

Which purpose of nitrogen supply to SCS Ground Service Equipment when filling SCS(

Using nitrogen pressure to push SCS coolant in hose return to Ground Service EquipmentTank

Supply nitrogen for Accumulator of SCS

Using nitrogen Pressure to pressurized filling system

On the overhead reset panel, when you pull PACK1 (2) Reset Pushbutton this mean reset which

ASCU1(2) and relate ACS application in CPIOM

For quickly control Pack Outlet Temperature, which component main control by ACSU

RAM Air inlet Door Actuator and Ram Air Outlet Door Actuator

Temp Control Valve and Pack Discharge Heating-Valve

Which purpose of the Pack Discharge Heating Valve

Minimum humid and also decrease ice build up

Add more hot air for increase temperature of pack outlet

Stop supply from pack when pack overheat

For control temperature of pack outlet, which component using by ACSU to get lowest temp

Water extractor temperature-sensor and pack discharge temperature-sensor.

Pack discharge Temperature sensor and compressor pack discharge sensor

Main Heat exchangerOutlet Temp Sensor and Pack Discharge

Which component take important data for ACSU control pack outlet temperature

Water Extractor Temperature-Sensor

Pack discharge temperature Sensor

Compressor Discharge Temperature-Sensor

In flight if packs overheat

Pack auto shutdown for prevent damaged component

What is the Function of Supplemental Cooling System (SCS)

Maintains at low temperature the air in the trolleys of the galleys

Maintains and cooling pack bay compartment

In normal operation the Avionics Ventilation System (AVS) uses?

The cargo air to ventilate the avionic equipments

The cooled fresh air from mixer to ventilate the avionic equipments

The cooled re-circulated air to ventilate the avionic equipments

When the DITCHING P/B SW set ON, which component will be close

FCV, RAI door, avionic overboard valve, OFV

FCV, avionic overboard valve, avinonic inboard valve

RAI door, Out Flow control Valve,

The Emergency Ram Air Inlet (ERAI) door is controlled open

Automatically in case of failure of both Packs and the aircraft in emergency descent configuration

Manually by pushing the RAM AIR P/B SW and the A/C altitude is less than 10000 feet .

How does the overboard valve of the Avionic Ventilation System operate

On ground the overboard valve is in fully open position

In flight configuration, the overboard is in the closed position

What is true regarding the operation of the Overpressure Relief Valve

It includes a Positive Pressure Relief and also a Negative Pressure Relief feature

It has a Positive Pressure Relief feature only.

It has a Negative Pressure Relief feature only

What is the Function of premixer unit?

Prevent ice accretion, decreesa noise

Prevent over-pressure in mixer unit

In avionic ventilation system. If one extraction fan Inop

Both overboard valve and inboard valve fully open

Overboard valve open and inboard valve fully close

Which is menthod control temperature in cabin and cockpit

Supply hot air to distribution duct

The ASCUs (Air Systems Control Units) installed in:

The air conditioning compartment.

Relate to ASCU? Which answers follow is correct

ASCU is dual Channel controller, one channel in active mode, one in standby mode

In case of the AP is engaged

The Side Stick Unit (SSU) and the rudder pedals are locked

Only the Side Stick Unit (SSU) is locked

Only the rudder pedals is locked

In case of ATHR engaged but not active

The cockpit crews control the thrust through the throttle control levers

The thrust of engine limit at idle position

The Auto Flight System (AFS) calculates orders to automatically control the

Flight controls and the engines

The Primary Flight Display and the Navigation Display

To select, change and monitor the F-PLN. The flight crew used:

The KCCUs (Keyboard and cursor control units) and the MFDs (Multi-Function Displays),

The KCCUs (Keyboard and cursor control units) and the FCU (Flight Control Unit),

The KCCUs (Keyboard and cursor control units) and the NDs (Navigation Displays).

1-150

Authored by Thu NguyenHongMinh

English

University

Used 17+ times

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MULTIPLE CHOICE QUESTION

30 sec • 1 pt

The fuselage station number shows the distance of a cross section from X=0 is measured in:

Inch

Centimeter

Millimeter

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Access doors and panels are identified by:

Four-character code (3 digits of its zone and 1 letters)

Five-character code (3 digits of its zone and 2 letters)

Five-character code (2 letters and 3 digits of its zone)

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

There are how many major zones in the aircraft

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Aircraft Maintenance Configuration before you Lift the aircraft

Remove the wheel chocks if they are in position, set the parking brake control switch to the OFF

Install the wheel chocks, set the parking brake control switch to OFF.

Remove the wheel chocks if they are in position, set the parking brake control switch to ON.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

When you jack aircraft for wheel change

Loading/unloading or fueling operation are not allowed

You can do loading/unloading or fueling operation

You can only do fueling operation, loading/unloading is not allowed

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

To prepare aircraft for lifting, before installing the jack pads you need

Open 3 access panels and install jack pads

Open 01 access panel for NLG jack pad only

Open 02 access panels for MLG jack pads only

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How many jack do you need to jack the aircraft:

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1-150

The fuselage station number shows the distance of a cross section from X=0 is measured in:

Access doors and panels are identified by:

There are how many major zones in the aircraft

Aircraft Maintenance Configuration before you Lift the aircraft

When you jack aircraft for wheel change

To prepare aircraft for lifting, before installing the jack pads you need

How many jack do you need to jack the aircraft:

When you jack the MLG with two rear tires are deflated and two forward tires are inflated

Towing can be carried out using

Before you tow the aircraft make sure that dimension H of the NLG is not more than.

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