CBT B

cbt-b

Exit

Question 1 of 1

Time Left

211200

999

block

The Fuel Temperature Indicator reads the temperature of the fuel in

Select the correct answer(s).

(0/0)

211201

999

none

Hydraulic system A power sources are

Select the correct answer(s).

(0/0)

211202

999

none

The standby hydraulic pump is automatically activated on the loss of system A or B hydraulic pressure

Select the correct answer(s).

(0/0)

211203

999

none

A leak in the system B hydraulic will also reduce the quantity in the B system

Select the correct answer(s).

(0/0)

211204

999

none

The standby system low quantity light is

Select the correct answer(s).

(0/0)

211205

999

none

With any control cabin window heating inoperative, speed should be restricted to

Select the correct answer(s).

(0/0)

211206

999

none

During a flight in icing conditions with wing anti-icing selected to ON

Select the correct answer(s).

(0/0)

211207

999

none

If the engine anti-ice switch is selected ON and a cowl valve failed in the closed position then the COWL VALVE OPEN light

Select the correct answer(s).

(0/0)

211208

999

none

The HYD Brake Pressure indicator reads zero but both hydraulic system pressures are normal

Select the correct answer(s).

(0/0)

211209

999

none

Rudder pedal steering is

Select the correct answer(s).

(0/0)

211210

999

none

When the autobrake RTO mode is selected on the ground

Select the correct answer(s).

(0/0)

211211

999

none

After manual extension of the landing gear, the indication on the flight deck that the correct procedure has been carried out is

Select the correct answer(s).

(0/0)

211212

999

none

The nose wheel steering lockout pin

Select the correct answer(s).

(0/0)

211213

999

none

To define the origin airport on the FMC Route page

Select the correct answer(s).

(0/0)

211214

999

none

CBT B

Question 1 of 1

Time Left

The Fuel Temperature Indicator reads the temperature of the fuel in

Select the correct answer(s).

(0/0)

Hydraulic system A power sources are

Select the correct answer(s).

(0/0)

The standby hydraulic pump is automatically activated on the loss of system A or B hydraulic pressure

Select the correct answer(s).

(0/0)

A leak in the system B hydraulic will also reduce the quantity in the B system

Select the correct answer(s).

(0/0)

The standby system low quantity light is

Select the correct answer(s).

(0/0)

With any control cabin window heating inoperative, speed should be restricted to

Select the correct answer(s).

(0/0)

During a flight in icing conditions with wing anti-icing selected to ON

Select the correct answer(s).

(0/0)

If the engine anti-ice switch is selected ON and a cowl valve failed in the closed position then the COWL VALVE OPEN light

Select the correct answer(s).

(0/0)

The HYD Brake Pressure indicator reads zero but both hydraulic system pressures are normal

Select the correct answer(s).

(0/0)

Rudder pedal steering is

Select the correct answer(s).

(0/0)

When the autobrake RTO mode is selected on the ground

Select the correct answer(s).

(0/0)

After manual extension of the landing gear, the indication on the flight deck that the correct procedure has been carried out is

Select the correct answer(s).

(0/0)

The nose wheel steering lockout pin

Select the correct answer(s).

(0/0)

To define the origin airport on the FMC Route page

Select the correct answer(s).

(0/0)

The FMC CRZ page displays a TURB N1 value which is a reference display of the N1% for turbulance penetration and it

Select the correct answer(s).

(0/0)

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