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block

The amber DUAL BLEED light is illuminated after engine start. What should the pilot do?

Select the correct answer(s).  

(0/0)

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Limit engine thrust to idle and/or place the APU BLEED air switch to OFF

Pull the engine fire handles.

Place the APU BLEED air switch to ON.

Limit engine thrust to 56% N2 while the light is illuminated.

none

The thrust reverser can be deployed:

Select the correct answer(s).  

(0/0)

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When the air/ground safety sensor is in the air mode.

During cruise when the thrust lever is at idle.

When either radio altimeter senses less than 10 feet altitude or when the air/ground safety sensor is in the ground mode.

When either radio altimeter senses less than 27 feet altitude

none

What are the indications that the engine starter has disengaged?

Select the correct answer(s).  

(0/0)

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The fuel LOW PRESSURE lights extinguish at 56% N1'.

The ENGINE START switch returns to OFF (or AUTO with automatic ignition) at 56% N2, and the START VALVE OPEN crew alert extinguishes.

The ENGINE START switch returns to OFF (or AUTO with automatic ignition) at 36% N2'.

The ENGINE START switch rotates to FLT, N1 goes to 17-20%, and N2 RPM stabilizes.

none

What position must the forward thrust levers be in before reverse thrust can be selected?

Select the correct answer(s).  

(0/0)

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Continuous thrust position.

Idle thrust position.

Any forward thrust position.

Takeoff thrust position.

none

Which APU annunciator light is not associated with an automatic shutdown of the APU?

Select the correct answer(s).  

(0/0)

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LOW OIL PRESSURE

FAULT

MAlNT

OVERSPEED

none

During normal operations, which hydraulic system powers the thrust reversers?

Select the correct answer(s).  

(0/0)

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The standby system powers both reversers.

System A powers both reversers.

System B powers both reversers.

System A powers engine No.1 reverser and system B powers engine No. 2 reverser.

none

An APU shutdown in flight occurs:

Select the correct answer(s).  

(0/0)

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With a LOW fuel alert in main tank No. 1.

Automatically by moving the battery switch to OFF.

Only by an exceedance.

When the MAINT annunciator light illuminates.

none

The APU may be used in flight as an electrical and bleed air source simultaneously up to:

Select the correct answer(s).  

(0/0)

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30,000 feet

25,000 feet

17,000 feet

10,000 feet

none

Electronic engine control abnormal start protection:

Select the correct answer(s).  

(0/0)

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Is inoperative; there is no abnormal start protection.

Is provided for EGT start limit exceedances and wet start protection both in flight and on the ground.

Is provided for EGT start limit exceedances and wet start protection on the ground only.

Requires that hydraulic system B must be pressurized prior to start.

none

If the upper DU fails:

Select the correct answer(s).  

(0/0)

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Engine indications automatically shift to the lower DU.

N1 and N2 indications are not displayed; manually select either inboard DU.

Display of all engine indications are lost.

Engine indications automatically shift to either inboard DU.

none

During a normal start, prior to placing the engine start switch to GRD, the EEC is not being powered:

Select the correct answer(s).  

(0/0)

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And only N1, N2, oil quantity, and engine vibration are available and are displayed directly from the engine sensors.

And only oil quantity and engine vibration are available.

And only digital readouts are visible for engine indications

Until the engine accelerates to a speed greater than 15% N2'.

none

What is the position of the engine BLEED air switches during the shutdown procedure?

Select the correct answer(s).  

(0/0)

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OFF

HIGH

AUTO

ON

none

When the EEC is not powered, the following indications are displayed directly from the engine sensors:

Select the correct answer(s).  

(0/0)

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Fuel flow and oil pressure.

Oil temperature, pressure, and quantity.

N1, N2, oil quantity, and engine vibration.

Oil temperature and engine vibration.

none

The EEC provides redline overspeed protection for:

Select the correct answer(s).  

(0/0)

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N1 and N2, in both the normal and alternate modes.

N2 only, in both the normal and alternate modes.

N1 and N2, in the normal mode only.

N1 only, in both the normal and alternate modes.

none

The EEC hard alternate mode thrust is:

Select the correct answer(s).  

(0/0)

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Used only for assumed temperature reduction takeoffs and go-arounds.

Always less than normal mode thrust for the same lever position.

Not approved for use.

Always equal to or greater than normal mode thrust for the same lever position.