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Question 1 of 1

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211365

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Maximum landing weight of the B737-800 is

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211366

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The maximum speed for landing gear extension is

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211367

999

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Maximum glide slope angle for autoland is

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211368

999

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The maximum aircraft altitude for both APU bleed and electrical load is

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211369

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The maximum differential pressure is

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211370

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The maximum aircraft altitude for APU bleed only is

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211371

999

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The maximum flap extension altitude is

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211372

999

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The minimum fuel required for ground operation of the hydraulic electric pumps is

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211373

999

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Do not operate engine or wing anti-ice when the temperature is above

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211374

999

none

The maximum altitude for take-off and landing is

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211375

999

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When engine bleeds are ON, both air conditioning packs must be set to

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211376

999

none

Speedbrake should not be deployed in flight at radio altitudes less than

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211377

999

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The autopilot must not be engaged on take-off below

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211378

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none

LIM A

Question 1 of 1

Time Left

Maximum landing weight of the B737-800 is

Select the correct answer(s).

(0/0)

The maximum speed for landing gear extension is

Select the correct answer(s).

(0/0)

Maximum glide slope angle for autoland is

Select the correct answer(s).

(0/0)

The maximum aircraft altitude for both APU bleed and electrical load is

Select the correct answer(s).

(0/0)

The maximum differential pressure is

Select the correct answer(s).

(0/0)

The maximum aircraft altitude for APU bleed only is

Select the correct answer(s).

(0/0)

The maximum flap extension altitude is

Select the correct answer(s).

(0/0)

The minimum fuel required for ground operation of the hydraulic electric pumps is

Select the correct answer(s).

(0/0)

Do not operate engine or wing anti-ice when the temperature is above

Select the correct answer(s).

(0/0)

The maximum altitude for take-off and landing is

Select the correct answer(s).

(0/0)

When engine bleeds are ON, both air conditioning packs must be set to

Select the correct answer(s).

(0/0)

Speedbrake should not be deployed in flight at radio altitudes less than

Select the correct answer(s).

(0/0)

The autopilot must not be engaged on take-off below

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(0/0)

The maximum lateral fuel imbalance between wing tanks 1 and 2 must be scheduled to be zero and, for all phases of flight, must not exceed

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Engine ignition must be on for

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