Landing Emergencies Flashcards

1
Q

During an EGPWS warning, (PULL UP!) do not change ___ or ___ until the plane is out of the warning condition and stabilized

A

Flaps or gear configuration

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2
Q

Adequate rudder is available to maintain directional control during patter, approach and landing if what 3 conditions for directional control are satisfied?

A

Speed, thrust setting and control inputs

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3
Q

For 3 engine operation, if the charted go-around N1 setting for the asymmetric/outboard engine is not exceeded, Vmca will be ____ than touchdown speed

A

Less than or equal to

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4
Q

At high gross weights consider flying a ___ final approach

A

Extended

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5
Q

To minimize trim changes with thrust adjustments use ____ to the max extent possible

A

Symmetric throttles

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6
Q

in a 3 engine approach, if the decision is made to go around advance __ engines to ____ then ___ if needed

A

Symmetric, charged go-around setting, asymmetric not to exceed max asymmetric thrust setting

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7
Q

If landing with one engine and powered rudder inoperative fly downwind and base legs with ___ flaps at minimum at a speed of ___

A

20 degrees, Vref+30

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8
Q

Remove __ trim prior to landing

A

Rudder

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9
Q

Time permitting, a gross weight that achieves a climb gradient of ___ % or greater is recommended

A

28%

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10
Q

Avoid excessive sideslip by maximum use of ___

A

Rudder

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11
Q

If landing with 2 engines out on the same side, once airspeed is below ____ go-around capability cannot be assured.

A

Approach speed

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12
Q

With 2 engines and powered rudder inoperative, ____ should be primary consideration of landing base with ___ conditions preferred

A

Weather conditions, VMC

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13
Q

With 2 engines and powered rudder inoperative, reduce gross weight to ____. Don’t lower flaps beyond ____

A

Minimum practical, 20 degrees

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14
Q

If full rudder will be required, ensure seat is ___

A

Full vertical

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15
Q

For two engine operation, if thrust setting doesn’t exceed charted go-around N1, Vmca should be ___ to approach speed

A

Less than or equal to

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16
Q

When landing with jammed stabilizer and differential flap configuration, use the patter, approach and threshold speed for ____. If leading edge flaps are not extended add__

A

Minimum flap setting, 6 knots to approach and threshold

17
Q

When landing with less than 20 degrees of flaps, approach and threshold speeds should not be less than ____

A

0 degree

18
Q

If landing with partial aileron control, a minimum approach and threshold speed of __ should be maintained

A

150 KIAS

19
Q

For landing with less than 2,800 psi of rudder pressure, apply performance data for ___

A

Rudder power inoperative

20
Q

If leading edge flaps fail to extend then add ____ to ______ speeds

A

6 knots to approach and threshold

21
Q

With all spoilers inoperative, extend main flaps to at least ___ to assure full ___ below ___ KIAS

A

23 degrees, outboard aileron, 250 KIAS

22
Q

If an ______ tire is flat and weight is above ___ then avoid turns in that direction

A

Aft outboard, 250,000

23
Q

When landing with a gear failure, ___ should be dumped prior to landing

A

Excess fuel

24
Q

If doing a gear up landing, before jettisoning, ____ flaps and reduce airspeed to ___

A

Lower full flaps, slowest practical

25
Q

Do not follow ___ during recovery from inadvertent windshear

A

Command bars

26
Q

If moderate icing conditions are encountered, do not retract flaps to less than ___

A

20 degrees