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EP Exam > Cruise Emergencies > Flashcards

Cruise Emergencies Flashcards

1
Q

Autopilot malfunction can result in bank angles of ____ degrees within ___ seconds even if recovery is initiated within ___ seconds. Pitch up malfunction can cause stall within ___ seconds

A

55 degrees within 5 seconds, 3 seconds, 3 seconds

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2
Q

Do not operate the AC system with the _______ system in full INCREASE for extended period of time

A

Right alt pressure system

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3
Q

Main boost pumps should not be run dry as catastrophic failure can occur within ___ minutes

A

2

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4
Q

Center wing override pumps should not be run dry for more than ____ minutes

A

5

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5
Q

While opening emergency hatches during flight, reduce airspeed to ___ or less. If opening all hatches then __ should be opened first

A

150 KIAS, aft emergency hatch

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6
Q

Ditching should be accomplished with the landing gear____

A

Retracted

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7
Q

While ditching and wind speed greater than 30 knots ditching should be made _____ the wind which will be indicated by extensive_____

A

Into the wind, whitecaps

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8
Q

When ditching the airplane shouldn’t be ______ as ____ and leaks may occur

A

Stalled in, structural damage

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9
Q

Night ditching should be made with the assistance of

A

Instruments

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10
Q

When ditching the flare should be made as to level off approx. _____ feet above the crest of the swell

A

10

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11
Q

At an approach speed of 160 knots it takes ____ seconds for the flaps to reach 20 degrees with windmilling engines

A

65 seconds

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12
Q

During ditching it is recommended that no one be positioned aft of ____

A

Right aft escape hatch

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13
Q

During ditching ___ may be used to determine altitude below 2,5000 ft

A

Radio altimeter

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14
Q

Installation of emergency hatches is hazardous above ___ KIAS

A

150

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15
Q

____ may have to be used by crew fighting fires

A

Portable oxygen bottles

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16
Q

___ or ___ will inform the crew of fuselage fire on the ___ position of the interphone

A

Pilot or copilot, CALL

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17
Q

In case of fire, breathing ____ may help provide respiratory protection

A

100% oxygen

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18
Q

If passengers are aboard and ____ is an issue, then consider ___

A

Oxygen duration, emergency descent

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19
Q

The _____ hand held fire extinguisher should be held ____

A

Halon 1211, upright

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20
Q

If rapid decompression occurs the pilot with direct crew to ____ and initiate ___

A

Go on 100% oxygen, initiate a descent

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21
Q

During controllability check don’t allow speed to decrease to where ___ is required

A

Full control deflection

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22
Q

Controllability check should be accomplished above ___ ft

A

10K

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23
Q

Large amplitude dutch roll oscillations coupled with incorrect inputs may result in

A

Engine separation

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24
Q

To prevent further damage to the boom in case of retraction mechanism failure, the receiver pilot will not try to ___

A

Try and push the boom back in

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25
Q

If electrical stab trim doesn’t work then check operation of ___

A

Manual trim wheel

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26
Q

Sudden reversal of rudder direction at high rudder deflections can result it ____

A

Overstressing the vertical fin

27
Q

If the emergency requires the shutting down of electrical systems be sure to set ____ to the desired position before shutdown

A

Fuel valves

28
Q

If the IDG fails to disconnect the affected engine should be shut down using ___ checklist

A

Engine fire/failure during flight

29
Q

Tripping the GCB switch with the corresponding BTB CIRCUIT OPEN light on causes loss of power until ____ closes

A

BTB

30
Q

If a CB trips ___ times do not attempt to reset

A

3

31
Q

Prior to checking or changing fuses be sure to ___

A

Turn off the affected equipment

32
Q

If an engine start is attempted and not completed, observe a ____ waiting period before trying again. This is to ______

A

30 seconds, allow fuel drainage from the nacelle

33
Q

Do not attempt and airstart without starter assist if N2 is below _____% or __ may occur

A

15%, hung start

34
Q

After an engine failure, the __ _may be trimmed without ___ the autopilot or yaw damper

A

Rudder, disengaging

35
Q

When shutting down the engine, make sure the generator breaker _____ caution light illuminates and trip the ___ to disengage the exciter field of the IDG

A

Circuit open, gen breaker switch

36
Q

If oil pressure fluctuates below ___ psi then __ the engine

A

11psi, shut down

37
Q

Bearing failure may occur as quickly as ___ after oil starvation

A

30 seconds

38
Q

If nose down stab trim failure is encountered during an approach then ____

A

Go around and next approach should be made using manual flight procedures

39
Q

For nose-up trim using the spoilers then set ___ to cut-off and ___

A

Inboard, raise the speed brakes

40
Q

. If runaway stab trim occurs prior to S1 then the pnf ____

A

Sets stab tim to CUTOFF

41
Q

When rudder power switch is turned off, check that the pressure (3 things)

A

Bleedown occurs, yaw damper/EFAS disengages

42
Q

Slow or rough movement of crossover valve could result in (2 things)

A

Rupture of return lines or unwanted pressurization

43
Q

Broken/jammed drive chain in forward stab trim mechanism can prevent __ or ___ trimming

A

Electrical or manual

44
Q

Indications of possible fuel leakage include (6 things)

A

Excessive fuel flowInadequate fuel flowFuel low pressure warning indicationsFuel quantity rapidly decreasingFuel line leakage in strut/nacelle areaBody tank fuel quantity increasing

45
Q

Discontinue emergency tank emptying procedures before the fuel quantity reaches

A

0

46
Q

If main tank leak is suspected it is imperative to __ and ___ to reduce further damage

A

Reduce airspeed and flap movement

47
Q

To prevent excessive fuel px surges at completeion of fuel dumping, set __ pump to ___ prior to setting fuel dump switch to ____.

A

A/R, OFF, OFF

48
Q

If a hydraulic pump inop light illuminates with no indications of fluid loss and remains on after L/R hydraulic system is depressurized and repressurized then ____

A

Set the affected pump supply switch to CLOSED

49
Q

. If a hydraulic pump inop light illuminates with indications of fluid loss then

A

Set the affected pump supply switch to CLOSED

50
Q

If a loss of hydraulic quantity occurs with no other indications then ____

A

Immediately depressurize the affected system

51
Q

If a loss of hydraulic quantity occurs with no other indications and depressurizing doesn’t fix it then ____

A

Close the supply switch for the affected pump (inboard/outboard)

52
Q

Another way to check the actual system pressure of the L hydraulic system is ___

A

Read the reserve brake gauge

53
Q

It is safe to use the crossover valve after loss of fluid provided ____ can occur with the appropriate hydraulic pressure and aux pump switches ON

A

Pressure can be built up and maintained in the affected system

54
Q

If source of hydraulic leakage cannot be determined, monitor ___ during and after use of crossover valve. If fluid loss in unaffected system occurs, then _____

A

Fluid quantity gages, return the crossover valve to NORMAL

55
Q

Application of hydraulic pressure to ____ system during manual extension can result in ____

A

Right system, injury to operator

56
Q

Failure to close ____ on malfunctioning side of manifold could result in ___ due to escaping bleed air

A

The engine bleed valves, damage to the aircraft

57
Q

Too rapid movement of cabin manual pressure knob towards the ___ position could cause harmful damage to ears

A

Increase and off

58
Q

The maximum speed for EMERGENCY gear extension, retraction or gear down is (SL, 10K, 20K, 26.5K, 28K, above 29,5K)

A

355 KIAS @ SL360 KIAS @10K368 KIAS @ 20K373 KIAS @ 26.5K361 KIAS @ 28K.9 Mach above 29.5K

59
Q

During recovery from unusual high attitude, if the landing gear is lowered then a ___ condition may result

A

Pitch up

60
Q

For unplanned penetration of severe turbulence, establish an airspeed of approximately ___ KIAS, or MACH _____ whichever is lower. Only change thrust in cases of ____. Don’t chase ___ and leave the ___ off. Ensure ___ is ON and don’t lower ____ or ____

A

280, .77 - .80, extreme airspeed variation, altitude, autopilot, yaw damper, gear and flaps

61
Q

Complete loss of airspeed indications will generally occur by the time approx. ____ inches of ice has accumulated on the nose.

A

2 inches

62
Q

Static port icing will affect ____ while pitot tube icing will affect (4 things)

A

All pitot and static instruments, IAS/TAS/MACH/Altimeter

63
Q

If Q-inlet icing occurs during powered rudder operation, rudder pedal forces may be ___ which may result in a tendency to ____

A

Reduced for all rudder deflections, overcontrol

64
Q

Boldface for SMOKE/FUME ELIMINATION

A

OXYGEN – ON/100% (ALL)

EP Exam (4 decks)

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