Cruise Emergencies

Question 1

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

Answer 1

55 degrees within 5 seconds, 3 seconds, 3 seconds

Question 2

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

Answer 2

Right alt pressure system

Question 3

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

Answer 3

2

Question 4

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

Answer 4

5

Question 5

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

Answer 5

150 KIAS, aft emergency hatch

Question 6

Ditching should be accomplished with the landing gear____

Answer 6

Retracted

Question 7

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

Answer 7

Into the wind, whitecaps

Question 8

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

Answer 8

Stalled in, structural damage

Question 9

Night ditching should be made with the assistance of

Answer 9

Instruments

Question 10

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

Answer 10

10

Question 11

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

Answer 11

65 seconds

Question 12

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

Answer 12

Right aft escape hatch

Question 13

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

Answer 13

Radio altimeter

Question 14

Installation of emergency hatches is hazardous above ___ KIAS

Answer 14

150

Question 15

____ may have to be used by crew fighting fires

Answer 15

Portable oxygen bottles

Question 16

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

Answer 16

Pilot or copilot, CALL

Question 17

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

Answer 17

100% oxygen

Question 18

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

Answer 18

Oxygen duration, emergency descent

Question 19

The _____ hand held fire extinguisher should be held ____

Answer 19

Halon 1211, upright

Question 20

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

Answer 20

Go on 100% oxygen, initiate a descent

Question 21

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

Answer 21

Full control deflection

Question 22

Controllability check should be accomplished above ___ ft

Answer 22

10K

Question 23

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

Answer 23

Engine separation

Question 24

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

Answer 24

Try and push the boom back in

Question 25

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

Answer 25

Manual trim wheel

Question 26

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

Answer 26

Overstressing the vertical fin

Question 27

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

Answer 27

Fuel valves

Question 28

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

Answer 28

Engine fire/failure during flight

Question 29

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

Answer 29

BTB

Question 30

If a CB trips ___ times do not attempt to reset

Answer 30

3

Question 31

Prior to checking or changing fuses be sure to ___

Answer 31

Turn off the affected equipment

Question 32

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

Answer 32

30 seconds, allow fuel drainage from the nacelle

Question 33

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

Answer 33

15%, hung start

Question 34

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

Answer 34

Rudder, disengaging

Question 35

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

Answer 35

Circuit open, gen breaker switch

Question 36

If oil pressure fluctuates below ___ psi then __ the engine

Answer 36

11psi, shut down

Question 37

Bearing failure may occur as quickly as ___ after oil starvation

Answer 37

30 seconds

Question 38

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

Answer 38

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

Question 39

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

Answer 39

Inboard, raise the speed brakes

Question 40

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

Answer 40

Sets stab tim to CUTOFF

Question 41

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

Answer 41

Bleedown occurs, yaw damper/EFAS disengages

Question 42

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

Answer 42

Rupture of return lines or unwanted pressurization

Question 43

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

Answer 43

Electrical or manual

Question 44

Indications of possible fuel leakage include (6 things)

Answer 44

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

Question 45

Discontinue emergency tank emptying procedures before the fuel quantity reaches

Answer 45

0

Question 46

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

Answer 46

Reduce airspeed and flap movement

Question 47

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

Answer 47

A/R, OFF, OFF

Question 48

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 ____

Answer 48

Set the affected pump supply switch to CLOSED

Question 49

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

Answer 49

Set the affected pump supply switch to CLOSED

Question 50

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

Answer 50

Immediately depressurize the affected system

Question 51

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

Answer 51

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

Question 52

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

Answer 52

Read the reserve brake gauge

Question 53

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

Answer 53

Pressure can be built up and maintained in the affected system

Question 54

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

Answer 54

Fluid quantity gages, return the crossover valve to NORMAL

Question 55

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

Answer 55

Right system, injury to operator

Question 56

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

Answer 56

The engine bleed valves, damage to the aircraft

Question 57

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

Answer 57

Increase and off

Question 58

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

Answer 58

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

Question 59

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

Answer 59

Pitch up

Question 60

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 ____

Answer 60

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

Question 61

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

Answer 61

2 inches

Question 62

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

Answer 62

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

Question 63

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

Answer 63

Reduced for all rudder deflections, overcontrol

Question 64

Boldface for SMOKE/FUME ELIMINATION

Answer 64

OXYGEN – ON/100% (ALL)