QRH. Flashcards

1
Q

On the ground, after an aborted engine start?

A

Aborted Engine start NNC

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2
Q

Airspeed or Mach indications are suspected

to be unreliable?

A

Airspeed Unreliable NNC

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3
Q

Fire is detected in the APU

A

APU fire NNC

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4
Q

•A cabin altitude exceedance

•In flight, the intermittent cabin
altitude/configuration warning horn
sounds or a CABIN ALTITUDE light illuminates

A

CABIN ALTITUD WARNING or RADIP DEPRESSURIZATION NNC

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5
Q
  • Cabin altitude cannot be controlled

* A rapid descent is needed

A

EMERCENCY DESCENT NNC

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6
Q

•Engine fire warning

•Airframe vibrations with abnormal engine
indications

•Engine separation.

A

ENGINE FIRE or Engine Severe Damage or

Separation NNC

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7
Q

•Engine indications are abnormal

•Engine indications are rapidly approaching
or exceeding limits

•Abnormal engine noises are heard,
possibly with airframe vibration

•There is no response to thrust lever
movement or the response is abnormal

•Flames in the engine inlet or exhaust are
reported.

A

Engine Limit or Surge or Stall NNC

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8
Q

An overheat is detected in the engine

A

ENGINE OVERHEAT NNC

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9
Q

An engine tailpipe fire occurs on the ground

with no engine fire warning

A

ENGINE TAILPIPE FIRE

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10
Q

Evacuation is needed

A

EVACUATION CHECKLIST

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11
Q

In flight, the steady warning horn sounds

A

LANDING CONFIGURATION NNC

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12
Q

On the ground, the intermittent cabin
altitude/configuration warning horn sounds
or a TAKEOFF CONFIG light illuminates when advancing the
thrust levers to takeoff thrust.

A

TAKEOFF CONFIGURATION NNC

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13
Q
  • Both engines have a loss of thrust

* Both ENG FAIL alerts show.

A

Loss Of Thrust On Both Engines NNC

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14
Q

Uncommanded stabilizer trim movement

occurs continuously.

A

RUNAWAY STABILIZER NNC

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15
Q

Smoke, fire or fumes occur

A

Smoke, fire or fumes occur NNC

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16
Q

“FAULT” LIGHT ILLUMINATE (IRS)

•An IRS fault occurs

•On the ground, if the ALIGN light is also
illuminated, the present position entry is
possibly incorrect.

A

IRS FAULT NNC

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17
Q

Flameout recognition?

A

We have:

*N1 and N2 and OIL QUANTITY

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18
Q

Engine severe damage recognition?

A

We have 0 of:

*N1 and/or N2 and/or OIL QUANTITY

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19
Q

Which checklist should we call for in case of an engine flameout?

A

ENGINE FAILURE OR SHUTDOWN NNC

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20
Q

“ALTN” LIGHT ILLUMINATE (EEC)

An EEC operates in the alternate control
mode

A

EEC ALTERNATE MODE NNC

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21
Q
  • An engine failure
  • An ENG FAIL alert shows
  • An engine flameout

•Another checklist directs an engine
shutdown.

A

Engine Failure or Shutdown NNC

22
Q

The vibration level is 4.0 units or greater.

Airframe vibration may or may not be felt

A

ENGINE HIGH VIBRATION NNC

23
Q

The engine oil temperature is high

A

ENGINE HIGH OIL TEMPERATURE NNC

24
Q

An engine start is needed and all of the
following are true:

  • There was no engine fire
  • There is N1 rotation
  • There is no abnormal airframe vibration
A

ENGINE IN-FLIGHT START NNC

25
"LOW OIL PRESS" LIGHT ILLUMINATE The engine oil pressure is low.
ENGINE LOW OIL PRESSURE NNC
26
The equipment cooling supply or exhaust fan is failed. "OFF" LIGHT ILLUMINATE
EQUIPMENT COOLING OFF NNC
27
Fire is detected in the related cargo | compartment
CARGO FIRE NNC
28
Fire is detected in the main wheel well
WHEEL WELL FIRE NNC
29
Hydraulic system pressure to the ailerons, elevators and rudder is low "LOW PRESSURE" LIGHT ILLUMINATE
FLIGHT CONTROL LOW PRESSURE NNC
30
"FMC p/rst" LIGHT ILLUMINATE Display of VTK followed by MAP failure flags on one or both navigation displays.
FMC FAIL NNC
31
An engine fuel leak is suspected for the reasons listed in the Additional Information section of this checklist.
FUEL ENGINE LEAK NNC
32
The landing gear position disagrees with the LANDING GEAR lever position. Any "gear" red light illuminate
GEAR DISAGREE NNC
33
Both "GEN OFF BUS", both "SOURCE OFF", both "TRANSFER BUS" illuminate. Both engine driven generators are off.
LOSS OF BOTH ENGINE DRIVEN | GENERATORS NNC
34
The hydraulic pump temperature is high.
HYDRAULIC PUMP OVERHEAT NNC
35
The IAS DISAGREE alert indicates the captain’s and first officer’s airspeed indications disagree
IAS DISAGREE NNC
36
•Amber or red weather radar returns below the airplane •Appearance of liquid water on the windshield at temperatures too cold for rain (the sound is different than rain) •The autothrottle is unable to maintain the selected airspeed •TAT indication stays near 0°C
ICE CRYSTAL ICING
37
A flight control is jammed or restricted in | roll, pitch, or yaw
Jammed or Restricted | Flight Controls NNC
38
The LANDING GEAR lever will not move from | the UP position.
Landing Gear Lever Jammed | in the Up Position NNC
39
The LANDING GEAR lever cannot be moved to the UP position due to one of the following: •Failure of the landing gear lever lock solenoid •Failure of the air/ground system •Failure of the ground spoiler interlock valve to close.
Landing Gear Lever Will Not | Move Up After Takeoff NNC
40
Hydraulic system A pressure is low
LOSS OF SYSTEM A NNC
41
Hydraulic system A and B pressures are low
MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B NNC
42
Landing must be made with one engine | inoperative
One Engine Inoperative Landing NNC
43
All landing gear are not down and locked | after attempting manual gear extension
Partial or All Gear Up Landing NNC
44
* An uncommanded roll occurs when the flaps change position | * The left and right flap indications disagree.
Trailing Edge Flap Asymmetry NNC
45
The trailing edge flaps are not in the commanded position.
Trailing Edge Flap Disagree NNC
46
A display in the common display system is failed.
Display Failure NNC
47
A forward flight deck window has one or more of these: * An electrical arc * A delamination * A crack * Is shattered.
Window Damage NNC
48
The leading edge devices fail to extend and trailing edge flaps are less than 1.
All Flaps Up Landing NNC
49
The brake accumulator has no nitrogen precharge
Brake Pressure Indicator Zero PSI NNC
50
Flight deck or passenger cabin temperature is excessively hot. The temperature can cause incapacitation.
Cabin Temperature Hot NNC
51
An elevator tab vibration occurs in flight. One or more of the following may be an indication of an elevator tab vibration: •Vibration that originates, and is strongest, in the aft part of the airplane but can be felt throughout the airplane •Vibration that is felt in the control wheel and rudder pedals •Vibration that causes items attached to the airplane, such as sun visors, to move.
Elevator Tab Vibration NNC
52
Loss of electric trim through the main electric stabilizer trim switches, or as directed by the STAB OUT OF TRIM checklist.
Stabilizer Trim Inoperative NNC