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Flybondi Lineas Aereas > QRH. > Flashcards

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
Q

“LOW OIL PRESS” LIGHT ILLUMINATE

The engine oil pressure is low.

A

ENGINE LOW OIL PRESSURE NNC

26
Q

The equipment cooling supply or exhaust fan
is failed.

“OFF” LIGHT ILLUMINATE

A

EQUIPMENT COOLING OFF NNC

27
Q

Fire is detected in the related cargo

compartment

A

CARGO FIRE NNC

28
Q

Fire is detected in the main wheel well

A

WHEEL WELL FIRE NNC

29
Q

Hydraulic system pressure to the ailerons,
elevators and rudder is low

“LOW PRESSURE” LIGHT ILLUMINATE

A

FLIGHT CONTROL LOW PRESSURE NNC

30
Q

“FMC p/rst” LIGHT ILLUMINATE

Display of VTK followed by MAP failure flags
on one or both navigation displays.

A

FMC FAIL NNC

31
Q

An engine fuel leak is suspected for the
reasons listed in the Additional Information
section of this checklist.

A

FUEL ENGINE LEAK NNC

32
Q

The landing gear position disagrees with the
LANDING GEAR lever position.

Any “gear” red light illuminate

A

GEAR DISAGREE NNC

33
Q

Both “GEN OFF BUS”, both “SOURCE OFF”, both “TRANSFER BUS” illuminate.

Both engine driven generators are off.

A

LOSS OF BOTH ENGINE DRIVEN

GENERATORS NNC

34
Q

The hydraulic pump temperature is high.

A

HYDRAULIC PUMP OVERHEAT NNC

35
Q

The IAS DISAGREE alert indicates the
captain’s and first officer’s airspeed
indications disagree

A

IAS DISAGREE NNC

36
Q

•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

A

ICE CRYSTAL ICING

37
Q

A flight control is jammed or restricted in

roll, pitch, or yaw

A

Jammed or Restricted

Flight Controls NNC

38
Q

The LANDING GEAR lever will not move from

the UP position.

A

Landing Gear Lever Jammed

in the Up Position NNC

39
Q

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.

A

Landing Gear Lever Will Not

Move Up After Takeoff NNC

40
Q

Hydraulic system A pressure is low

A

LOSS OF SYSTEM A NNC

41
Q

Hydraulic system A and B pressures are low

A

MANUAL REVERSION or LOSS OF SYSTEM A AND SYSTEM B NNC

42
Q

Landing must be made with one engine

inoperative

A

One Engine Inoperative Landing NNC

43
Q

All landing gear are not down and locked

after attempting manual gear extension

A

Partial or All Gear Up Landing NNC

44
Q
  • An uncommanded roll occurs when the flaps change position

* The left and right flap indications disagree.

A

Trailing Edge Flap Asymmetry NNC

45
Q

The trailing edge flaps are not in the commanded position.

A

Trailing Edge Flap Disagree NNC

46
Q

A display in the common display system is failed.

A

Display Failure NNC

47
Q

A forward flight deck window has one or more of these:

  • An electrical arc
  • A delamination
  • A crack
  • Is shattered.
A

Window Damage NNC

48
Q

The leading edge devices fail to extend and trailing edge flaps are less than 1.

A

All Flaps Up Landing NNC

49
Q

The brake accumulator has no nitrogen precharge

A

Brake Pressure Indicator Zero PSI NNC

50
Q

Flight deck or passenger cabin temperature is excessively hot. The temperature can cause incapacitation.

A

Cabin Temperature Hot NNC

51
Q

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.

A

Elevator Tab Vibration NNC

52
Q

Loss of electric trim through the main electric stabilizer trim switches, or as directed by the STAB OUT OF TRIM checklist.

A

Stabilizer Trim Inoperative NNC

Flybondi Lineas Aereas (16 decks)

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