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Flashcards > EICAS / NNC Checklist Conditions > Flashcards

EICAS / NNC Checklist Conditions Flashcards

To assess general knowledge of the meaning of EICAS warnings, cautions and advisories.

1
Q

AUTO UNLOCK

A

Condition:

The correct emergency access code is entered.

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2
Q

CREW OXYGEN LOW

A

Condition:

Crew oxygen pressure is low.

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3
Q

[ ] DOOR AFT CARGO

A

Condition:

The aft lower cargo door is not closed and secure.

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4
Q

[ ] DOOR BULK CARGO

A

Condition:

The bulk cargo door is not closed and secure.

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5
Q

[ ] DOOR E/E ACCESS

A

Condition:

The E/E access door is not closed and secure.

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6
Q

[ ] DOOR ENTRY 1–5L, R

A

Condition:

An entry door is not closed and secure.

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7
Q

[ ] DOOR FWD ACCESS

A

Condition:

The forward access door is not closed and secure.

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8
Q

[ ] DOOR FWD CARGO

A

Condition:

The forward lower cargo door is not closed and secure.

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9
Q

DOOR WING SLIDE L, R

A

Condition:

The door for the unpressurized wing slide compartment is not closed and secure.

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10
Q

DOORS

A

Condition:

Two or more doors are not closed and secure.

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11
Q

ELT ON

A

Condition:

The emergency locator transmitter is on.

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12
Q

EMER LIGHTS

A

Condition:

One of these occurs:

  • The emergency lights are on
  • The emergency lights switch is not ARMED
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13
Q

Lock Fail

Unannunciated Checklist

A

Condition:

One or more of these occur:

  • The flight deck access system switch is OFF
  • The lock is failed
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14
Q

PASS OXYGEN ON

A

Condition:

The passenger oxygen system is on.

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15
Q

[ ] WINDOW FLT DECK L, R

A

Condition:

The side window is not closed and secure.

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16
Q

[ ] WINDOWS

A

Condition:

The left and right side windows are not closed and secure.

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17
Q

[ ] CABIN ALTITUDE

A

Condition:

Cabin altitude is excessive.

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18
Q

BLEED ISLN CLOSED C, L, R

A

Condition:

One of the following occurs:

  • The isolation valve is failed closed
  • The bleed isolation switch is off
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19
Q

BLEED ISLN OPEN C, L, R

A

Condition:

The isolation valve is failed open.

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20
Q

[ ] BLEED LEAK BODY

A

Condition:

A bleed air leak occurs in the body area.

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21
Q

[ ] BLEED LEAK L, R

A

Condition:

A bleed air leak occurs in the wing or pack bay area.

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22
Q

[ ] BLEED LEAK STRUT L, R

A

Condition:

A bleed air leak or starter duct leak occurs in the strut area.

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23
Q

[ ] BLEED LOSS BODY

A

Condition:

Bleed air from the left and right body ducts is not available.

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24
Q

[ ] BLEED LOSS BODY L

A

Condition:

Bleed air from the left body duct is not available.

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25
Q

[ ] BLEED LOSS BODY R

A

Condition:

Bleed air from the right body duct is not available.

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26
Q

[ ] BLEED LOSS WING L, R

A

Condition:

Bleed air from the wing duct is not available.

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27
Q

BLEED OFF APU

A

Condition:

One of the following occurs:

  • The APU bleed valve is closed because of a system fault
  • The APU bleed switch is off
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28
Q

BLEED OFF ENG L, R

A

Condition:

One of the following occurs:

  • The engine bleed valve is closed because of a system fault
  • The engine bleed switch is off
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29
Q

[ ] CABIN ALTITUDE AUTO

A

Condition:

One of these occurs:

  • Automatic pressurization control is failed
  • Both outflow valve switches are in manual
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30
Q

CARGO HEAT AFT

A

Condition:

One of these occurs:

  • Aft lower cargo heat is inoperative
  • The aft cargo temperature selector is OFF
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31
Q

CARGO HEAT BULK

A

Condition:

One of these occurs:

  • Bulk cargo heat is inoperative
  • The bulk cargo temperature selector is OFF
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32
Q

EQUIP COOLING

A

Condition:

The forward equipment cooling system is failed.

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33
Q

[ ] EQUIP COOLING OVRD

A

Condition:

The equipment cooling system is in override mode.

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34
Q

[ ] LANDING ALTITUDE

A

Condition:

One of these occurs:

  • The FMC does not supply a landing altitude
  • The landing altitude selector is pulled
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35
Q

[ ] OUTFLOW VALVE AFT, FWD

A

Condition:

One of these occurs:

  • Automatic control of the outflow valve is inoperative
  • The outflow valve switch is in manual
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36
Q

[ ] PACK L

A

Condition:

The left pack is inoperative.

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37
Q

[ ] PACK R

A

Condition:

The right pack is inoperative.

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38
Q

[ ] PACK L+R

A

Condition:

Both packs are inoperative.

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39
Q

[ ] PACK MODE L, R

A

Condition:

The pack is in the standby mode.

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40
Q

[ ] TRIM AIR L, R

A

Condition:

The trim air valve is closed.

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41
Q

[ ] ANTI–ICE ENG L, R

A

Condition:

The engine anti–ice valve is closed when commanded open.

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42
Q

[ ] ANTI–ICE LEAK ENG L, R

A

Condition:

A bleed air leak occurs in the engine anti-ice duct.

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43
Q

ANTI–ICE LOSS ENG L, R

A

Condition:

Anti–ice bleed air for the engine is not available.

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44
Q

[ ] ANTI–ICE ON

A

Condition:

All of these occur:

  • An anti-ice selector is ON
  • TAT is more than 10 degrees C
  • Ice is not detected
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45
Q

[ ] ANTI–ICE WING

A

Condition:

One or both wing anti–ice valves are failed closed.

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46
Q

[ ] HEAT PITOT C

A

Condition:

The center pitot probe heat is failed.

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47
Q

[ ] HEAT PITOT L

A

Condition:

The left pitot probe heat is failed.

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48
Q

[ ] HEAT PITOT R

A

Condition:

The right pitot probe heat is failed.

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49
Q

[ ] HEAT PITOT L+C+R

A

Condition:

The left, center and right pitot probe heat are failed.

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50
Q

Ice Crystal Icing

Unannunciated Checklist

A

Condition:

Engine ice crystal icing or TAT probe icing is suspected. Ice crystal icing conditions exist when in visible moisture, and one or more of the following indications are present:

  • 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 disconnects or is unable to maintain the selected airspeed
  • TAT indication on EICAS stays near 0 degrees C
  • Abnormal engine vibration indications

(Additional items that can indicate ice crystal icing are listed in the Additional Information section.)

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51
Q

[ ] ICE DETECTORS

A

Condition:

The ice detectors are failed.

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52
Q

ICING ENG

A

Condition:

Ice is detected and an engine anti-ice selector is OFF.

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53
Q

ICING WING

A

Condition:

Ice is detected and one of these occurs:

  • The wing anti-ice selector is OFF
  • The wing anti-ice takeoff inhibit is active
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54
Q

WINDOW HEAT

A

Condition:

Two or more window heats are off.

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55
Q

[ ] WINDOW HEAT L, R FWD

A

Condition:

Primary window heat for the forward window is inoperative.

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56
Q

[ ] WINDOW HEAT L, R SIDE

A

Condition:

Window heat for the side window is inoperative.

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57
Q

AUTOPILOT

A

Condition:

One or more of these occur:

  • The autopilot is in a degraded mode other than the selected mode
  • The engaged roll mode is failed
  • The engaged pitch mode is failed
  • The autopilot is in flight envelope protection
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58
Q

AUTOPILOT DISC

A

Condition:

All autopilots are disengaged.

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59
Q

AUTOTHROTTLE DISC

A

Condition:

Both autothrottles are disconnected.

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60
Q

[ ] AUTOTHROTTLE L, R

A

Condition:

One autothrottle is inoperative.

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61
Q

NO AUTOLAND

A

Condition:

The autoland system is not available.

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62
Q

NO LAND 3

A

Condition:

The autoland system does not have redundancy for a triple channel autoland.

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63
Q

DATALINK LOST

A

Condition:

The ACARS datalink is temporarily lost.

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64
Q

DATALINK SYS

A

Condition:

The datalink system is failed.

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65
Q

[ ] RADIO TRANSMIT

A

Condition:

A microphone switch is on and causes a radio to transmit for 30 seconds or more.

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66
Q

SATCOM

A

Condition:

The SATCOM system is failed.

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67
Q

SATCOM DATALINK

A

Condition:

The SATCOM datalink is failed.

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68
Q

SATCOM VOICE

A

Condition:

SATCOM voice communication is failed.

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69
Q

SATVOICE LOST

A

Condition:

SATCOM voice communication is temporarily lost.

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70
Q

VHF DATALINK

A

Condition:

The VHF datalink is failed.

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71
Q

[ ] ELEC AC BUS L, R

A

Condition:

The AC bus is not energized.

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72
Q

[ ] ELEC BACKUP GEN L, R

A

Condition:

The backup generator is failed.

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73
Q

[ ] ELEC BACKUP SYS

A

Condition:

The backup power system is failed.

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74
Q

ELEC BATTERY OFF

A

Condition:

The battery switch is OFF.

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75
Q

ELEC BUS ISLN L, R

A

Condition:

The bus tie breaker is open.

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76
Q

ELEC CABIN/UTIL OFF

A

Condition:

The cabin/utility power switch is OFF.

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77
Q

[ ] ELEC GEN DRIVE L, R

A

Condition:

A generator drive fault occurs.

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78
Q

[ ] ELEC GEN OFF APU

A

Condition:

The generator control breaker is open.

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79
Q

[ ] ELEC GEN OFF L, R

A

Condition:

The generator control breaker is open.

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80
Q

ELEC GND HDLG BUS

A

Condition:

A fault occurs in the ground handling bus.

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81
Q

ELEC IFE/SEATS OFF

A

Condition:

The IFE/passenger seats power switch is OFF.

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82
Q

ELEC STANDBY SYS

A

Condition:

A standby power system failure occurs.

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83
Q

[ ] MAIN BATTERY DISCH

A

Condition:

One of these occurs:

  • The main battery is discharging
  • The hot battery bus is not energized
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84
Q

Aborted Engine Start L, R

Unannunciated Checklist

A

Condition:

On the ground, an aborted engine start is needed.

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85
Q

Dual Eng Fail/Stall

Unannunciated Checklist

A

Condition:

Engine speed for both engines is below idle.

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86
Q

[ ] ENG AUTOSTART L, R

A

Condition:

During a ground start, one of these occurs:

  • Autostart did not start the engine
  • Fuel control switch is in RUN at low engine RPM with the autostart switch OFF
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87
Q

Eng Lim/Surge/Stall L, R

Unannunciated Checklist

A

Condition:

One or more of these occur:

  • Engine indications are abnormal
  • Engine indications are quickly nearing or show an exceedance
  • 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
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88
Q

Eng Svr Damage/Sep L, R

Unannunciated Checklist

A

Condition:

One or more of these occur:
- Airframe vibrations with abnormal engine indications
Engine separation

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89
Q

[ ] APU LIMIT

A

Condition:

An APU limit exceedance occurs.

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90
Q

[ ] APU SHUTDOWN

A

Condition:

An APU automatic shutdown occurs.

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91
Q

ENG AUTOSTART OFF

A

Condition:

The engine autostart switch is OFF.

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92
Q

ENG CONTROL L, R

A

Condition:

An EEC system fault occurs.

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93
Q

[ ] ENG EEC MODE L, R

A

Condition:

An EEC is in the alternate control mode.

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94
Q

[ ] ENG FAIL L, R

A

Condition:

Engine speed is below idle.

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95
Q

[ ] ENG FUEL FILTER L, R

A

Condition:

Fuel contamination can cause fuel to bypass the engine fuel filter.

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96
Q

[ ] ENG FUEL VALVE L, R

A

Condition:

One or more of these occur:

  • The engine fuel valve is not in the commanded position
  • The fuel spar valve is not in the commanded position
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97
Q

ENG IDLE DISAGREE

A

Condition:

One engine is at approach idle and the other engine is at minimum idle.

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98
Q

Eng In-Flight Start L, R

Unannunciated Checklist

A

Condition:

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

  • There is N1 rotation
  • There was no engine fire
  • There is no abnormal airframe vibration
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99
Q

[ ] ENG LIMIT PROT L, R

A

Condition:

The EEC is in the alternate mode and the commanded N1 exceeds the limit.

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100
Q

[ ] ENG OIL FILTER L, R

A

Condition:

Oil filter contamination has caused oil to bypass the oil filter.

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101
Q

[ ] ENG OIL PRESS L, R

A

Condition:

The engine oil pressure is low.

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102
Q

[ ] ENG OIL TEMP L, R

A

Condition:

The engine oil temperature is high.

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103
Q

[ ] ENG REV LIMITED L, R

A

Condition:

The engine reverser operation is limited.

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104
Q

ENG REVERSER L, R

A

Condition:

A fault occurs in the thrust reverser system.

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105
Q

ENG RPM LIMITED L, R

A

Condition:

Engine thrust is at the N1 or N2 red line limit.

106
Q

ENG SHUTDOWN

A

Condition:

Both engines were shut down by the fuel control switches or the engine fire switches.

107
Q

ENG SHUTDOWN L, R

A

Condition:

The engine was shut down by the fuel control switch or the engine fire switch.

108
Q

[ ] ENG START VALVE L, R

A

Condition:

The start valve is not in the commanded position.

109
Q

[ ] ENG STARTER CUTOUT L, R

A

Condition:

One of these occurs:

  • The start valve fails to close
  • The start selector stays in start
110
Q

ENG THRUST L, R

A

Condition:

The engine thrust is less than the commanded thrust.

111
Q

Volcanic Ash

Unannunciated Checklist

A

Condition:

Volcanic ash is suspected when one or more of these occur:

  • A static discharge around the windshield
  • A bright glow in the engine inlets
  • Smoke or dust on the flight deck
  • An acrid odor
112
Q

[ ] FIRE APU

A

Condition:

Fire is detected in the APU.

113
Q

[ ] FIRE ENG L, R

A

Condition:

Fire is detected in the engine.

114
Q

Fire Eng Tailpipe L, R

Unannunciated Checklist

A

Condition:

An engine tailpipe fire occurs on the ground with no engine fire warning.

115
Q

Smoke, Fire or Fumes

Unannunciated Checklist

A

Condition:

Smoke, fire or fumes occurs.

116
Q

BOTTLE 1, 2 DISCH ENG

A

Condition:

The engine fire extinguisher bottle pressure is low.

117
Q

BOTTLE DISCH APU

A

Condition:

The APU fire extinguisher bottle pressure is low.

118
Q

BOTTLE DISCH CARGO

A

Condition:

Both rapid discharge cargo fire extinguisher bottle pressures are low.

119
Q

[ ] DET FIRE APU

A

Condition:

APU fire detection is failed.

120
Q

DET FIRE CARGO AFT, FWD

A

Condition:

Lower cargo compartment smoke detection is failed.

121
Q

DET FIRE ENG L, R

A

Condition:

Engine fire and overheat detection is failed.

122
Q

[ ] FIRE CARGO AFT

A

Condition:

Smoke is detected in the aft lower cargo compartment.

123
Q

[ ] FIRE CARGO FWD

A

Condition:

Smoke is detected in the forward lower cargo compartment.

124
Q

[ ] FIRE WHEEL WELL

A

Condition:

Fire is detected in a main wheel well.

125
Q

[ ] OVERHEAT ENG L, R

A

Condition:

An overheat is detected in the engine.

126
Q

[ ] SMOKE COMPT UPR DR 2

A

Condition:

Smoke is detected in a compartment.

127
Q

SMOKE LAVATORY

A

Condition:

Smoke is detected in one or more lavatories.

128
Q

[ ] SMOKE LAV/COMPT

A

Condition:

Smoke is detected in one or more lavatories, or other enclosed area.

129
Q

[ ] SMOKE REST UPR DR 4

A

Condition:

Smoke is detected in the crew rest area.

130
Q

[ ] SMOKE REST UPR DR 5

A

Condition:

Smoke is detected in the crew rest area.

131
Q

Smoke or Fumes Removal

Unannunciated Checklist

A

Condition:

Smoke or fumes removal is needed.

132
Q

[ ] STABILIZER

A

Condition:

One of these occurs:

  • Stabilizer movement without a signal to trim
  • The stabilizer is failed
133
Q

[ ] AUTO SPEEDBRAKE

A

Condition:

An automatic speedbrake fault occurs.

134
Q

[ ] FLAPS DRIVE

A

Condition:

The flap drive mechanism is failed.

135
Q

[ ] FLAPS PRIMARY FAIL

A

Condition:

The flaps primary mode is failed.

136
Q

[ ] FLAP/SLAT CONTROL

A

Condition:

The flap/slat electronics units are failed.

137
Q

[ ] FLIGHT CONTROL MODE

A

Condition:

The flight control system is in the secondary mode.

138
Q

[ ] FLIGHT CONTROLS

A

Condition:

One or more of these occur:

  • Two or more flight control surfaces are inoperative
  • Other faults in the flight control system are detected
139
Q

FLT CONTROL VALVE

A

Condition:

One or more of these occur:

  • One or more flight control shutoff valves are failed closed
  • One or more flight control shutoff switches are in shutoff
140
Q

Jammed Flight Controls

Unannunciated Checklist

A

Condition:

Flight controls are jammed or restricted in roll, pitch, or yaw.

141
Q

[ ] PITCH DOWN AUTHORITY

A

Condition:

Pitch down authority is restricted.

142
Q

[ ] PITCH UP AUTHORITY

A

Condition:

Pitch up and flare authority are restricted.

143
Q

[ ] PRI FLIGHT COMPUTERS

A

Condition:

The flight control system is operating in the direct mode.

144
Q

[ ] SLATS DRIVE

A

Condition:

The slat drive mechanism is failed.

145
Q

[ ] SLATS PRIMARY FAIL

A

Condition:

The slats primary mode is failed.

146
Q

SPEEDBRAKE EXTENDED

A

Condition:

The speedbrakes are extended and one or more of these occur:

  • The radio altitude is between 15 and 800 feet
  • The flap lever is in a landing setting
  • A thrust lever is not at idle
147
Q

[ ] SPOILERS

A

Condition:

One or more spoiler pairs are failed.

148
Q

[ ] STAB GREENBAND

A

Condition:

The nose gear pressure sensor disagrees with the computed stabilizer greenband and all doors are closed.

149
Q

[ ] STABILIZER C

A

Condition:

The center stabilizer control path is failed.

150
Q

STABILIZER CUTOUT

A

Condition:

Both stabilizer cutout switches are in CUTOUT.

151
Q

[ ] STABILIZER R

A

Condition:

The right stabilizer control path is failed.

152
Q

[ ] THRUST ASYM COMP

A

Condition:

Thrust asymmetry compensation is failed or off.

153
Q

Airspeed Unreliable

Unannunciated Checklist

A

Condition:
Airspeed or Mach indications are suspected to be unreliable. (Items which can indicate unreliable airspeed are listed in the Additional Information section.)

154
Q

[ ] ALTN ATTITUDE

A

Condition:

Both pilots’ AIR DATA/ATT source switches are in ALTN.

155
Q

BARO SET DISAGREE

A

Condition:

The captain’s and first officer’s barometric settings disagree.

156
Q

[ ] CHKL INCOMPLETE NORM

A

Condition:

A normal checklist needs to be completed.

157
Q

[ ] CHKL NON-NORMAL

A

Condition:

There is a hidden non-normal checklist. All of these occur:

  • A non-normal checklist is not complete
  • The ECL is not displayed
  • The related EICAS message is not shown
158
Q

DISPLAY SELECT PNL

A

Condition:

Left, center, or right CDU control of the display select panel is used.

159
Q

[ ] EFIS CONTROL PNL L, R

A

Condition:

One of these occurs:

  • The EFIS control panel is failed
  • CDU control of the EFIS is used
160
Q

SGL SOURCE AIR DATA

A

Condition:

Both PFDs use the same air data source.

161
Q

[ ] SGL SOURCE DISPLAYS

A

Condition:

Some or all display units use a single source of display data.

162
Q

[ ] SGL SOURCE RAD ALT

A

Condition:

Both PFDs use the same radio altimeter source.

163
Q

SINGLE SOURCE F/D

A

Condition:

Both PFDs use the same flight director source.

164
Q

ADS-B Failure

Unannunciated Checklist

A

Condition:

One or more of these occur:

  • ATC reports ADS-B is lost or degraded
  • On the CDU POS REF 3/3 page, the GPS L line is blank and the left transponder is selected
  • On the CDU POS REF 3/3 page, the GPS R line is blank and the right transponder is selected
165
Q

[ ] ADS-B OUT L

A

Condition:

Position data is not available to the left transponder.

166
Q

[ ] ADS-B OUT R

A

Condition:

Position data is not available to the right transponder.

167
Q

[ ] AIR DATA SYS

A

Condition:

The three air data sources disagree.

168
Q

[ ] FMC

A

Condition:

One of these occurs:

  • The FMC selector is in L and the left FMC is failed
  • The FMC selector is in R and the right FMC is failed
  • Both FMCs are failed
169
Q

FMC L, R

A

Condition:

An FMC is failed.

170
Q

FMC MESSAGE

A

Condition:

An alerting message is in the FMC scratchpad.

171
Q

[ ] GPS

A

Condition:

Both GPS receivers are failed.

172
Q

[ ] GPS L

A

Condition:

The left GPS receiver is failed.

173
Q

[ ] GPS R

A

Condition:

The right GPS receiver is failed.

174
Q

[ ] ILS ANTENNA

A

Condition:

Two or more ILS receivers do not use the correct antenna.

175
Q

[ ] INSUFFICIENT FUEL

A

Condition:

FMC estimated fuel at the destination is less than the entered RESERVES fuel.

176
Q

[ ] NAV ADIRU INERTIAL

A

Condition:

The ADIRU cannot supply correct attitude, position, heading, track, and groundspeed data.

177
Q

[ ] NAV UNABLE RNP

A

Condition:

The actual navigational performance is not sufficient.

178
Q

SINGLE SOURCE ILS

A

Condition:

Both pilots’ displays use the same ILS source.

179
Q

TRANSPONDER L, R

A

Condition:

A transponder fault occurs.

180
Q

[ ] VNAV STEP CLIMB

A

Condition:

A FMC-predicted or manually-entered VNAV step climb point has sequenced and a climb has not started.

181
Q

[ ] FUEL AUTO JETTISON

A

Condition:

One of these occurs:

  • The total fuel quantity is less than or equal to the fuel to remain and a jettison nozzle valve is open
  • The fuel jettison automatic shutoff is failed
182
Q

[ ] FUEL CROSSFEED AFT

A

Condition:

The aft fuel crossfeed valve is not in the commanded position.

183
Q

[ ] FUEL CROSSFEED FWD

A

Condition:

The forward fuel crossfeed valve is not in the commanded position.

184
Q

[ ] FUEL DISAGREE

A

Condition:

The totalizer fuel quantity and the FMC calculated fuel quantity disagree.

185
Q

[ ] FUEL FLOW ENG L, R

A

Condition:

Engine fuel flow is abnormally high.

186
Q

[ ] FUEL IMBALANCE

A

Condition:

There is a fuel imbalance between the main tanks.

187
Q

FUEL IN CENTER

A

Condition:

The center tank fuel quantity is at the level where the pump switches must be ON.

188
Q

FUEL JETT NOZZLE L, R

A

Condition:

A jettison nozzle valve is not in the commanded position.

189
Q

Fuel Jettison

Unannunciated Checklist

A

Condition:

Fuel jettison is needed.

190
Q

[ ] FUEL JETTISON MAIN

A

Condition:

The main tank fuel jettison system is failed.

191
Q

[ ] FUEL JETTISON SYS

A

Condition:

The fuel jettison system is failed.

192
Q

Fuel Leak

Unannunciated Checklist

A

Condition:

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

193
Q

FUEL LOW CENTER

A

Condition:

The center tank fuel quantity is at the level where the pump switches must be off.

194
Q

[ ] FUEL PRESS ENG L, R

A

Condition:

The affected engine is on suction feed.

195
Q

FUEL PRESS ENG L+R

A

Condition:

Fuel pressure to both engines is low on the ground with the engines shut down.

196
Q

[ ] FUEL PUMP CENTER L, R

A

Condition:

The center fuel pump pressure is low.

197
Q

[ ] FUEL PUMP L AFT, FWD

A

Condition:

The left fuel pump pressure is low.

198
Q

[ ] FUEL PUMP R AFT, FWD

A

Condition:

The right fuel pump pressure is low.

199
Q

[ ] FUEL QTY LOW

A

Condition:

The fuel quantity is low in a main tank.

200
Q

[ ] FUEL SCAVENGE SYS

A

Condition:

The fuel scavenge system is failed.

201
Q

[ ] FUEL TEMP LOW

A

Condition:

Fuel temperature is near the minimum.

202
Q

[ ] FUEL VALVE APU

A

Condition:

The APU fuel valve is not in the commanded position.

203
Q

[ ] HYD AUTO CONTROL C

A

Condition:

Both of the following occur:

  • Automatic control of both center demand pumps fails
  • System indications fail
204
Q

[ ] HYD AUTO CONTROL L, R

A

Condition:

Both of the following occur:

  • Automatic control of demand pump fails
  • System indications fail
205
Q

[ ] HYD OVERHEAT DEM C1, C2, L, R

A

Condition:

The pump temperature is high.

206
Q

[ ] HYD OVERHEAT PRI C1, C2

A

Condition:

The pump temperature is high.

207
Q

[ ] HYD OVERHEAT PRI L, R

A

Condition:

The pump temperature is high.

208
Q

[ ] HYD PRESS DEM C1, C2, L, R

A

Condition:

The demand pump output pressure is low when commanded on.

209
Q

[ ] HYD PRESS PRI C1, C2

A

Condition:

The pump pressure is low.

210
Q

[ ] HYD PRESS PRI L

A

Condition:

The left primary pump pressure is low.

211
Q

[ ] HYD PRESS PRI R

A

Condition:

The right primary pump pressure is low.

212
Q

[ ] HYD PRESS SYS C

A

Condition:

The center hydraulic system pressure is low.

213
Q

[ ] HYD PRESS SYS L

A

Condition:

The left hydraulic system pressure is low.

214
Q

[ ] HYD PRESS SYS L+C

A

Condition:

The left and center hydraulic system pressures are low.

215
Q

HYD PRESS SYS L+C+R

A

Condition:

All hydraulic system pressures are low.

216
Q

[ ] HYD PRESS SYS L+R

A

Condition:

The left and right hydraulic system pressures are low.

217
Q

[ ] HYD PRESS SYS R

A

Condition:

The right hydraulic system pressure is low.

218
Q

[ ] HYD PRESS SYS R+C

A

Condition:

The right and center hydraulic system pressures are low.

219
Q

[ ] HYD QTY LOW C

A

Condition:

The center hydraulic quantity is low.

220
Q

HYD QTY LOW L, R

A

Condition:

The hydraulic quantity is low.

221
Q

[ ] HYD QTY LOW L+C

A

Condition:

The left and center hydraulic quantities are low.

222
Q

[ ] HYD QTY LOW L+C+R

A

Condition:

All three hydraulic quantities are low.

223
Q

[ ] HYD QTY LOW L+R

A

Condition:

The left and right hydraulic quantities are low.

224
Q

[ ] HYD QTY LOW R+C

A

Condition:

The right and center hydraulic quantities are low.

225
Q

RAT UNLOCKED

A

Condition:

The ram air turbine is not stowed and locked.

226
Q

[ ] ANTISKID

A

Condition:

An antiskid system fault occurs.

227
Q

AUTOBRAKE

A

Condition:

One of these occurs:

  • The autobrake system is disarmed
  • The autobrake system is failed
228
Q

[ ] BRAKE SOURCE

A

Condition:

Normal and alternate brake system pressures are low, and reserve hydraulic source for alternate brake system is low.

229
Q

[ ] BRAKE TEMP

A

Condition:

One or more brake temperatures are high.

230
Q

[ ] GEAR DISAGREE

A

Condition:

The gear position disagrees with the landing gear lever position.

231
Q

[ ] GEAR DOOR

A

Condition:

One or more gear doors are not closed.

232
Q

Gear Lever Locked Down

Unannunciated Checklist

A

Condition:

The landing gear lever cannot move to UP.

233
Q

[ ] MAIN GEAR BRACE L, R

A

Condition:

The main gear is down with one brace unlocked.

234
Q

MAIN GEAR STEERING

A

Condition:

Main gear steering does not lock.

235
Q

[ ] RESERVE BRAKES/STRG

A

Condition:

One or more of these are possibly not available:

  • Alternate brakes from the reserve hydraulic source
  • Normal nose gear extension
  • Nose wheel steering
236
Q

TAIL SKID

A

Condition:

The tailskid is not in the commanded position.

237
Q

[ ] TIRE PRESS

A

Condition:

One or more tire pressures are not normal.

238
Q

AIRSPEED LOW

A

Condition:

Airspeed is less than minimum maneuvering speed.

239
Q

ALTITUDE ALERT

A

Condition:

A deviation from the MCP set altitude occurs.

240
Q

ALTITUDE CALLOUTS

A

Condition:

Altitude and minimums voice callouts during approach are not available.

241
Q

CONFIG DOORS

A

Condition:

An entry, forward cargo, or aft cargo door is not closed and latched and locked during takeoff.

242
Q

CONFIG FLAPS

A

Condition:

The flaps are not in a takeoff position during takeoff.

243
Q

CONFIG GEAR

A

Condition:

A landing gear is not down and locked and one of these occurs:

  • Below 800 feet radio altitude and a thrust lever is at or near idle
  • The flaps are in a landing position
244
Q

CONFIG GEAR STEERING

A

Condition:

Main gear steering is not locked during takeoff.

245
Q

CONFIG PARKING BRAKE

A

Condition:

The parking brake is set during takeoff.

246
Q

CONFIG RUDDER

A

Condition:

Rudder trim is not centered during takeoff.

247
Q

CONFIG SPOILERS

A

Condition:

One of these occurs:

  • The speedbrake lever is not down during takeoff
  • The speedbrake lever is extended beyond ARMED in flight with climb thrust or greater
248
Q

CONFIG STABILIZER

A

Condition:

The stabilizer is not in the greenband during takeoff.

249
Q

[ ] CONFIG WARNING SYS

A

Condition:

A configuration warning system fault occurs.

250
Q

[ ] GND PROX SYS

A

Condition:

A ground proximity warning system fault occurs.

251
Q

OVERSPEED

A

Condition:

Airspeed is more than Vmo/Mmo.

252
Q

PILOT RESPONSE

A

Condition:

Pilot action is not detected during a specified time.

253
Q

[ ] TAIL STRIKE

A

Condition:

The tail hits the runway.

254
Q

Tail Strike

Unannunciated Checklist

A

Condition:

A tail strike is suspected or confirmed.

255
Q

TCAS

A

Condition:

TCAS is failed.

256
Q

TCAS OFF

A

Condition:

TCAS modes TA or TA/RA are not selected.

257
Q

TCAS RA CAPTAIN, F/O

A

Condition:

TCAS cannot show RA guidance on the PFD.

258
Q

TERR OVRD

A

Condition:

The ground proximity terrain override switch is in OVRD.

259
Q

[ ] TERR POS

A

Condition:

Terrain position data is lost.

260
Q

[ ] WINDSHEAR SYS

A

Condition:

A windshear system fault occurs.

Flashcards (6 decks)

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