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B737 > Condition Statements > Flashcards

Condition Statements Flashcards

1
Q

Bomb on Board

A

Condition: Bomb threat received from ground or cabin, or suspicious article is found on board.

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2
Q

Chemical / Biological or

HAZMAT / Dangerous Goods Threat

A

Condition: One of these occur

  • Hazardous material (chemical or biological threat) received from the ground or cabin
  • Dangerous goods threat
  • Reports of unknown multiple cabin illness
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3
Q

Ditching

A

Condition: Aircraft ditching and evacuation are needed

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4
Q

Precautionary Disembarkation

A

Condition: The situation requires the orderly but rapid disembarkation of the passengers and crew

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5
Q

AUTOMATIC UNLOCK

A

Condition: The correct emergency access code is entered

Objective: To deny unauthorised access to the flight before the door automatically unlocks.

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6
Q

CARGO DOOR

A

Condition: One or more cargo doors are not closed and secure

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7
Q

ELT

A

Condition: The emergency locator transmitter is on

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8
Q

EMERGENCY EXIT LIGHTS NOT ARMED

A

Condition: The emergency exit lights switch is not ARMED

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9
Q

ENTRY DOOR

A

Condition: One or more entry door are not closed and secure

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10
Q

EQUIPMENT DOOR

A

Condition: The equipment door is not closed and secure

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11
Q

LOCK FAIL

A

Condition: One or more of these occur

  • The FLIGHT DECK ACCESS SYSTEM switch is off
  • The lock failed

Objective: To remove electrical power from the lock to prevent possible overheat

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12
Q

OVERWING DOOR

A

Condition: One or more service doors are not closed and secure

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13
Q

PASSENGER OXYGEN ON

A

Condition: The passenger oxygen system is on

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14
Q

SERVICE DOOR

A

Condition: One or more of the service doors are not closed and secure

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15
Q

Window Damage - Forward

L1, L2, R1, R2

A

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

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

Objective: To remove electrical power, if needed, to prevent arcing. To reduce differential pressure and descend if the inner pane is shattered of cracked.

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16
Q

Window Damage - Unheated Side

L3, R3

A

Condition: An unheated side flight deck window has one or more of these:

  • A crack
  • Is shattered

Objective: To reduce differential pressure to 0 psi if both panes are shattered or cracked.

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17
Q

Window Noise

A

Condition: Excessive noise from a number 2 flight deck window seal.

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18
Q

Window Open

A

Condition: A side window opens during takeoff or in flight.

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19
Q

CABIN ALTITUDE WARNING
or
Rapid Depressurisation

A

Condition: One or more of these occur

  • A cabin altitude exceedance
  • In flight, the intermittent cabin altitude/configuration warning horn sounds or the CABIN ALTITUDE light (if installed and operative) illuminates.
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20
Q

AUTO FAIL
or
Unscheduled Pressurization Change

A

Condition: One or more of these occur

  • Automatic pressurization mode has failed
  • The cabin altitude is uncontrollable

Objective: To maintain control of the cabin altitude

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21
Q

BLEED TRIP OFF

A

Condition: One or more of these occur

  • An engine bleed air overheat
  • An engine bleed air overpressure
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22
Q

Cabin Temperature Hot

A

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

Objective: To regain temperature control. If unable to regain control, to descend and configure to provide alternate ventilation.

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23
Q

DUAL BLEED

A

Condition: The APU bleed valve is open and one of these occurs

  • BLEED 1 air switch is on
  • BLEED 2 air switch is on and the ISOLATION VALVE is open

Objective: To prevent possible back pressure of the APU.

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24
Q

EQUIPMENT COOLING OFF

A

Condition: The equipment cooling supply or exhaust fan is failed

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25
Q

OFF SCHEDULE DESCENT

A

Condition: A descent is started before reaching the planned cruise altitude set in the FLT ALT indicator.

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26
Q

PACK

A

Condition: One or more of these occur

  • The primary and standby pack controls are failed
  • A pack overheat.
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27
Q

WING-BODY OVERHEAT

A

Condition: An overheat from a bleed duct leak occurs

Objective: To isolate the bleed duct leek

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28
Q

ZONE TEMP

A

Condition: One or more of these occur

  • A zone duct overtemp
  • Flight deck temperature control is failed.
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29
Q

Emergency Descent

A

Condition: One or more of these occur

  • Cabin altitude cannot be controlled
  • A rapid descent is needed.
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30
Q

ENGINE COWL ANTI-ICE

A

Condition: An engine cowl anti-ice duct overpressure occurs.

Objective: To reduce cowl duct pressure by reducing thrust

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31
Q

ENGINE COWL VALVE OPEN OR TAI INDICATION

A

Condition: One or both of the following occurs

  • An engine COWL VALVE OPEN light stays illuminated bright blue
  • An amber TAI indication is shown.
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32
Q

Ice Crystal Icing

A

Condition: Engine ice crystal 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 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 selected airspeed
- TAT indication stays near 0*C
(Additional items that indicate ice crystal icing are listed in the Additional Information section)

Objective: To exit the ice crystal icing conditions and reduce the operational effects of the icing

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33
Q

PROBE HEAT

A

Condition: One or more probe heats are failed

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34
Q

WINDOW OVERHEAT

A

Condition: A window overheat occurs

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35
Q

WING ANTI-ICE VALVE OPEN

A

Condition: A wing anti-ice L VALVE OPEN or R VALVE OPEN light stays illuminated bright blue. The wing anti-ice valve is not in the commanded position.

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36
Q

AUTOPILOT DISENGAGE

A

Condition: All autopilots are disengaged. The red light flashes and the aural tone sounds.

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37
Q

AUTOTHROTTLE DISENGAGE

A

Condition: The autothrottle is disengaged. The red light flashes.

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38
Q

ACARS Electrical Power Loss

A

Condition: The ACARS AC power is lost.

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39
Q

ACARS MU Fail or DU Fail

A

Condition: The ACARS system is failed.

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40
Q

Radio Transmit Continuous

Stuck Microphone Switch

A

Condition: A radio transmits continuously without crew input.

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41
Q

BATTERY DISCHARGE

A

Condition: A battery discharge exceedance occurs.

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42
Q

DRIVE

A

Condition: A generator drive malfunction occurs.

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43
Q

ELEC

A

Condition: A standby power or DC system fault occurs.

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44
Q

LOSS OF BOTH ENGINE DRIVEN GENERATORS

A

Condition: Both engine driven generators are off.

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45
Q

SOURCE OFF

A

Condition: The transfer bus is not powered by the last selected source.

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46
Q

STANDBY POWER OFF

A

Condition: One or more of these buses are not energised.

  • AC Standby bus
  • DC Standby bus
  • Battery bus.
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47
Q

TR UNIT

A

Condition: One or more of the transformer rectifiers are failed.

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48
Q

TRANSFER BUS OFF

A

Condition: The transfer bus is not energised.

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49
Q

Aborted Engine Start

A

Condition: On the ground, an aborted engine start is needed.

Objective: To shut down the engine and motor it.

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50
Q

Engine Limit or Surge or Stall

A

Condition: One or more of these occur

  • 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 inlet or exhaust are reported.

Objective: To attempt to recover normal engine operation or shut down the engine if recovery is not possible.

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51
Q

Loss Of Thrust On Both Engines

A

Condition: Both of these occur

  • Both engines have a loss of thrust
  • Both ENG FAIL alerts show.

Objective: To restart at least one engine

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52
Q

APU FAULT

A

Condition: An APU malfunction occurs.

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53
Q

APU LOW OIL PRESSURE

A

Condition: The APU pressure is low.

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54
Q

APU OVERSPEED

A

Condition: One of these occurs

  • An APU RPM limit exceedance causes automatic shutdown
  • During normal APU shutdown the overspeed shutdown protection logic fails a self-test
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55
Q

EEC ALTERNATE MODE

A

Condition: An EEC operates in the alternate control mode.

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56
Q

ENGINE CONTROL

A

Condition: An engine control system fault occurs.

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57
Q

Engine Failure or Shutdown

A

Condition: One of these occurs

  • An engine failure
  • An ENG FAIL alert is shown
  • An engine flameout
  • Another checklist directs an engine shutdown.
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58
Q

Engine High Oil Temperature

A

Condition: The engine oil temperature is high.

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59
Q

Engine High Vibration

A

Condition: The vibration is more than 4.0 units. Airframe vibration may or may not be felt.

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60
Q

Engine In-Flight Start

A

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

  • There was no engine fire
  • There is N1 rotation
  • There is no abnormal airframe vibration.
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61
Q

ENGINE LOW OIL PRESSURE

A

Condition: The engine oil pressure is low. The LOW OIL PRESSURE alert may or may not be illuminated.

62
Q

ENGINE OIL FILTER BYPASS

A

Condition: The OIL FILTER BYPASS alert indicates oil filter contamination can cause oil to bypass the oil filter.

63
Q

One Engine Inoperative Landing

A

Condition: Landing must be made with one engine inoperative.

64
Q

REVERSER

A

Condition: A fault occurs in the thrust reverser system.

65
Q

REVERSER UNLOCKED (IN FLIGHT)

A

Condition: The amber REV indication shows with uncommanded reverse thrust.

66
Q

START VALVE OPEN

A

Condition: The START VALVE OPEN alert indicates the start valve fails to close.

67
Q

Volcanic Ash

A

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

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

Objective: To exit the ash cloud and restart the engines if needed.

68
Q

APU FIRE

A

Condition: Fire is detected in the APU.

69
Q

ENGINE FIRE
or
Engine Severe Damage or Separation

A

Condition: One or more of these occur:

  • Engine fire warning
  • Airframe vibrations with abnormal engine indications
  • Engine separation.
70
Q

ENGINE OVERHEAT

A

Condition: An overheat is detected in the engine

71
Q

Engine Tailpipe Fire

A

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

72
Q

Smoke, Fire or Fumes

A

Condition: Smoke, fire or fumes occur.

73
Q

APU DETECTION INOPERATIVE

A

Condition: APU fire detection is inoperative.

74
Q

CARGO FIRE

A

Condition: Fire is detected in the related cargo compartment.

75
Q

CARGO FIRE DETECTOR FAULT

A

Condition: Fire detection is inoperative in one or both cargo compartments.

76
Q

ENGINE FIRE/OVERHEAT DETECTOR FAULT

A

Condition: Engine fire and overheat detection is inoperative.

77
Q

LAVATORY SMOKE

A

Condition: Smoke is detected in one or more lavatories.

78
Q

Smoke or Fumes Removal

A

Condition: Smoke or fumes removal is needed.

79
Q

WHEEL WELL FIRE

A

Condition: Fire is detected in the main wheel well.

80
Q

Runaway Stabilizer

A

Condition: Uncommanded stabilizer trim movement occurs continuously.

81
Q

All Flaps Up Landing

A

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

Objective: To configure for a landing with the leading edge devices retracted and trailing edge flaps less than 1.

82
Q

AUTO SLAT FAIL

A

Condition: The auto slat system is failed.

83
Q

Elevator Tab Vibration

A

Condition: 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 aircraft but can be felt throughout the aircraft
- Vibration that is felt in the control wheel and rudder pedals
- Vibration that causes items attached to the aircraft, such as sun visors, to move.

84
Q

FEEL DIFFERENTIAL PRESSURE

A

Condition: High differential pressure is measured by the elevator feel computer.

85
Q

FLIGHT CONTROL LOW PRESSURE

A

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

Objective: To activate the standby hydraulic system and standby rubber PCU.

86
Q

Jammed or Restricted Flight Controls

A

Condition: A flight control is jammed or restricted in roll, pitch or yaw.

87
Q

LEADING EDGE FLAPS TRANSIT

A

Condition: One or more of these occur:

  • The leading edge devices are not in the commanded position.
  • A leading edge device asymmetry is detected
  • A leading edge device skew is detected.
88
Q

MACH TRIM FAIL

A

Condition: The Mach trim system is failed.

89
Q

SPEED BRAKE DO NOT ARM

A

Condition: An automatic speedbrake fault occurs.

90
Q

SPEED TRIM FAIL

A

Condition: The speed trim system is failed.

91
Q

SPEEDBRAKES EXTENDED

A

Condition: In flight, the speedbrakes are extended beyond the ARMED position and one or more of these occur:

  • The radio altitude is below 800 feet
  • The flap lever setting is more than flaps 10.

On the ground, the SPEED BRAKE lever is down and the speedbrakes are extended.

92
Q

STABILIZER OUT OF TRIM

A

Condition: The autopilot does not set the stabilizer trim correctly.

93
Q

Stabilizer Trim Inoperative

A

Condition: Both of these occur:

  • Loss of electric trim through the autopilot
  • Loss of electric trim through the control wheel switches.

Objective: To land the airplane using manual trim or, if manual trim is not available, to land the airplane using elevator control only.

94
Q

STANDBY RUDDER ON

A

Condition: The standby rudder hydraulic system is commanded on.

95
Q

Trailing Edge Flap Asymmetry

A

Condition: One or more of these occur:

  • An uncommanded roll occurs when the flaps change position
  • The left and right flap indicators disagree.

Objective: To configure the airplane for landing.

96
Q

Trailing Edge Flap Disagree

A

Condition: The trailing edge flaps are not in the commanded position.

Objective: To configure the aircraft for landing.

97
Q

Trailing Edge Flaps Up Landing

A

Condition: The trailing edge flaps are less than 1.

Objective: To configure for a landing with trailing edge flaps less than 1.

98
Q

YAW DAMPER

A

Condition: The yaw damper is disengaged.

99
Q

Airspeed Unreliable

A

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

Objective: To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight with Unreliable Airspeed table in the Performance Inflight chapter.

100
Q

ALT DISAGREE

A

Condition: The ALT DISAGREE alert indicates the captain’s and first officer’s altitude indications disagree by more than 200ft.

101
Q

AOA DISAGREE

A

Condition: The AOA DISAGREE alert indicates the left and right angle of attack vanes disagree

102
Q

CDS FAULT

A

Condition: The CDS FAULT annunciation indicates a CDS fault occurs.

103
Q

Display Failure

A

Condition: A display in the common display system is failed.

104
Q

DISPLAYS CONTROL PANEL

A

Condition: The DISPLAYS CONTROL PANEL annunciation indicates the EFIS control panel is failed.

105
Q

DISPLAY SOURCE

A

Condition: The DISPLAY SOURCE annunciation indicates only one DEU is supplying display information. Indications may include:

  • No hydraulic pressure indication on the failed side
  • Speed limit flag shown on the failed side
  • Minimum manoeuvre speed and stick shaker band removed on the failed side
  • Both EEC ALTN lights illuminated.
106
Q

FLIGHT RECORDER OFF

A

Condition: The flight recorder is off.

107
Q

IAS DISAGREE

A

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

108
Q

ADS-B Out Failure

A

Condition: One or more of these occur:

  • ATC reports ADS-B Out is lost or degraded
  • GPS-L or GPS-R INVALID message is in the FMC scratchpad and the transponder is selected to the related side.
109
Q

FMC DISAGREE

A

Condition: Data needed for dual FMC operation disagree.

110
Q

FMC DISAGREE - VERTICAL

A

Condition: One of the following occur:

  • Left FMC and right FMC target airspeed disagree during descent
  • Left FMC and right FMC vertical paths disagree during descent.
111
Q

FMC FAIL

A

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

Objective: To restore dual FMC operation, configure for single FMC operation or resume conventional navigation.

112
Q

FMC/CDU ALERTING MESSAGE

A

Condition: An alert message is in the FMC scratchpad.

113
Q

GLS

A

Condition: A GLS failure occurs.

114
Q

GPS

A

Conditions: Both GPS receivers are failed.

115
Q

ILS

A

Conditions: An ILS failure occurs.

116
Q

IRS DC FAIL

A

Conditions: IRS backup DC power is failed.

117
Q

IRS FAULT

A

Conditions: One or more of these occur:

  • An IRS fault occurs
  • On the ground, if the ALIGN light is also illuminated, the present position entry is possibly incorrect.
118
Q

IRS ON DC

A

Conditions: IRS AC power is failed.

119
Q

RVSM Contingency Procedures

A

Condition: Unable to meet RVSM requirements.

120
Q

UNABLE REQD NAV PERF - RNP

A

Condition: UNABLE REQD NAV PERF - RNP is shown. The actual navigation performance is not sufficient.

121
Q

CONFIG

A

Condition: All of these occur:

  • Both centre tank fuel pump switches are off
  • There is more than 726 kgs of fuel in the centre tank.
  • An engine is running.
122
Q

CROSSFEED SELECTOR INOPERATIVE

A

Condition: One of the following occurs:

  • The crossfeed VALVE OPEN light stay illuminated bright blue
  • The CROSSFEED selector is in the open position and the crossfeed VALVE OPEN light is extinguished
  • When the CROSSFEED selector is rotated to a new position, the crossfeed VALVE OPEN light does not illuminate bright blue.
123
Q

FUEL FILTER BYPASS

A

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

124
Q

Fuel Leak Engine

A

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

Objective: To confirm there is an engine fuel leak and shut down the affected engine if needed. This checklist does not address the unlikely possibility of a tank leak.

125
Q

FUEL PUMP LOW PRESSURE

A

Condition: The fuel pump pressure is low.

126
Q

Fuel Quantity Indication Inoperative

A

Condition: The fuel quantity indication is blank.

127
Q

Fuel Temperature Low

A

Condition: The fuel temperature is near the minimum.

128
Q

IMBAL

A

Condition: There is a fuel imbalance between the main tanks.

Objective: To decide if a fuel leak is suspected. To balance fuel if a fuel leak is not suspected.

129
Q

LOW

A

Condition: The fuel quantity is low in the main tank

Objective: To decide is a fuel leak is suspected. To ensure that all fuel is available for use.

130
Q

HYDRAULIC PUMP LOW PRESSURE

A

Condition: The hydraulic pump pressure is low

131
Q

HYDRAULIC PUMP OVERHEAT

A

Condition: The hydraulic pump temperature is high.

132
Q

LOSS OF SYSTEM A

A

Condition: Hydraulic system A pressure is low.

133
Q

LOSS OF SYSTEM B

A

Condition: Hydraulic system B pressure is low

134
Q

MANUAL REVERSION
or
LOSS OF SYSTEM A AND SYSTEM B

A

Condition: Hydraulic system A and B pressure are low.

135
Q

STANDBY HYDRAULIC LOW PRESSURE

A

Condition: The standby hydraulic pump pressure is low.

136
Q

STANDBY HYDRAULIC LOW QUANTITY

A

Condition: The standby hydraulic quantity is low.

137
Q

ANTISKID INOPERATIVE

A

Condition: An antiskid system fault occurs.

138
Q

AUTO BRAKE DISARM

A

Condition: The autobrake system disarms after being set.

139
Q

Brake Pressure Indicator Zero PSI

A

Condition: The brake accumulator has no nitrogen precharge.

140
Q

GEAR DISAGREE

A

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

141
Q

Landing Gear Lever Jammed in the Up Position

A

Condition: The LANDING GEAR lever will not move from the UP position.

142
Q

Landing Gear Lever Will Not Move Up After Takeoff

A

Condition: 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 bypass valve to close.
143
Q

Manual Gear Extension

A

Condition: One of these occurs:

  • Any landing gear is not down and locked when the LANDING GEAR lever is down
  • The LANDING GEAR lever is jammed in the OFF position.
144
Q

Partial or All Gear Up Landing

A

Condition: All landing gear are not down and locked after attempting manual gear extension.

145
Q

LANDING CONFIGURATION

A

Condition: In flight, the steady warning horn sounds.

146
Q

TAKEOFF CONFIGURATION

A

Condition: On the ground, the intermittent cabin altitude/configuration warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.

147
Q

WARNING HORN (INTERMITTENT)
or
WARNING LIGHT - CABIN ALTITUDE OR TAKEOFF CONFIGURATION

A

Condition: One of these occurs:

  • In flight, at an airplane flight altitude above 10,000 feet MSL, the intermittent warning horn or a CABIN ALTITUDE light (if installed and operative) illuminates
  • On the ground, the intermittent warning horn sounds or a TAKEOFF CONFIG light (if installed and operative) illuminates when advancing the thrust levers to takeoff thrust.
148
Q

GROUND PROXIMITY INOPERATIVE

A

Condition: A ground proximity warning system fault occurs.

149
Q

Overspeed

A

Condition: Airspeed is more than Vmo/Mmo.

150
Q

PSEU

A

Condition: A proximity switch electronics unit fault occurs.

151
Q

Tail Strike

A

Condition: A tail strike is suspected or confirmed.

B737 (6 decks)

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