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QRH Checklists Flashcards

1
Q
  1. Airplane General

CREW OXYGEN LOW

A

Crew oxygen pressure is low

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2
Q
  1. Airplane General

[] DOOR AFT CARGO

A

The aft lower cargo door is not closed and latched and locked.

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3
Q
  1. Airplane General

[] DOOR BULK CARGO

A
  1. [] DOOR BULK CARGO

The bulk cargo door is not closed and latched and locked

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4
Q
  1. Airplane General

[] DOOR E/E ACCESS

A
  1. [] DOOR E/E ACCESS

The electrical and electronic access door is not closed and latched and locked

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5
Q
  1. Airplane General

[] DOOR ENTRY 1L, 1 R

A
  1. [] DOOR ENTRY 1L, 1R

An entry door is not closed and latched and locked

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6
Q
  1. Airplane General

[] DOOR FWD ACCESS

A
  1. [] DOOR FWD ACCESS

The forward access door is not closed and secure

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7
Q
  1. Airplane General

[] DOOR FWD CARGO

A
  1. [] DOOR FWD CARGO

The forward lower cargo door is not closed and secure

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8
Q
  1. Airplane General

[] DOOR MAIN DECK CARGO

A

Main deck cargo door is not closed and latched and locked

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9
Q
  1. Airplane General

[] DOORS

A
  1. DOORS

Two or more doors are not closed and secure

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10
Q
  1. Airplane General

ELT ON

A
  1. ELT ON

The emergency locator transmitter is on

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11
Q
  1. Airplane General

EMER LIGHTS

A
  1. EMER LIGHTS

One of these occurs:
• The emergency lights habe been manually activated
• The emergency lights switch is OFF

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12
Q
  1. Airplane General

SUPRNMRY OXYGEN ON

A
  1. PASS OXYGEN ON

The supernumerary oxygen system is activated

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13
Q
  1. Airplane General

[] WINDOW FLT DECK L, R

A
  1. [] WINDOW FLT DECK L, R

The side window is not closed and latched

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14
Q
  1. Airplane General

[] WINDOWS

A
  1. [] WINDOWS

The left and right side windows are not closed and latched

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15
Q
  1. Airplane General

DOORS AUTO/MANUAL

A

Some entry doors are in the armed mode and some are in the disarmed mode

Memo

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16
Q
  1. Air Systems

[] CABIN ALTITUDE (M)

A
  1. [] CABIN ALTITUDE (M)
Cabin Altitude is excessive (M)
1 don oxy masks
2 establish crew communications
3 check cabin altitude and rate
4 if cabin alt uncontrollable:
   - pax oxygen switch.. push on and hold 1 second
   - descend LSA or 10000 if higher
      • thrust to idle
      • extend speedbrakes
      • if struct integ in doubt
         - limit airspeed 
         - avoid high manoeuvring loads
      • descend at Vmo/Mmo
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17
Q
  1. Air Systems

BLEED ISLN CLOSED C, L, R

A
  1. BLEED ISLN CLOSED C, L, R

One of the following occurs:
• the isolation valve has failed closed;
• the bleed isolation switch is off

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18
Q
  1. Air Systems

BLEED ISLN OPEN C, L, R

A
  1. BLEED ISLN OPEN C, L, R

The isolation valve is failed open

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19
Q
  1. Air Systems

[] BLEED LEAK BODY

A
  1. [] BLEED LEAK BODY

A bleed air leak occurs in the body area

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20
Q
  1. Air Systems

[] BLEED LEAK L, R

A
  1. [] BLEED LEAK L, R

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

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21
Q
  1. Air Systems

[] BLEED LEAK STRUT L, R

A
  1. [] BLEED LEAK STRUT L, R

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

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22
Q
  1. Air Systems

[] BLEED LOSS BODY

A
  1. [] BLEED LOSS BODY

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

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23
Q
  1. Air Systems

[] BLEED LOSS BODY L

A
  1. [] BLEED LOSS BODY L

Bleed air from the left body duct is not available.

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24
Q
  1. Air Systems

[] BLEED LOSS BODY R

A
  1. [] BLEED LOSS BODY R

Bleed air from the right body duct is not available

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25
2. Air Systems [] BLEED LOSS WING L, R
2. [] BLEED LOSS WING L, R Bleed air from the wing duct is not available
26
2. Air Systems BLEED OFF APU
2. BLEED OFF APU One of the following occurs: • The APU bleed valve is closed because of a system fault; • The APU bleed switch is off.
27
2. Air Systems BLEED OFF ENG L, R
2. BLEED OFF ENG L, R One of the following occurs: • The engine bleed valve is closed because of a system fault; • The engine bleed switch is off.
28
2. Air Systems [] CABIN ALTITUDE AUTO
2. [] CABIN ALTITUDE AUTO One of these occurs: • Automatic pressurisation control is failed; • Both outflow valve switches are in manual.
29
2. Air Systems CARGO HEAT AFT
2. CARGO HEAT AFT One of these occurs: • Aft lower cargo heat is inoperative; • The aft cargo temperature selector is OFF.
30
2. Air Systems CARGO HEAT BULK
2. CARGO HEAT BULK One of these occurs: • bulk cargo heat is inoperative; • the bulk cargo temperature selector is off.
31
2. Air Systems EQUIP COOLING
2. EQUIP COOLING The forward equipment cooling system is failed
32
2. Air Systems [] EQUIP COOLING OVRD
2. [] EQUIP COOLING OVRD The equipment cooling system is in override mode.
33
2. Air Systems [] LANDING ALTITUDE
2. [] LANDING ALTITUDE One of these occurs: • The FMC does not supply a landing altitude; • The landing altitude selector is pulled.
34
2. Air Systems [] OUTFLOW VALVE AFT, FWD
One of these occurs: • Automatic control of the outflow valve is inoperative; • The outflow valve switch is in manual.
35
2. Air Systems [] PACK L
The left pack is inoperative
36
2. Air Systems [] PACK L+R
Both packs are inoperative
37
2. Air Systems [] PACK MODE L, R
The pack is in the standby mode. Note: At lower altitudes or higher outside air temperatures, the pack may shut down.
38
2. Air Systems [] PACK R
The right pack is inoperative
39
2. Air Systems [] TRIM AIR L, R
The trim air valve is closed
40
3. Anti-Ice, Rain [] ANTI-ICE ENG L, R
The engine anti-ice valve is closed when commanded open
41
3. Anti-Ice, Rain [] ANTI-ICE LEAK ENG L, R
A bleed air leak occurs in the engine anti-ice duct
42
3. Anti-Ice, Rain ANTI-ICE LOSS ENG L, R
Anti-ice bleed air for the engine is not available
43
3. Anti-Ice, Rain [] ANTI-ICE ON
All of these occur: • wAn anti-ice selector is ON; • TAT is more than 10 degrees C; • Ice is not detected.
44
3. Anti-Ice, Rain [] ANTI-ICE WING
One or both wing anti-ice valves are failed closed.
45
3. Anti-Ice, Rain [] HEAT PITOT C
The Center pitot probe heat is failed. Note: The standby air data is unreliable in icing conditions.
46
3. Anti-Ice, Rain [] HEAT PITOT L
The left pitot probe heat is failed. Note: The PFD air data is not affected by single pitot heat failure. Ensure that the right AIR DATA/ATT source switch stays off.
47
3. Anti-Ice, Rain [] HEAT PITOT L+C+R
The left, Center and right pitot probe heat are failed. Note: The air data is unreliable in icing conditions.
48
3. Anti-Ice, Rain [] HEAT PITOT R
The right pitot probe heat is failed. Note: The PFD air data is not affected by single pitot heat failure. Ensure that the left AIR DATA/ATT source switch stays off.
49
3. Anti-Ice, Rain ICE CRYSTAL ICING
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 aeroplane; • Appearance of liquid water on the windshield temperatures too low 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° C; • Abnormal engine vibration indications. (additional items that can indicate ice crystal icing are listed in the additional information section)
50
3. Anti-Ice, Rain [] ICE DETECTORS
The ice detectors are failed. Note: Run the engine and wing anti-icing systems manually.
51
3. Anti-Ice, Rain ICING ENG
Ice is detected and an engine anti-ice selector is off.
52
3. Anti-Ice, Rain ICING WING
Icing is detected and one of these occurs: • The wing anti-ice selector is OFF; • The wing anti-ice takeoff inhibit is active.
53
3. Anti-Ice, Rain [] WINDOW HEAT L, R FWD
Primary window heat for the forward window is inoperative.
54
3. Anti-Ice, Rain [] WINDOW HEAT L, R SIDE
Window heat for the side window is inoperative
55
4. Automatic Flight AUTOPILOT
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.
56
4. Automatic Flight AUTOPILOT DISC
All autopilots are disengaged
57
4. Automatic Flight AUTOTHROTTLE DISC
Both autothrottles are disconnected
58
4. Automatic Flight [] AUTOTHROTTLE L, R
The Autothrottle is inoperative
59
4. Automatic Flight NO AUTOLAND
The autoland system is not available
60
4. Automatic Flight NO LAND 3
The autoland system does not have redundancy for a triple channel autoland
61
5. Communications DATALINK LOST
The ACARS datalink is temporarily lost
62
5. Communications DATALINK SYS
The datalink system is failed
63
5. Communications [] RADIO TRANSMIT
The microphone switch is on and causes a radio to transmit for 40 seconds or more.
64
5. Communications SATCOM
The SATCOM system is failed
65
5. Communications SATCOM DATALINK
The SATCOM datalink is failed
66
5. Communications SATCOM VOICE
SATCOM voice communication is failed
67
5. Communications SATVOICE LOST
SATCOM voice communication is temporarily lost
68
5. Communications VHF DATALINK
The VHF datalink is failed
69
6. Electrical [] ELEC AC BUS L, R
The AC Bus is not energised
70
6. Electrical [] ELEC BACKUP GEN L, R
The backup generator is failed
71
6. Electrical [] ELEC BACKUP SYS
The backup power system is failed
72
6. Electrical ELEC BATTERY OFF
The battery switch is off
73
6. Electrical ELEC BUS ISLN L, R
The bus tie breaker is open
74
6. Electrical ELEC CABIN/UTIL OFF
The cabin/utility power switch is OFF
75
6. Electrical [] ELEC GEN DRIVE L, R
A generator drive fault occurs
76
6. Electrical [] ELEC GEN OFF APU
The generator control breaker is open
77
6. Electrical [] ELEC GEN OFF L, R
The generator control breaker is open
78
6. Electrical ELEC GRD HDLG BUS
A fault occurs in the ground handling bus
79
6. Electrical ELEC IFE/SEATS OFF
The IFE/passenger seats power switch is OFF.
80
6. Electrical ELEC STANDBY SYS
A standby power system failure occurs
81
6. Electrical [] MAIN BATTERY DISCH
One of these occurs: • The main battery is discharging; • The hot battery bus is not energised. Note: The main battery can power the standby system for a minimum of 10 minutes.
82
7. Engines, APU ABORTED ENGINE START L, R (M)
On the ground, an aborted engine start is needed (M) 1. FUEL CONTROL switch (effected side)... CUTOFF
83
7. Engines, APU DUAL ENG FAIL/STALL (M)
Engine speed for both engines is below idle (M) 1. FUEL CONTROL switches (both)... CUTOFF, then RUN; 2. RAM AIR TURBINE switch... Push and hold for 1 second
84
7. Engines, APU [] ENG AUTOSTART L, R (M)
During ground start, one of these occurs: • Autostart did not start the engine; • Fuel control switch is in RUN at low engine RPM with the auto start switch OFF. (M) 1. FUEL CONTROL switch (affected side)... CUTOFF.
85
7. Engines, APU ENG LIM/SURGE/STALL L, R (M)
One or more of these occur: • Engine indications are abnormal; • Engine indications are quickly nearing or showing 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. (M) 1. A/T ARM switch (affected side)... Confirm... OFF; 2. Thrust Lever (affected side)... Confirm... Retard until engine indications stay within limits or the thrust lever is at idle.
86
7. Engines, APU ENG SVR DAMAGE/SEP L, R (M)
One or more of these occur: • Airframe vibrations with abnormal engine indications; • Engine separation. (M) 1. A/T ARM switch (affected side)... Confirm... OFF; 2. Thrust Lever (affected side)... Confirm... Idle; 3. FUEL CONTROL Switch (affected side)... Confirm... CUTOFF; 4. Engine Fire Switch (affected side)... Confirm... Pull.
87
7. Engines, APU [] APU LIMIT
An APU limit exceedance occurs.
88
7. Engines, APU [] APU SHUTDOWN
An APU automatic shutdown occurs.
89
7. Engines, APU ENG AUTOSTART OFF
The engine autostart switch is off
90
7. Engines, APU ENG CONTROL L, R
An EEC system fault occurs.
91
7. Engines, APU [] ENG EEC MODE L, R
The EEC is in the alternate control mode
92
7. Engines, APU [] ENG FAIL L, R
Engine speed is below idle
93
7. Engines, APU [] ENG FUEL FILTER L, R
Fuel contamination can cause fuel to bypass the engine fuel filter.
94
7. Engines, APU [] ENG FUEL VALVE L, R
One or more of these occur: • The engine fuel valve is not in the commanded position; • The fuel spa valve is not in the commanded position.
95
7. Engines, APU ENG IDLE DISAGREE
One engine is at approach idle and the other is at minimum idle
96
7. Engines, APU ENG IN-FLIGHT START L, R
And 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.
97
7. Engines, APU [] ENG LIMIT PROT L, R
The EEC is in the alternate mode and the commanded N1 exceeds the limit.
98
7. Engines, APU [] ENG OIL FILTER L, R
Oil filter contamination has caused oil to bypass the oil filter
99
7. Engines, APU [] ENG OIL PRESS L, R
The engine oil pressure is low
100
[] ENG OIL TEMP L,R
The engine oil temperature is high
101
7. Engines, APU [] ENG REV LIMITED L, R
The engine Reverser operation is limited. Note: On landing, the effected thrust reverser will not deploy or affected reverse thrust will be limited to idle.
102
7. Engines, APU ENG REVERSER L, R
A fault occurs in the thrust reverser system
103
7. Engines, APU ENG RPM LIMITED L, R
Engine thrust is at the N1 or N2 red line limit.
104
7. Engines, APU ENG SHUTDOWN
Both engines were shut down by the fuel control switches or the engine fire switches
105
7. Engines, APU ENG SHUTDOWN L, R
The engine was shutdown by the fuel control switch or the engine fire switch.
106
7. Engines, APU [] ENG START VALVE L, R
The start valve is not in the commanded position.
107
7. Engines, APU [] ENG STARTER CUTOUT L, R
One of these occurs: • The start valve fails to close; • The start selector stays in start.
108
7. Engines, APU ENG THRUST L, R
The engine thrust is less than the commanded thrust
109
7. Engines, APU VOLCANIC ASH
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 in the flightdeck; • An acrid odour.
110
8. Fire Protection [] FIRE APU
Fire is detected in the APU
111
8. Fire Protection [] FIRE ENG L, R (M)
Fire is detected in the engine. (M) 1. A/T ARM switch (affected side)... Confirm... OFF; 2. Thrust Lever (affected side)... Confirm... Idle; 3. FUEL CONTROL switch (affected side)... Confirm... CUTOFF; 4. Engine fire switch (affected side)... Confirm... Pull; 5. If the FIRE ENG message stays shown: • Engine fire switch (affected side)... Rotate to the stop and hold for 1 second; • If after 30 seconds, the FIRE ENG message stays shown: - Engine fire switch (affected side)... Rotate to the other stop and hold for 1 second.
112
8. Fire Protection FIRE ENG TAILPIPE L, R
An engine tailpipe fire occurs on the ground with no fire warning.
113
8. Fire Protection SMOKE, FIRE OR FUMES
Smoke, fire or fumes occurs
114
8. Fire Protection BOTTLE 1, 2 DISCH ENG
The engine fire extinguisher bottle pressure is low
115
8. Fire Protection BOTTLE DISCH APU
The APU fire bottle pressure is low.
116
8. Fire Protection BOTTLE DISCH CARGO
Both rapid discharge cargo fire extinguisher bottle pressures are low
117
8. Fire Protection [] DET FIRE APU
APU fire detection is failed
118
8. Fire Protection DET FIRE CARGO AFT, FWD
Lower cargo compartment smoke detection is failed
119
8. Fire Protection DET FIRE ENG L, R
Engine fire and overheat detection is failed
120
8. Fire Protection [] FIRE CARGO AFT
Smoke is detected in the aft lower cargo compartment.
121
8. Fire Protection [] FIRE CARGO FWD
Smoke is detected in the forward lower cargo compartment.
122
8. Fire Protection [] FIRE WHEEL WELL
Fire is detected in a main wheel well
123
8. Fire Protection [] OVERHEAT ENG L, R
An overheat is detected in an engine.
124
8. Fire Protection [] SMOKE REST UPR DR 1
Smoke is detected in the crew rest area.
125
8. Fire Protection [] SMOKE REST UPR DR 5
Smoke is detected in the crew rest area.
126
8. Fire Protection SMOKE OR FUMES REMOVAL
Smoke or fumes removal is needed
127
9. Flight Controls [] STABILIZER (M)
One of these occurs: • Stabilizer movement without a signal to trim; • The stabilizer is failed. (M) 1. STAB cutout switches (both)... CUTOUT; 2. Do not exceed the current airspeed.
128
9. Flight Controls [] AUTO SPEEDBRAKE
An automatic speedbrake fault occurs. NOTE: Do not arm the speedbrake lever. This prevents inadvertent in-flight speedbrake extension. Manually extend the speedbrakes after landing.
129
9. Flight Controls [] FLAPS DRIVE
The flap drive mechanism is failed.
130
9. Flight Controls [] FLAPS PRIMARY FAIL
The flaps primary mode is failed
131
9. Flight Controls [] FLAP/SLAT CONTROL
The flap/slat electronics units are failed.
132
9. Flight Controls [] FLIGHT CONTROL MODE
The flight control system is in the secondary mode.
133
9. Flight Controls [] FLIGHT CONTROLS
One or more of these occurs: • Two or more flight control surfaces are inoperative; • Other faults in the flight control system are detected.
134
9. Flight Controls FLT CONTROL VALVE
One or more of these occur: • One or more of the flight control shutoff valves are failed closed; • One or more of the flight control switches are in shutoff.
135
9. Flight Controls JAMMED FLIGHT CONTROLS
Flight Controls are jammed or restricted in roll, pitch, or yaw.
136
9. Flight Controls [] PITCH DOWN AUTHORITY
Pitch down authority is restricted. Note: Slower airspeeds assist nosedown pitch control. The aeroplane is approaching it's pitch down limit. Avoid speedbrake use and rapid thrust increases in flight. Only limited elevator authority is available to counter nose up pitch. Do not speed brake lever. Slowly extend the speedbrakes after landing. Refer to the non-normal configuration landing distance table in the performance in-flight chapter.
137
9. Flight Controls [] PITCH UP AUTHORITY
Pitch up and flare authority are restricted.
138
9. Flight Controls [] PRI FLIGHT COMPUTERS
The flight control system is operating in the direct mode.
139
9. Flight Controls [] SLATS DRIVE
The slat drive mechanism is failed.
140
9. Flight Controls [] SLATS PRIMARY FAIL
The slats primary mode is failed.
141
9. Flight Controls SPEEDBRAKE EXTENDED
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.
142
9. Flight Controls [] SPOILERS
One or more spoiler pairs are failed. Note: Roll rate may be reduced in flight. Speedbrake affectivness may be reduced in flight and during landing. Roll tendencies, yaw tendencies, or airframe buffet can indicate a spoiler failed in the extended position. Do not use FMC fuel predictions with a spoiler panel extended.
143
9. Flight Controls [] STAB GREENBAND
The nose gear pressure sensor disagrees with the computed stabiliser greenband.
144
9. Flight Controls [] STABILIZER C
The Center stabiliser control path is failed.
145
9. Flight Controls STABILIZER CUTOUT
Both Stabilizer cutout switches are in CUTOUT.
146
9. Flight Controls [] STABILIZER R
The right Stabilizer control path is failed.
147
9. Flight Controls [] THRUST ASYM COMP
Thrust asymmetry compensation is failed or off.
148
10. Flight Instruments, Displays AIRSPEED UNRELIABLE (M)
Airspeed or Mach indications are suspected to be unreliable. (Items which can indicate unreliable airspeed are listed in the Additional Information section) (M) 1. Autopilot disengage switch... Push; 2. A/T ARM switches (both)... OFF; 3. F/D switches (both)... OFF; 4. Set the following gear up pitch attitude and thrust: • Flaps Extended... 10 deg/85% N1; • Flaps Up............. 4 deg/70% N1.
149
10. Flight Instruments, Displays [] ALTN ATTITUDE
Both pilots AIR DATA/ATT source switches are in ALTN. Note: Both PFDs show the SAARU attitude information.
150
10. Flight Instruments, Displays BARO SET DISAGREE
The captains and first offices barometric settings disagree
151
10. Flight Instruments, Displays [] CHKL INCOMPLETE NORM
A normal checklist needs to be completed
152
10. Flight Instruments, Displays [] CHKL NON-NORMAL
There is a hidden nonnormal checklist. All of these occur: • A non-normal checklist is not complete; • The ECL is not displayed; • The related EICAS message is not shown.
153
10. Flight Instruments, Displays DISPLAY SELECT PNL
Left, Centre, or right CDU control of the display select panel is used.
154
10. Flight Instruments, Displays [] EFIS CONTROL PNL L, R
One of these occurs: • The EFIS control panel is failed; • CDU control of the EFIS is used. NOTE: Backup control of the EFIS is accessed from the CDU menu page.
155
10. Flight Instruments, Displays SGL SOURCE AIR DATA
Both PFDs use the same air data source.
156
10. Flight Instruments, Displays [] SGL SOURCE DISPLAYS
Some or all display units use a single source of display data. Note: Both PFDs and NDs or just both NDs show information generated from a single source. The lower Center display unit may be blank or may not be capable of showing all normal formats. The left EFIS control panel controls either the right PFD and ND or the right ND only.
157
10. Flight Instruments, Displays [] SGL SOURCE RAD ALT
Both PFDs use the same radio Altimeter source. NOTE: A/T retard during flare is inoperative.
158
10. Flight Instruments, Displays SINGLE SOURCE F/D
Both PFDs use the same flight director source.
159
11. Flight Management, Navigation ADS-B OUT FAILURE
One or more of these occur: • ATC reports ADS-B Out 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.
160
11. Flight Management, Navigation [] AIR DATA SYS
The three air data sources disagree.
161
11. Flight Management, Navigation [] FMC
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.
162
11. Flight Management, Navigation FMC L, R
An FMC is failed.
163
11. Flight Management, Navigation FMC MESSAGE
An alerting message is on the FMC scratchpad.
164
11. Flight Management, Navigation [] GPS
Both GPS receivers are failed. Note: The FMC uses inertial inputs only, unless radio updating is enabled. ADS-B Out is inoperative. If radio updating is allowed: • Select the FMC REF NAV DATA page; • Select OFF for RAD NAV INHIBIT.
165
11. Flight Management, Navigation [] ILS ANTENNA
Two or more ILS receivers do not use the correct antenna. Note: AFDS may have difficulty capturing or tracking localiser or glideslope. The airplane path may be lower than indicated by the glideslope pointer.
166
[] INSUFFICIENT FUEL
FMC estimated fuel at the destination is less than the entered RESERVES fuel.
167
11. Flight Management, Navigation [] NAV ADIRU INERTIAL
The ADIRU cannot supply correct attitude, position, heading, track, and ground speed data.
168
11. Flight Management, Navigation [] NAV UNABLE RNP
The actual navigation performance is not sufficient.
169
11. Flight Management, Navigation SINGLE SOURCE ILS
Both pilots' displays use the same ILS source.
170
11. Flight Management, Navigation TRANSPONDER L, R
A transponder fault occurs.
171
11. Flight Management, Navigation [] VNAV STEP CLIMB
A FMC-predicted or manually-entered VNAV step climb point has been sequenced and the climb has not started.
172
12. Fuel [] FUEL AUTO JETTISON
One of these occur: • 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.
173
12. Fuel [] FUEL CROSSFEED AFT
The aft fuel crossfeed valve is not in the commanded position.
174
12. Fuel [] FUEL CROSSFEED FWD
The forward fuel crossfeed valve is not in the commanded position.
175
12. Fuel [] FUEL DISAGREE
The totaliser fuel quantity and the FMC calculated fuel quantity disagree.
176
12. Fuel [] FUEL FLOW ENG L, R
Engine fuel flow is abnormally high.
177
12. Fuel [] FUEL IMBALANCE
There is a fuel imbalance between the main tanks.
178
12. Fuel FUEL IN CENTER
The Center tank fuel quantity is at the level where the pump switches must be ON.
179
12. Fuel FUEL JETT NOZZLE L, R
A jettison nozzle valve is not in the commanded position.
180
12. Fuel FUEL JETTISON
Fuel jettison is needed.
181
12. Fuel [] FUEL JETTISON MAIN
The main tank fuel jettison system is failed.
182
12. Fuel [] FUEL JETTISON SYS
The fuel jettison system is failed.
183
12. Fuel FUEL LEAK
A fuel leak is suspected for the reasons listed in the Additional Information section of this checklist.
184
12. Fuel FUEL LOW CENTER
The Center tank fuel quantity is at the level where the pump switches must be off.
185
12. Fuel [] FUEL PRESS ENG L, R
The affected engine is on suction feed.
186
12. Fuel FUEL PRESS ENG L+R
Fuel pressure to both engines is low on the ground with the engines shut down.
187
12. Fuel [] FUEL PUMP CENTER L, R
The Center fuel pump pressure is low.
188
12. Fuel [] FUEL PUMP L AFT, FWD
The left fuel pump pressure is low.
189
12. Fuel [] FUEL PUMP R AFT, FWD
The right fuel pump pressure is low.
190
12. Fuel [] FUEL QTY LOW
The fuel quantity is low in a main tank.
191
12. Fuel [] FUEL SCAVENGE SYS
The fuel scavenge system is failed.
192
12. Fuel [] FUEL TEMP LOW
Fuel temperature is near the minimum.
193
12. Fuel [] FUEL VALVE APU
The APU fuel valve is not in the commanded position.
194
13. Hydraulics [] HYD AUTO CONTROL C
Both of the following occur: • Automatic control of both Center demand pumps fails; • System indications fail.
195
13. Hydraulics [] HYD AUTO CONTROL L, R
Both of the following occur: • Automatic control of demand pump fails; • System indications fail.
196
13. Hydraulics [] HYD OVERHEAT DEM C1, C2, L, R
The pump temperature is high.
197
13. Hydraulics [] HYD OVERHEAT PRI C1, C2
The pump temperature is high.
198
13. Hydraulics [] HYD OVERHEAT PRI L, R
The pump temperature is high.
199
13. Hydraulics [] HYD PRESS DEM C1, C2, L, R
The demand pump output pressure is low when commanded on.
200
13. Hydraulics [] HYD PRESS PRI C1, C2
The pump pressure is low.
201
13. Hydraulics [] HYD PRESS PRI L, R
The pump pressure is low.
202
13. Hydraulics [] HYD PRESS SYS C
The Center hydraulic system pressure is low.
203
13. Hydraulics [] HYD PRESS SYS L
The left hydraulic system pressure is low.
204
13. Hydraulics [] HYD PRESS SYS L+C
The left and Center hydraulic systems pressures are low.
205
13. Hydraulics HYD PRESS SYS L+C+R
All hydraulic system pressures are low.
206
13. Hydraulics [] HYD PRESS SYS L+R
The left and right hydraulic system pressures are low.
207
13. Hydraulics [] HYD PRESS SYS R
The right hydraulic system pressure is low.
208
13. Hydraulics [] HYD PRESS SYS R+C
The right and Center hydraulic system pressures are low.
209
13. Hydraulics [] HYD QTY LOW C
The Center hydraulic quantity is low.
210
13. Hydraulics HYD QTY LOW L, R
The hydraulic quantity is low.
211
13. Hydraulics [] HYD QTY LOW L+C
The left and Center hydraulic quantities are low.
212
13. Hydraulics [] HYD QTY LOW L+C+R
All three hydraulic quantities are low.
213
13. Hydraulics [] HYD QTY LOW L+R
The left and right hydraulic quantities are low.
214
13. Hydraulics [] HYD QTY LOW R+C
The right and Center hydraulic quantities are low.
215
13. Hydraulics RAT UNLOCKED
The ram air turbine is not stowed and locked.
216
14. Landing Gear [] ANTISKID
An antiskid system fault occurs.
217
14. Landing Gear AUTOBRAKE
One of these occurs: • The autobrake system is disarmed; • The autobrake system is failed.
218
14. Landing Gear [] BRAKE SOURCE
Normal and alternate brake system pressures are low, and reserve hydraulic source for alternate brake system is low. Note: Only accumulator pressure is available for braking. During landing rollout, apply steady, increasing brake pressure and hold to full stop. Do not taxi.
219
14. Landing Gear [] BRAKE TEMP
One or more of the brake temperatures are high.
220
14. Landing Gear [] GEAR DISAGREE
The gear position disagrees with the landing gear lever position.
221
14. Landing Gear [] GEAR DOOR
One or more gear doors and not closed.
222
14. Landing Gear GEAR LEVER LOCKED DOWN
The landing gear lever cannot move to UP.
223
14. Landing Gear [] MAIN GEAR BRACE L, R
The main gear is down with one brace unlocked.
224
14. Landing Gear MAIN GEAR STEERING
Main gear steering does not lock.
225
14. Landing Gear [] RESERVE BRAKES/STRG
One or more of these are possibly not available: • Alternate brakes from the reserve hydraulic source; • Normal nose gear extension; • Nose wheel steering. note: Plan for possible alternate gear extension. Do not taxi with loss of steering.
226
14. Landing Gear TAIL SKID
The tail skid is not in the commanded position.
227
14. Landing Gear [] TIRE PRESSURES
One or more of the tire pressures are not normal.
228
15. Warning Systems AIRSPEED LOW
Airspeed is less than minimum maneuvering speed.
229
15. Warning Systems ALTITUDE ALERT
A deviations from the MCP set altitude occurs.
230
15. Warning Systems ALTITUDE CALLOUTS
Altitude and minimums voice callouts during approach are not available.
231
15. Warning Systems CONFIG DOORS
An entry, forward cargo, or aft cargo door is not closed and latched and locked during takeoff.
232
15. Warning Systems CONFIG FLAPS
The flaps are not in the takeoff position during takeoff.
233
15. Warning Systems CONFIG GEAR
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.
234
15. Warning Systems CONFIG GEAR STEERING
Main gear steering is not locked during takeoff.
235
15. Warning Systems CONFIG PARK BRAKE
The parking brake is set during takeoff.
236
15. Warning Systems CONFIG RUDDER
Rudder trim is not centered during takeoff.
237
15. Warning Systems CONFIG SPOILERS
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.
238
15. Warning Systems CONFIG STABILISER
The stabiliser is not in the greenband during takeoff.
239
15. Warning Systems [] CONFIG WARNING SYS
A configuration warning system fault occurs.
240
15. Warning Systems [] GRD PROX SYS
A ground proximity warning system fault occurs.
241
15. Warning Systems OVERSPEED
Airspeed is more than Vmo/Mmo
242
15. Warning Systems PILOT RESPONSE
Pilot action is not detected during a specified time.
243
15. Warning Systems [] TAIL STRIKE
The tail hits the runway.
244
15. Warning Systems [] TAIL STRIKE
A tail strike is suspected or confirmed.
245
15. Warning Systems TCAS
TCAS is failed.
246
15. Warning Systems TCAS OFF
TCAS modes TA or TA/RA are not selected.
247
15. Warning Systems TCAS RA CAPTAIN, F/O
TCAS cannot show RA guidance on the PFD.
248
15. Warning Systems TERR OVRD
The ground proximity terrain override switch is in OVRD.
249
15. Warning Systems [] TERR POS
Terrain position data is lost. Note: Position data for the ND terrain map and look-ahead terrain alerts are lost. Ground proximity alerts that occur are valid.
250
15. Warning Systems [] WINDSHEAR SYS
15. [] WINDSHEAR SYS A windshear system fault occurs.
251
1. Airplane General DOORS MANUAL
All entry doors are in the disarm mode Memo
252
1. Airplane General SEATBELTS ON
The seatbelt switch is in the on position Memo
253
1. Airplane General DOOR AUTO
All entry doors are in armed mode

* half B777 FCOM (4 decks)

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