QRH Checklists Flashcards
- Miscellaneous
BOMB WARNING IN FLIGHT
A bomb warning is received in flight
- Miscellaneous
BOMB WARNING ON GROUND
A bomb warning is received while on the ground
- Miscellaneous
DITCHING
Airplane ditching and evacuation are needed
- Miscellaneous
HIJACK
A hijack is in progress
- Miscellaneous
OVERWEIGHT LANDING
A landing at greater than maximum landing weight is needed
- Airplane General
Automatic Unlock
The correct emergency code access is entered.
- Airplane General
CREW OXYGEN LOW
Crew oxygen pressure is low
- Airplane General
[] DOOR AFT CARGO
VPD-VPF
VPD-VPF
The aft lower cargo door is not closed and secured.
- Airplane General
[] DOOR AFT CARGO
VOZ, VPH
VOZ, VPH
The aft lower cargo door is not closed and secure
- Airplane General
[] DOOR BULK CARGO
- [] DOOR BULK CARGO
The bulk cargo door is not closed and secure
- Airplane General
[] DOOR E/E ACCESS
- [] DOOR E/E ACCESS
The electrical and electronic access door is not closed and secure
- Airplane General
[] DOOR ENTRY 1-5L, R
- [] DOOR ENTRY 1-5L, R
An entry door is not closed and secure
- Airplane General
[] DOOR FWD ACCESS
- [] DOOR FWD ACCESS
The forward access door is not closed and secure
- Airplane General
[] DOOR FWD CARGO
- [] DOOR FWD CARGO
The forward lower cargo door is not closed and secure
- Airplane General
DOOR WING SLIDE L, R
- DOOR WING SLIDE L, R
The door for the unpressurised wing slide compartment is not secure
- Airplane General
DOORS
- DOORS
Two or more doors are not closed and secure
- Airplane General
ELT ON
- ELT ON
The emergency locator transmitter is on
- Airplane General
EMER LIGHTS
- EMER LIGHTS
One of these occurs:
• The emergency lights are on;
• The emergency lights switch is not ARMED
- Airplane General
LOCK FAIL
- LOCK FAIL
One or more of these occur:
• The flight deck access system switch is off;
• The lock is failed.
- Airplane General
PASS OXYGEN LOW
- PASS OXYGEN LOW
The Passenger oxygen pressure is low
- Airplane General
PASS OXYGEN ON
- PASS OXYGEN ON
The passenger oxygen system is on
- Airplane General
WINDOW DAMAGE FWD L, R
- WINDOW DAMAGE FWD L, R
The forward flight deck window has one or more of these: • An electrical arc; • A delamination; • A crack; • Is shattered.
- Airplane General
WINDOW DAMAGE SIDE L, R
- WINDOW DAMAGE SIDE L, R
The side flight deck window has one or more of these: • An electrical arc; • A delamination; • A crack; • Is shattered.
- Airplane General
[] WINDOW FLT DECK L, R
- [] WINDOW FLT DECK L, R
The side window is not closed and secure
- Airplane General
[] WINDOWS
- [] WINDOWS
The left and right side windows are not closed and secure
- Air Systems
[] CABIN ALTITUDE (M)
- [] 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
- Air Systems
BLEED ISLN CLOSED C, L, R
- BLEED ISLN CLOSED C, L, R
One of the following occurs:
• the isolation valve has failed closed;
• the bleed isolation switch is off
- Air Systems
BLEED ISLN OPEN C, L, R
- BLEED ISLN OPEN C, L, R
The isolation valve is failed open
- Air Systems
[] BLEED LEAK BODY
- [] BLEED LEAK BODY
A bleed air leak occurs in the body area
- Air Systems
[] BLEED LEAK L, R
- [] BLEED LEAK L, R
A bleed air leak occurs in the wing or pack bay area
- Air Systems
[] BLEED LEAK STRUT L, R
- [] BLEED LEAK STRUT L, R
A bleed air leak or starter duct leak occurs in the strut area.
- Air Systems
[] BLEED LOSS BODY
- [] BLEED LOSS BODY
Bleed air from the left and right body ducts is not available.
- Air Systems
[] BLEED LOSS BODY L
- [] BLEED LOSS BODY L
Bleed air from the left body duct is not available.
- Air Systems
[] BLEED LOSS BODY R
- [] BLEED LOSS BODY R
Bleed air from the right body duct is not available
- Air Systems
[] BLEED LOSS WING L, R
- [] BLEED LOSS WING L, R
Bleed air from the wing duct is not available
- Air Systems
BLEED OFF APU
- 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.
- Air Systems
BLEED OFF ENG L, R
- 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.
- Air Systems
[] CABIN ALTITUDE AUTO
- [] CABIN ALTITUDE AUTO
One of these occurs:
• Automatic pressurisation control is failed;
• Both outflow valve switches are in manual.
- Air Systems
CARGO HEAT AFT
- CARGO HEAT AFT
One of these occurs:
• Aft lower cargo heat is inoperative;
• The aft cargo temperature selector is OFF.
- Air Systems
CARGO HEAT BULK
- CARGO HEAT BULK
One of these occurs:
• bulk cargo heat is inoperative;
• the bulk cargo temperature selector is off.
- Air Systems
EQUIP COOLING
- EQUIP COOLING
The forward equipment cooling system is failed
- Air Systems
[] EQUIP COOLING OVRD
- [] EQUIP COOLING OVRD
The equipment cooling system is in override mode.
- Air Systems
[] LANDING ALTITUDE
- [] LANDING ALTITUDE
One of these occurs:
• The FMC does not supply a landing altitude;
• The landing altitude selector is pulled.
- 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.
- Air Systems
[] PACK L
The left pack is inoperative
- Air Systems
[] PACK L+R
Both packs are inoperative
- 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.
- Air Systems
[] PACK R
The right pack is inoperative
- Air Systems
[] TRIM AIR L, R
The trim air valve is closed
- Anti-Ice, Rain
[] ANTI-ICE ENG L, R
The engine anti-ice valve is closed when commanded open
- Anti-Ice, Rain
[] ANTI-ICE LEAK ENG L, R
A bleed air leak occurs in the engine anti-ice duct
- Anti-Ice, Rain
ANTI-ICE LOSS ENG L, R
Anti-ice bleed air for the engine is not available
- 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.
- Anti-Ice, Rain
[] ANTI-ICE WING
One or both wing anti-ice valves are failed closed.
- Anti-Ice, Rain
[] HEAT PITOT C
The Center pitot probe heat is failed.
Note: The standby air data is unreliable in icing conditions.
- 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.
- 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.
- 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.
- 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)
- Anti-Ice, Rain
[] ICE DETECTORS
The ice detectors are failed.
Note: Run the engine and wing anti-icing systems manually.
- Anti-Ice, Rain
ICING ENG
Ice is detected and an engine anti-ice selector is off.
- 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.
- Anti-Ice, Rain
[] WINDOW HEAT L, R FWD
Primary window heat for the forward window is inoperative.
- Anti-Ice, Rain
[] WINDOW HEAT L, R SIDE
Window heat for the side window is inoperative
- 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.
- Automatic Flight
AUTOPILOT DISC
All autopilots are disengaged
- Automatic Flight
AUTOTHROTTLE DISC
Both autothrottles are disconnected
- Automatic Flight
[] AUTOTHROTTLE L, R
The Autothrottle is inoperative
- Automatic Flight
NO AUTOLAND
The autoland system is not available
- Automatic Flight
NO LAND 3
The autoland system does not have redundancy for a triple channel autoland
- Communications
DATALINK LOST
The ACARS datalink is temporarily lost
- Communications
DATALINK SYS
The datalink system is failed
- Communications
[] RADIO TRANSMIT
The microphone switch is on and causes a radio to transmit for 40 seconds or more.
- Communications
SATCOM
The SATCOM system is failed
- Communications
SATCOM DATALINK
The SATCOM datalink is failed
- Communications
SATCOM VOICE
SATCOM voice communication is failed
- Communications
SATVOICE LOST
SATCOM voice communication is temporarily lost
- Communications
VHF DATALINK
The VHF datalink is failed
- Electrical
[] ELEC AC BUS L, R
The AC Bus is not energised
- Electrical
[] ELEC BACKUP GEN L, R
The backup generator is failed
- Electrical
[] ELEC BACKUP SYS
The backup power system is failed
- Electrical
ELEC BATTERY OFF
The battery switch is off
- Electrical
ELEC BUS ISLN L, R
The bus tie breaker is open
- Electrical
ELEC CABIN/UTIL OFF
The cabin/utility power switch is OFF
- Electrical
[] ELEC GEN DRIVE L, R
A generator drive fault occurs
- Electrical
[] ELEC GEN OFF APU
The generator control breaker is open
- Electrical
[] ELEC GEN OFF L, R
The generator control breaker is open
- Electrical
ELEC GRD HDLG BUS
A fault occurs in the ground handling bus
- Electrical
ELEC IFE/SEATS OFF
The IFE/passenger seats power switch is OFF.
- Electrical
ELEC STANDBY SYS
A standby power system failure occurs
- 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.
- 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
- 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
- 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.
- 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.
- 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.
- Engines, APU
[] APU LIMIT
An APU limit exceedance occurs.
- Engines, APU
[] APU SHUTDOWN
An APU automatic shutdown occurs.
- Engines, APU
ENG AUTOSTART OFF
The engine autostart switch is off
- Engines, APU
ENG CONTROL L, R
An EEC system fault occurs.
- Engines, APU
[] ENG EEC MODE L, R
The EEC is in the alternate control mode
- Engines, APU
[] ENG FAIL L, R
Engine speed is below idle
- Engines, APU
[] ENG FUEL FILTER L, R
Fuel contamination can cause fuel to bypass the engine fuel filter.
- 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.