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CRG FWD (AFT) SMOKE (Associated Cargo Fire-Extinguishing Button light illuminates)
- ∗ Associated Cargo Fire Extinguishing Button....................................PUSH
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT
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LAV SMOKE
- ∗ Oxygen Masks.................... IF REQ’D DON, 100 %
- ∗ Crew Communication..........................ESTABLISH
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT
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SMOKE EVACUATION
- ∗ Oxygen Masks .....................................DON, 100 %
- ∗ Crew Communication .........................ESTABLISH
- ∗ Pressurization Dump Button................... PUSH IN
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT
- Verify cabin rate, then EMERGENCY DESCENT procedure
- ∗ Fasten Belts Signs............................................................................................ON
- ∗ Altitude ......................................10,000 FT OR MEA, WHICHEVER IS HIGHER
- ∗ FLCH..................................................................................................... SELECT
- ∗ Airspeed .................................................................MAN, MAX/APPROPRIATE If structural damage is suspected, limit airspeed and avoid high maneuvering loads.
- ∗ Thrust Levers............................................................................................. IDLE
- ∗ Speedbrake.................................................................................... FULL OPEN
- ∗ ATC........................................................................................................ NOTIFY
- ∗ Transponder............................................................................................... 7700
- When level off altitude has been reached: PA............................................................. “IN CHARGE FLIGHT ATTENDANT CALL (OR REPORT TO) THE FLIGHT DECK” (“USING OXYGEN” IF REQ’D)
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SMOKE / FIRE / FUMES
CONDITION: Smoke fire or fumes have been spotted by the crew without an EICAS warning.
- ∗ Oxygen Masks ......................................DON, 100%
- ∗ Crew Communication..........................ESTABLISH
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT
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SMOKE/FIRE FROM LITHIUM BATTERY
∗ PA ....................“BACKUP TO THE FLIGHT DECK, BACKUP TO THE FLIGHT DECK”
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CARGO COMPARTMENT FIRE
- ∗ Associated Cargo Fire Extinguishing Button........................................ PUSH
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT After CRG AFT (FWD) FIREX HI ARM message is displayed and the associated Cargo Fire Extinguishing Button is illuminated:
- ∗ Associated Cargo Fire Extinguishing Button ........................PUSH AGAIN
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DUAL ENGINE FAILURE EICAS INDICATION: FAIL icon inside both N1 indicators. Both oil pressure indications in red.
- ∗ Airspeed...................................................................................... 265 KIAS MIN
- ∗ RAT Manual Deploy Lever............................................................................. PULL
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EMERGENCY DESCENT
- ∗ Fstn Belts Signs ...........................................................................................ON
- ∗ Altitude..................................... 10,000 FT OR MEA, WHICHEVER IS HIGHER
- ∗ FLCH.................................................................................................... SELECT
- ∗ Airspeed...........................................................................MAX/APPROPRIATE
- ∗ Thrust Levers............................................................................................ IDLE
- ∗ Speedbrake.................................................................................... FULL OPEN
- ∗ ATC........................................................................................................ NOTIFY
- ∗ Transponder .............................................................................................. 7700
- ∗ When level off altitude has been reached: PA......................................................... “IN CHARGE FLIGHT ATTENDANT CALL (OR REPORT TO) THE FLIGHT DECK” (“USING OXYGEN” IF REQ’D)
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ENGINE ABNORMAL START
- ∗ Affected engine:
- ∗ Start/Stop Selector..................................................................................STOP
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ENGINE FIRE, SEVERE DAMAGE OR SEPARATION
- ∗ Autothrottle.................................................................................. DISENGAGE
- ∗ Affected engine:
- ∗ Thrust Lever............................................................................................ IDLE
- ∗ Start/Stop Selector.................................................................................STOP
- ∗ Fire Extinguishing Handle..................................................................... PULL
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JAMMED CONTROL COLUMN - PITCH
∗ Elev Disc Handle...................................................................................... PULL
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JAMMED CONTROL WHEEL - ROLL
∗ Aileron Disc Handle................................................................................. PULL
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LOSS OF BRAKING
∗ Emergency/Parking Brake....................................................................... PULL
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PITCH TRIM RUNAWAY
- ∗ A/P Disc Button ...................................................................PRESS and HOLD
- ∗ Pitch Trim System 1 and 2 Cutout Buttons.......................................PUSH IN
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ROLL (YAW) TRIM RUNAWAY
∗ A/P Disc Button ..................................................................PRESS AND HOLD
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STEERING RUNAWAY
- ∗ Steer Disc Switch.................................................................................. PRESS
- ∗ Use differential braking and rudder to steer the airplan
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VOLCANIC ASH
- ∗ Autothrottle.................................................................................. DISENGAGE
- ∗ Thrust Levers (If altitude permits)........................................................... IDLE
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UNRELIABLE AIRSPEED
- ∗ Autothrottle.................................................................................. DISENGAGE
- Avoid quick Thrust Lever movements.
- ∗ Autopilot....................................................................................... DISENGAGE
- ∗ Flight Director............................................................................................. OFF
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CABIN ALTITUDE HI OR RAPID DEPRESSURIZATION EICAS Indication: Cabin Altitude indication in red. Aural Warning: CABIN.
- ∗ Oxygen Masks................................................................................. DON, 100%
- ∗ Crew Communication.................................................................... ESTABLISH
- ∗ Fasten Belts Signs............................................................................................ON
- ∗ PA (if conditions permit).............................. “ATTENTION-FLIGHT ATTENDANTS SECURE THE CABIN-PASSENGERS TAKE YOUR SEATS”
- ∗ Altitude ......................................10,000 FT OR MEA, WHICHEVER IS HIGHER
- ∗ FLCH..................................................................................................... SELECT
- ∗ Airspeed .................................................................MAN, MAX/APPROPRIATE If structural damage is suspected, limit airspeed and avoid high maneuvering loads.
- ∗ Thrust Levers............................................................................................. IDLE
- ∗ Speedbrake.................................................................................... FULL OPEN
- ∗ ATC........................................................................................................ NOTIFY
- ∗ Transponder............................................................................................... 7700
- Cabin Altitude ....................................................................................MONITOR CABIN ALTITUDE REACHES 14,000 FT? No Yes
- ∗ Passenger Oxygen Selector................................................................. OVRD
- ∗ PA.......................................................................... “ATTENTION PUT ON YOUR OXYGEN MASKS IMMEDIATELY”
- When level off altitude has been reached: PA............................................................. “IN CHARGE FLIGHT ATTENDANT CALL (OR REPORT TO) THE FLIGHT DECK” (“USING OXYGEN” IF REQ’D)
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BATT 1(2) OVERTEMP
- ∗ Associated Battery.................................................................................... OFF
- Note: Do not start the APU.
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APU FIRE Light: APU Emergency Stop Button upper half illuminates in red.
∗ APU Emergency Stop Button............................................................PUSH IN
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ENG 1(2) FIRE EICAS Indication: FIRE icon on the associated ITT indicator. Light: Associated fire handle illuminates.
- ∗ Autothrottle.................................................................................. DISENGAGE
- ∗ Affected engine:
- ∗ Thrust Lever............................................................................................ IDLE
- ∗ Start/Stop Selector ................................................................................STOP
- ∗ Fire Extinguishing Handle.................................................................... PULL
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LG BAY FIRE
- ∗ INITIATE DIVERSION TO NEAREST SUITABLE AIRPORT.
- ∗ Airspeed...............................................................................................MAX 265
- ∗ Landing gear .......................................................................................EXTEND
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ENG FAIL/FIRE IN CRUISE
- – Verify or move the thrust levers to the TOGA detent.
- – Verify or select CON thrust. – Disconnect the autothrottle.
- – Set the single engine drift down altitude obtained from the speed card.
- – Advise ATC.
- – Maintain altitude until speed decreases to Green Dot speed.
- – Set speed to MAN.
- – Select FLCH to begin descent after confirming the autothrottle is off and thrust levers are in the TOGA detent.
- – Adjust speed to match Green Dot speed in descent.
- – Land at nearest suitable airport.
- Note: When an engine failure is accompanied with a fire, the drill may be started prior to reaching driftdown speed.
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WINDSHEAR/EGPWS
- Call “FIREWALL” (max thrust)
- Disconnect AP/AT Level Wings
- Press the TO/GA button Follow FD Guidance (windshear) or maintain 20° or PLI whichever is lower
- (GPWS).
- PM call “CLEAR OF WARNING”
- Reconfigure aircraft
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STALL RECOVERY
- Calls “STALL”
- Disconnect AP/AT
- Apply nose down attitude and level wings until out of stall
- Apply thrust as required
- Accelerate the aircraft to a safe speed
- Retract speed brakes
- PM Call “CLEAR OF WARNING”
- Return the aircraft to a normal flight path Call for configuration changes and re-engage automation as required
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LOW ENERGY GO AROUND
- PF............ “FIREWALL” (MAX THRUST), “GO-AROUND, NAV, FLAP”
- – Pitch.................................................................................. ADJUST TO TOUCHDOWN ATTITUDE
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TCAS RA
- – AUTOPILOT................................................................................................................DISCONNECT
- – AUTOTHROTTLE .......................................................................................................DISCONNECT
- – THRUST LEVERS ...............................................................................................................ADJUST
- – PITCH .................................................................................................................AS REQ’D FOR RA If a TCAS "CLIMB" RA occurs on final approach when configured for landing:
- – AUTOPILOT................................................................................................................DISCONNECT
- – AUTOTHROTTLE .......................................................................................................DISCONNECT
- – THRUST LEVERS ...............................................................................................................ADJUST
- – PITCH .................................................................................................................AS REQ'D FOR RA
- – GO-AROUND..........................................................................................PROCEDURE COMPLETE
- PM call “Air Canada ___ TCAS RA”.
- Aural message "CLEAR OF CONFLICT".
- PF return to required flight path, no greater than 500 fpm.
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RTO / GROUND INCIDENT, SEVERE DAMAGE
As per I wills you wills.
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ENG ABNORMALS AT OR ABOVE V1
As per I wills, you wills.
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CREW INCAPACITATION
Two communications with no response, or challenge with significant deviation from profile
- -Assume control of aircraft, maintain/correct flight profile
- -Engage autopilot
- -Request assistance from FAs or flight deck jumpseat observer
- -Adjust seat full aft, tilt back, lock shoulder harness and use as a restraint, rudder pedals full forward
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Emergency Comm during pushback, ground crew and flight deck
- "Emergency, emergency, set brakes, set brakes"
- "Emergency, emergency, stop pushback, stop pushback"
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EMERGENCY Comms
- 2 mins prior to touchdown
- 30 sec prior to touch down
- Rapid Deplanement
- Evacuation
- "Emergency stations, emergency stations"
- "Brace for landing, brace for landing"
- “Deplane immediately and leave your personal belongings”
- “Evacuate, Evacuate”
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BOUNCED LANDING RECOVERY
- Light bounce
- - Maintain landing attitude
- - Apply power
- Severe Bounce
- - TOGA and TL to MAX
- - Hold the flare attitude
- - Low energy GA procedure
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NOSE UP RECOVERY
- - Disengage AP/AT
- - Reduce pitch angle (if necessary, use pitch trim, reduce thrust, bank at 45-60 degrees)
- When pitch back to normal
- - Level wings
- - Reconfigure aircraft
*PM, confirm AP/AT disengage, make callouts
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NOSE DOWN RECOVERY
- - Disengage AP/AT
- - Level wings
- - If airspeed too high, reduce thrust and use speed brakes
- - Pull the control column or use pitch trim to bring back to level flight
- - Resume normal flight, reconfigure aircraft
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Discontinued Approach
- - “DISCOUNTINUED APPROACH”
- - Adjust or verify ALT Preselector.
- - Select the most appropriate vertical mode (VS or FLCH recommended).
- - Select FMS if it is not the navigation source and select HDG/NAV to comply with ATC instructions
or to follow the missed approach profile. If req'd, MISSED APP key on FMS to sequence.
- - Resume proper airplane configuration (gear and flaps) and speed as desired
- * use instead of GA if outside of FAF, not fully configured, or within 400’ of ALT SEL (won't capture if TOGA pressed)
- * select missed app key on FMS if required for navigation (not sequenced auto without TOGA)
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