Engine Fire/Failure in Flight
Affected engine:
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
ENGINE FAILURE DURING TAKEOFF AT/BELOW V1 - TAKEOFF ABORTED
2. Brakes - MAXIMUM (or as required to achieve desired stopping distance)
ENGINE FAILURE DURING TAKEOFF AT/ABOVE V1 - TAKEOFF CONTINUED
ENGINE FAILURE IN FLIGHT BELOW Vmca
2. Nose - LOWER TO ACCELERATE ABOVE Vmca
GLIDE (BOTH ENGINES INOPERATIVE)
DUAL GENERATOR FAILURE [L DC GEN] and [R DC GEN]
UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION
2. AP/Trim disconnect - DEPRESS FULLY (Pitch Trim OFF) - ILLUMINATED
UNSCHEDULED RUDDER BOOST ACTIVATION
SPINS
If a spin is entered inadvertently:
These action should be accomplished as nearly simultaneously as possible
ELECTRICAL SMOKE OR FIRE
WARNING: Dissipation of smoke is not sufficient evidence that a fire has been extinguished. If it cannot be visually confirmed that no fire exists, land at the nearest suitable airport.
ENVIRONMENTAL SYSTEM SMOKE OR FUMES
Oxygen:
AIRSTAIR/CARGO DOOR UNLOCKED
WARNING: Do not attempt to check the security of the airstair door or cargo door in flight. Remain as far from the door as possible with seat belts securely fastened.
If the [DOOR UNLOCKED] Illuminates, of If An Unlatched Airstair Door/Cargo Door is Suspected:
EMERGENCY DESCENT
OXYGEN USE
Crew System:
PRESSURIZATION LOSS [CABIN ALT HI]
WARNING: The highest recommended cabin altitude for sustained flight is 25,000 ft.
HIGH DIFFERENTIAL PRESSURE
AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE
BLEED AIR FAILURE
If illuminated during flight:
AUTOPILOT MISTRIM [E] or [A]
WARNING: Intentional or automatic disengagement of the autopilot without restraining the control wheel during mistrim condition will produce a significant airplane response in the direction of the mistrim force.
If a Mistrim Indication continues for more than a few seconds:
AUTOPILOT TRIM FAIL [TRIM]
2. AP - DISENGAGE
AUTOPILOT AUTOMATIC DISENGAGEMENT
If an Automatic Disengagement occurs:
EGPWS in IMC or NIGHT
TAWS+ in IMC or NIGHT