ABORTED TAKEOFF
ENGINE FAILURE ABOVE V1
At positive rate of climb:
1. Landing Gear Lever – UP 2. Main Air VLVs – CLOSE BOTH 3. F/DK Valve – CLOSE
DOUBLE ENGINE FAILURE
ENGINE FIRE ON GROUND
ENGINE FIRE BELOW V1
OIL LOW PRESSURE
If below 25 PSI:
2. HP Cock (affected engine) – CLOSE
ENGINE FIRE ABOVE V1
At positive rate of climb:
1. Landing Gear Lever – UP 2. Main Air VLVs – CLOSE BOTH 3. F/DK Valve – CLOSE
ENGINE FIRE IN FLIGHT
INADVERTENT THRUST REVERSER DEPLOYMENT BELOW V1
INADVERTENT THRUST REVERSER DEPLOYMENT ABOVE V1
INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT
HIGH PRESSURE AIR OVERHEAT
REAR EQUIPMENT BAY OVERHEAT
APU FIRE (HONEYWELL GTCP 36-50 W)
If fire warning persists:
4. APU FIRE WARN CB – PULL
APU FIRE (GARRET GTCP 30-92C(A))
APU FIRE (TURBOMACH T62T-40C)
FIRE IN FLIGHT COMPARTMENT OR PASSENGER CABIN