EMERGENCY ENGINE SHUTDOWN
•Engine torque increase - unschedule in flight (not responsive to power lever movement)
• Engine fire in flight
• Engine failure in flight
• Low oil pressure
AFFECTED ENGINE
- Condition Lever - - - - - FUEL CUTOFF
- Propeller Lever - - - - - FEATHER
- Fuel FW Shutoff Valve - - - - - CLOSE
- Fire Extinguisher (if installed) (if fire warning persists) - - - - - ACTUATE
ENGINE FIRE ON GROUND
AFFECTED ENGINE
- Condition Lever - - - - - FUEL CUTOFF
- Fuel FW Shutoff Valve - - - - - CLOSE
ENGINE FAILURE DURING GROUND ROLL
- Power Lever - - - - - GROUND FINE
- Brakes - - - - - MAXIMUM (or as required to achieve stopping performance)
If Insufficient Runway Remains for Stopping
- Condition Lever - - - - - FUEL CUTOFF
- Fuel FW Shutoff Valve - - - - - CLOSE
- Master Switch - - - - - OFF (Gang Bar down)
- Boost Pumps - - - - - OFF
ENGINE FAILURE AFTER LIFT-OFF
(IF CONDITIONS PRECLUDE AN IMMEDIATE LANDING)
- Maximum Continuous Power - - - - SET
- Airspeed - - - - - MAINTAIN (Takeoff Speed or above)
- Landing Gear - - - - - UP
- Propeller (inoperative engine) - - - - - FEATHER (or verify FEATHER if Autofeather is installed)
- Airspeed (after obstacle clearance altitude is reached) - - - - - 108 KNOTS
ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMcA)
- Power - - - - - REDUCE
- Nose - - - - - LOWER TO ACCELERATE ABOVE VMcA
2ND ENGINE FLAMEOUT
- Power Lever - - - - - IDLE
- Propeller - - - - - DO NOT FEATHER
- Condition Lever - - - - - FUEL CUTOFF
- Conduct Air Start Procedures in Abnormal Procedures
ELECTRICAL SMOKE OR FIRE OR ENVIRONMENTAL SYSTEM SMOKE OR FUMES
- Oxygena. Oxygen System Control - - - - - CONFIRM ON
b. Crew - - - - - DON MASKS
CABIN DOOR UNLOCKED
If the [CABIN DOOR] Illuminates, or If an Unlocked Cabin Door Is Suspected:
1 . All Occupants - - - - - SEATED WITH SEAT BELTS SECURELY FASTENED
EMERGENCY DESCENT
- Power Levers - - - - - IDLE
- Propeller Levers - - - - - HIGH RPM
- Flaps (184 knots maximum) - - - - - APPROACH
- Landing Gear (182 knots maximum) - - - - - DOWN
- Airspeed - - - - - 182 KNOTS MAXIMUM
GLIDE
- Landing Gear - - - - - UP
- Flaps - - - - - UP
- Propellers - - - - - FEATHERED
- Airspeed - - - - - 125 KNOTS
UNSCHEDULED ELECTRIC ELEVATOR TRIM
- Maintain pitch control with elevator
- Control Wheel Trim Switch - - - - - ATTEMPT TO TRIM IN OPPOSITE DIRECTION OF RUNAWAY
- Elevator Trim Switch (Pedestal) - - - - - OFF
- Manual Trim - - - - - RETRIM AS REQUIRED
UNSCHEDULED RUDDER BOOST ACTIVATION
- Rudder Boost - - - - - OFF
USE OF OXYGEN
- Oxygen System Control - - - - - CONFIRM ON
- Crew - - - - - DON MASKS
PRESSURIZATION LOSS [CABIN ALT HI]
- Oxygen System Control - - - - - CONFIRM ON
- Crew - - - - - DON MASKS
HIGH DIFFERENTIAL PRESSURE
Anytime the Differential Pressure Goes Into the Red Arc:
1. Cabin Altitude Controller - - - - SELECT HIGHERCABIN ALTITUDE SETTING
If Condition Persists:
2. Bleed Air Valves - - - - - CLOSE
3. Cabin Pressure (after cabin is depressurized) - - - - - DUMP
4. Bleed Air Valves - - - - - OPEN
EMERGENCY EXIT
- Emergency Release Hatch Cover - - - - - OPEN
- Release Button - - - - - PUSH
- If release button will not push, PULL hooks to override pressure lock and then PUSH the release button
- PULL handle and PUSH out hatch
SPINS
- Control Column - - - - - FULL FORWARD, AILERONS NEUTRAL
- Full Rudder - - - - - OPPOSITE THE DIRECTION OF SPIN
- Power Levers - - - - - IDLE
- Rudder - - - - - NEUTRALIZE WHEN ROTATION STOPS
- Execute a smooth pullout
