Emergency Engine Shutdown -Unscheduled Engine Torque Increase -Engine Fire In Flight -Engine Failure In Flight Illumination of Magnetic Chip Detector Annunciator
Affecteed Engine:
- AP/YD DISC/TRIM INTRPT - PRESS and RELEASE
- Condition Lever - CUTOFF
- Propeller Lever - FEATHER
- Fuel Firewall Valve - CLOSED
- Fire Extinguisher - ACTUATE (if required)
Engine Fire on Ground
Affected Engine:
- Condition Lever - CUTOFF
- Fuel Firewall Valve - CLOSED
- Starter Switch - STARTER ONLY
- Fire Extinguisher - ACTUATE (if required)
Engine Failure During Ground Roll
- Power Levers - IDLE
- Brakes - AS REQUIRED
- Operative Engine - MAX REVERSE
if insufficient runway remains for stopping - Condition Levers - CUTOFF
- Fuel Firewall Valves - CLOSED
- Master Switch - OFF (Gang Bar Down)
Engine Failure After Liftoff (If conditions preclude an immediate landing)
- Power - MAX ALLOWABLE
- Airspeed - MAINTAIN (takeoff speed or above)
- Landing Gear - UP
- Propeller (inop engine) - FEATHER
- Airspeed - BEST RATE OF CLIMB (after obstacle clearance altitude is reached)
- Flaps - UP
Engine Failure in Flight Below Vmca
- Reduce power on operative engine as required
2. Lower nose to accelerate above minimum control speed.
2nd Engine Flameout
- Power Lever - IDLE
- Propeller Lever - DO NOT FEATHER
- Condition Lever - CUTOFF
- Conduct Air Start Procedures
Glide
- Landing Gear - UP
- Wing Flaps - UP
Determine that procedures for restarting 1st and 2nd failed engines are ineffective before feathering 2nd propeller - Propellers - FEATHERED
- Airspeed - 135 KNOTS
Electrical Smoke or Fire
- Oxygen Mask - DON
2. Mic Selector Switch - OXYGEN MASK
Environmental System Smoke or Fumes
- Oxygen Mask - DON
2. Mic Selector Switch - OXYGEN MASK
Emergency Descent
- Power Levers - IDLE
- Propeller Levers - FULL FORWARD
- Flaps - APPROACH (200KT)
- Landing Gear - EXTEND (181KT)
- Airspeed - 181 KNOTS MAX
One Engine Inoperative Go-Around
- Power - MAX ALLOWABLE
- Landing Gear - UP
- Flaps - UP
- Airspeed - Vyse
Autopilot Malfunction/ Pitch Trim Runaway
- Control Wheel - GRIP FIRMLY
- AP/YD/TRIM INTRPT Button - PRESS AND HOLD (be prepared for high elevator pressures)
- Aircraft Attitude - MAINTAIN/REGAIN AIRCRAFT CONTROL (use standby attitude indicator if necessary)
SPINS
- Contol Column - FULL FORWARD
- Rudder - FULL RUDDER OPPOSITE SPIN DIRECTION
- Power - REDUCE
These 3 actions should be done as nearly simultaneously as possible; then continue to hold this control position until rotation stops and then neutralize control and execute a smooth pullout. Ailerons should be neutral during recovery.
Electrical Smoke or Fire
- Oxygen Masks - DON and 100%
- Mic Selector SW - OXYGEN MASK
- PASSENGER MANUAL OVERRIDE - PULL ON
- Passengers - PULL LANYARD PIN, DON MASK
Electrical Smoke or Fire
Windshield Electrical Fault
- Windshield Ht SW - OFF
if smoke or fire persists - CONDUCT ELECTRICAL SMOKE OR FIRE procedure
Environmental System Smoke or Fumes
- Oxygen Masks - DON and 100%
- Mic Selector SW - OXYGEN MASK
- PASSENGER MANUAL OVERRIDE - PULL ON
- Passengers - PULL LANYARD PIN, DON MASK
Emergency Descent
- Power Levers - IDLE
- Propeller Levers - FULL FORWARD
- Flaps - APPROACH (200)
- Landing Gear - EXTEND (181)
- Airspeed - 181 MAXIMUM
Unscheduled Rudder Boost Activation
- Rudder Boost SW - OFF
L or R BLEED AIR FAIL
- Bleed Air Valve SW - INSTR & ENVIR OFF
Dual Generator Failure
- Gen 1 and Gen 2 SW - RESET, THEN ON
2. Operating Gen - DON NOT EXCEED 100% (88% above 31,000)
TAWS OR GPWS Warning
- AP/TRIM DISC/TRIM INTRPT - PRESS and RELEASE
- Aircraft Attitude - PULL BACK ON CONTROL WHEEL
- Power - MAX ALLOWABLE
- Airspeed - BEST ANGLE OF CLIMB SPEED
Windshear Encounter
- AP/TRIM DISC/TRIM INTRPT - PRESS and RELEASE
2. Perform etablished windshear escape maneuvers
