Engine Fire or Failure in Flight
Affected Engine:
1. Condition Lever: FUEL CUTOFF
2. Prop Lever: FEATHER
3. Firewall Fuel Valve: CLOSE
4. Fire Extinguisher (if fire warning persists): ACTUATE
Engine Fire on Ground
Affected Engine:
1. Condition Lever: FUEL CUTOFF
2. Firewall Fuel Valve: CLOSE
3. Starter Switch: STARTER ONLY
4. Fire Extinguisher (if fire warning persists): ACTUATE
Emergency Engine Shutdown on the Ground
- Condition Levers: FUEL CUTOFF
- Prop Levers: FEATHER
- Firewall Fuel Valves: CLOSE
- Master Switch (gang bar): OFF
- Battery Bus: EMERG OFF
- ESIS Power: OFF
Engine Failure During Takeoff (at or below V1) - Takeoff Aborted
- Power Levers: GROUND FINE
- Brakes: MAXIMUM
Do not use reverse thrust with one engine inoperative. Care must be exercised when using single-engine ground fine on surfaces with reduced traction.
Engine Failure During Takeoff (at or above V1) - Takeoff Continued
- Vr Speed: ROTATE TO APPROXIMATELY 10 DEGREE PITCH ATTITUDE
- Landing Gear (when positive climb established): UP
- Airspeed: MAINTAIN V2 TO 400ft AGL
- Propellor (inoperative engine): VERIFY FEATHERED
Do not retard the failed engine power lever until the autofeather system has completely stopped propellor rotation. To do so will deactivate the autofeather circuit and prevent automatic feathering.
Engine Failure in Flight Below Air Minimum Control Speed (Vmca)
- Power: REDUCE AS REQUIRED TO MAINTAIN CONTROL
- Nose: LOWER TO ACCELERATE ABOVE VMCA
Electrical Smoke or Fire
- Oxygen Mask(s): DON
- Mask Selector Switch: EMERG
- Mic Switch(es): OXY
Environmental System Smoke or Fumes
- Oxygen Mask(s): DON
- Mask Selector Switch: EMERG
- Mic Switch(es): OXY
Airstair Door / Cargo Door Unlocked (Door Unlocked)
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 seatbelts securely fastened.
If the (DOOR UNLOCKED) illuminates, or if an unlatched airstair door / cargo door is suspected:
1. All Occupants: SEATED WITH SEAT BELTS SECURELY FASTENED
Emergency Descent
- Power Levers: IDLE
- Prop Levers: FULL FORWARD
- Flaps (202 KIAS maximum): APPROACH
- Landing Gear (184 KIAS maximum): DOWN
- Airspeed: 184 KIAS MAXIMUM
Glide
- Landing Gear: UP
- Flaps: UP
Do not feather second engine propellor if a No Starter Assist Air Start is to be conducted. Air Starts with a windmilling propellor will result in lower starting temperatures. - Prop Levers: FEATHERED
- Airspeed: 135 KIAS
Dual Generator Failure (L DC GEN) & (R DC GEN)
- Instrument Emergency Lights (if required): ON
- Generators: RESET, THEN ON
If either generator will reset: - Operating Generator Loadmeter: MONITOR
If neither generator will reset: - ECS Mode: OFF
- Cockpit / Cabin Blower: AUTO
- Non-Essential Equipment: OFF
Do not place the GEN TIES switch in the MAN CLOSE position. This action reconnects the left and right generator bus loads to the battery, severely limiting battery duration.
Pressurisation Loss (Cabin Alt Hi)
- Oxygen Mask(s): DON
- Mic Switch(es): OXY
- Passenger Manual Drop Out: PULL ON
- Descend: AS REQUIRED
The highest recommended cabin altitude for sustained flight is 25000 ft.
High Differential Pressure (Cabin Diff Hi)
- Bleed Air Valves: ENVIR OFF
- Oxygen (crew and passengers): AS REQUIRED
- Descend: AS REQUIRED
Auto-Deployment Oxygen System Failure (CABIN ALT HI) Illuminated, (PASS OXYGEN ON) Extinguished
- Passenger Manual Drop Out: PULL ON
Bleed Air Fail (L BLEED FAIL) or (R BLEED FAIL)
Illumination of an annunciator in flight indicated a possible rupture of a bleed air line aft of the engine firewall.
- Bleed Air Valve (affected engine): PNEU & ENVIR OFF
The BLEED FAIL annunciator will not extinguish after closing the Bleed Air Valve.
BLEED FAIL annunciators may momentarily illuminate during simultaneous wing boot and brake deice operation at low N1 speeds. If annunciators immediately extinguish, they may be disregarded.
Spins
- Control Column: FULL FORWARD, AILERONS NEUTRAL
- Full Rudder: OPPOSITE THE DIRECTION OF SPIN
- Power Levers: IDLE
- Rudder: NEUTRALISE WHEN ROTATION STOPS
- Execute a smooth pullout
Unscheduled Electric Pitch Trim Activation
- Airplane Attitude: MAINTAIN USING ELEVATOR CONTROL
- AP / Trim Disconnect: DEPRESS FULLY & HOLD
Unscheduled Rudder Boost Activation
- AP / Trim Disconnect: DEPRESS TO 1st LEVEL AND HOLD
- Rudder Boost: OFF
If condition persists: - YD / AP DISC (on Flight Guidance Panel): PULL DOWN
Autopilot and Yaw Damper functions will not be available with the YD / AP Disconnect switch in the down position.
Autopilot Mistrim (E) or (A)
Illumination of a red-boxed E (Elevator) or A (Aileron) annunciator on the PFD’s indicates the autopilot is flying the airplane in a mistrimmed condition.
Intentional or automatic disengagement of the autopilot without restraining the control wheel during a 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:
1. Flight Controls: HOLD FIRMLY
2. AP: DISENGAGE
Autopilot Trim Fail (TRIM)
Illumination of a red TRIM annunciation on the PFD’s indicates that the autopilot pitch trim system has failed. The autopilot will not automatically disengage, but it may not function properly.
A mistrimmed condition may occur in conjunction with the pitch trim failure. When the autopilot is disengaged in a mistrimmed condition, expect an abrupt change in control force.
- Flight Controls: HOLD FIRMLY
- AP: DISENGAGE
