EMERGENCY ENGINE SHUTDOWN

Unscheduled Engine Torque Increase In Flight

(not responsive to Power Lever Movement)

Engine Fire In Flight [L ENG FIRE] or [R ENG FIRE]

Engine Failure In Flight

Affected Engine:

Condition Lever ........................FUEL CUTOFF

Prop Lever ...................................FEATHER

Firewall Shutoff Valve .......................CLOSE

Fire Extinguisher(if fire warning persists)...ACTUATE

ENGINE FIRE ON THE GROUND

[L ENG FIRE] or [R ENG FIRE]

Affected Engine:

Condition Lever .................... Fuel Cutoff

Firewall Shutoff Valve ................... Close

Ignition and Engine Start ............ Starter Only

If fire warning persists:

Fire Extinguisher (if installed) ........... Actuate

Condition Levers........... Fuel Cutoff
Prop Levers .................................... Feather
Firewall Shutoff Valves ............... Close

Master Switch (gang bar) ........ Off

ESIS Power .............................. Off

              ENGINE FAILURE DURING TAKEOFF

(AT OR BELOW V1)

TAKEOFF ABORTED

Power Levers ..........Ground Fine

Brakes .......... as required to achieve stopping distance

Operative Engine ............... Maximum Reverse

ENGINE FAILURE DURING TAKEOFF

(AT OR ABOVE V1)

TAKEOFF CONTINUED

POWER ............... MAXIMUM ALLOWABLE

AIRSPEED......... MAINTAIN (takeoff speed or above)

LANDING GEAR (when positive climb established) .... UP

PROPELLAR (inoperative engine) .......... VERIFY FEATHERED

POWER ........ REDUCE as required to MAINTAIN CONTROL

NOSE .............. LOWER TO ACCCELERATE ABOVE VMCA

POWER ............. AS REQUIRED

FAILED ENGINE ................. SECURE

POWER LEVER ............... IDLE

PROP LEVER ................... DO NOT FEATHER

CONDITION LEVER ................. FUEL CUTOFF

CONDUCT AIR START PROCEDURE in QRH 3A ABNORMAL PROCEDURES

OIL PRESSURE ............... CONFRIM BELOW 60 PSI

IF CONFIRMED

ENGINE ............... SECURE (see Emergency Engine Shutdown)

OR

Land at the nearest suitable airport using the minimum power required to sustain flight.

Limitation Max. 1100 ft/lbs TQE

FUEL PRESSURE LOW

[L FUEL PRESS] or [R FUEL PRESS]

Standby Pump (failed side) .................. ON

[FUEL PRESS] .................... EXTINGUISHED

Oil Temperature and Pressure Indicators (failed side) ............ MONITOR

Oxygen Mask(s) ............... DON

Mask Selector Switch ................. EMERG POSITION

MIC Switch ........................ OXY

Oxygen Mask(s) ..................... DON

Mask Selector Switch .............EMERG POSITION

MIC Switch .................... OXY

AIRSTAIR DOOR/CARGO DOOR UNLOCKED

[DOOR UNLOCKED]

If the [DOOR UNLOCKED] illuminates! or if an unlatched Airstair Door/Cargo Door is suspected:

All Occupants ...................... Seated with Seat Belts  securely fastened.

POWER LEVERS ...................... IDLE

PROP LEVERS ................... FULL FORWARD

FLAPS (200 knots maximum) ........... APPROACH

LANDING GEAR (181 knots maximum) ......... DOWN

AIRSPEED ..................... 181 KNOTS MAXIMUM

LANDING GEAR ....................... UP

FLAPS ..................... UP

PROPELLARS ...................... FEATHERED

AIRSPEED ..................... 135 KNOTS

DUAL GENERATOR FAILURE 

[L DC GEN] & [R DC GEN]

GENERATORS .................... RESET, THEN ON

If either generator will reset:

Operating Generator Loadmeter..............DO NOT EXCEED 100%

(88% above 31000FT)

Inoperative Generator.................... OFF

PRESSURISATION LOSS

[ALT WARN]

OXYGEN MASK(S) ................. DON

MIC SWITCH ................ OXY

PASSENGER MANUAL DROP OUT ........ PULL ON

[PASS OXY ON] - Illluminated

DESCEND .................. AS REQUIRED

HIGH DIFFERENTIAL PRESSURE

Cabin Differential Pressure exceeds 6.6 PSI

BLEED AIR  VALVES ........................... ENVIR OFF

OXYGEN (Crew & Passengers) ............ AS REQUIRED

DESCEND ........................ AS REQUIRED

AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE

[ALT WARN] ILLUMINATED

[PASS OXY ON] EXTINGUISHED

PASSENGER MANUAL DROP-OUT .............. PULL ON

BLEED AIR FAIL

[L BL AIR FAIL] or [R BL AIR FAIL]

BLEED AIR VALVE (affected engine) ...........PNEU & ENVIR OFF

[L BL AIR OFF] or [R BL AIR OFF] - ILLUMINATED

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.

Directional Control ..... Maintain using Rudder Pedals

Rudder Boost ..................................... OFF

UNSCHEDULED ELECTRIC ELEVATOR TRIM

ACTIVATION

Aircraft Attitude ..... Maintain using Elevator control

AP/Trim Disconnect ................ Depress fully & hold

[TRIM] - Illuminated

If a mistrim indication occurs for more than a few seconds:

Flight Controls ................ HOLD FIRMLY

(Control forces may exceed 25 pounds)

AP .................... DISENGAGE

AUTOPILOT TRIM FAIL

[TRIM]

Flight Controls ................... Hold Firmly

AP .................. DISENGAGE

If an Automatic Autopilot Disengagement Occurs:

Maintain Aircraft Control

AP/TRIM Disconnect ........ depress to first level to cancel horn.

HOT START OR HUNG START

If rate of ITT increase predicts an over temperature occurrence , or if N1 ceases to accelerate in a normal manner:

Condition Lever ............. Fuel Cutoff

Ignition and Engine Start ............ Starter Only (for remainder of starter time limit)

Ignition and Engine Start ............. Off

Do not attempt another start until cause the of the hot or hung start has been corrected.

 NO LIGHT START

If no ITT rise is observed within 10 seconds after moving the Condition Lever to Low Idle:

Condition Lever .............. Fuel Cutoff

Ignition and Engine Start ............... Off

Follow Engine Clearing Procedure

ENGINE CLEARING

Use the following procedure to remove internally trapped fuel and vapour, or if there is evidence of a fire within the engine.

Condition Lever ................ confirm Fuel Cutoff

Starter ........... Cool for 1 minute after previous start

Ignition & Engine Start .............. Starter Only

(for a maximum of 40 seconds)

Ignition & Engine Start ..................... Off

Starter ........... Cool for 1 minute before attempting another start.