Hot Start
1) CONDITION LEVERCUT-OFF / FEATHER Note Max ITT indicated
2) STARTER ON For 20 seconds observe ITT decrease
3) STARTER RESET
4) Monitor the engine during deceleration
Hung Start
1) Condition Lever CUT-OFF / FEATHER
2) Starter RESET
3) Monitor the engine during deceleration
4) Inform maintenance. A Dry Motoring Run procedure will be required
No Start
1) Condition Lever CUT-OFF / FEATHER
2) Starter RESET Inform maintenance. A Dry Motoring Run procedure will be required
Rejected Take-off (not engine related)
Engine Failure Before Rotation
ENGINE FAILURE AFTER ROTATION — LANDING GEAR DOWN
ENGINE FAILURE AFTER ROTATION — LANDING GEAR UP (TOTAL POWER LOSS)
ENGINE FAILURE IN FLIGHT — PARTIAL POWER LOSS
ENGINE FAILURE IN FLIGHT — TOTAL POWER LOSS
2. Condition Lever CUT-OFF - FEATHER
ENGINE FIRE — ON GROUND
ENGINE FIRE — IN FLIGHT
PROPELLER — LOW PITCH
PROPELLER OVERSPEED
2. AIRCRAFT SPEED REDUCE
PROPELLER UNDERSPEED IN FLIGHT
2. AIRCRAFT SPEED INCREASE
MAXIMUM RANGE DESCENT — AFTER ENGINE FAILURE — SINGLE BATTERY
MAXIMUM RANGE DESCENT — AFTER ENGINE FAILURE — DUAL BATTERY
MAXIMUM RATE DESCENT
COCKPIT-CABIN FIRE, SMOKE, OR FUMES
LOW FUEL PRESSURE
2. Fuel Pumps ON
BATTERY HOT
BATTERY THERMAL RUNAWAY
INVERTER FAILURE
CABIN PRESSURIZATION FAILURE
IF CABIN PRESSURE DIFF > 5.75 PSI
CABIN PRESSURIZATION FAILURE IF CABIN ALTITUDE > 10,700 ft