Memory Items Flashcards
Emergency Engine Shutdown Reasons
Torque increase unscheduled in flight
Engine fire
Engine failure
And Low Oil Pressure
EMERGENCY ENGINE SHUTDOWN
- Condition Lever IDLE
- Prop lever FEATHER
- Fuel FW Shutoff Valve. CLOSE
ENGINE FIRE ON GROUND
Affected Engine:
Condition Lever: FUEL CUTOFF
Fuel FW Shutoff Valve: CLOSE
ENGINE FAILURE DURING GROUND ROLL
POWER LEVERS: GROUND FINE
BRAKES: MAX AS REQUIRED TO ACHIEVE STOPPING PERFORMANCE
(If insufficient runway remains): CONDITION LEVERS: IDLE
FUEL FW SHUTOFF VALVE: CLOSE
MASTER SWITCH: OFF. (Gang bar down)
BOOST PUMPS: OFF
ENGINE FAILURE AFTER LIFTOFF
MAX CONTINUOUS POWER - SET
AIRSPEED - MAINTAIN T/O SPEED OR ABOVE
LANDING GEAR - UP
PROP - AFFECTED ENGINE FEATHER OR VERIFY FEATHERED
Airspeed - After obstacle clearance is reached - 108
Engine Failure In Flight below VMCA*
POWER. Reduce as required to maintain control
NOSE Lower to accelerate above VMCA
2nd Engine Flameout*
Power Lever. IDLE
Prop DO NOT FEATHER
Condition Lever FUEL CUTOFF
CONDUCT AIRSTART PROCEDURE IN ABNORMAL PROCEDURES
ELEC SMOKE OR FUMES
Oxygen System Control CONFIRM ON
Crew. DON MASKS
Mic, MASK
CABIN DOOR OPEN. *
Illuminated or suspected
All Occupants. SEATED WITH SEAT BELT SECURELY FASTENED
EMERGENCY DESCENT
Power Levers. IDLE Prop Levers HIGH RPM Flaps 184 knots max APPROACH Landing Gear DOWN Airspeed. 182 knots Max.
Glide*
Landing Gear. UP Flaps UP (Determine no restart) Props FEATHER Airspeed 125 KNOTS
Unscheduled electric elevator trim
MAINTAIN PITCH CONTROL WITH ELEVATOR
Control Wheel Trim Switch ATTEMPT TRIM IN OPPOSITE DIRECTION OF RUNAWAY
Elevator Trim Switch on 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
Oxygen System Control. CONFIRM ON
Crew. DON MASKS
High Differential Pressure
Cabin Alt Controller. SET HIGHER ALTITUDE SETTING
If condition persists:
Bleed Air Valves. CLOSED
Cabin Pressure (after cabin depressurized) DUMP
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 PUSH THE RELEASE BUTTON
PULL HANDLE AND PUSH OUT HATCH
Spins*
Control Column FULL FORWARD AILERONS NEUTRAL FULL RUDDER OPPOSITE DIRECTION OF SPIN Power Levers IDLE Rudder. NEUTRALIZE WHEN ROTATION STOPS EXECUTE A SMOOTH PULLOUT
Low oil pressure*
40-80 psi in the yellow arc
HOT OR HUNG START
Condition lever. FUEL CUTOFF
Engine Start Switch. STARTER ONLY FOR REMAINDER OF LIMIT
Engine Start Switch OFF
No Light Off Start
Condition Lever. FUEL CUTOFF
Engine Start Switch. OFF
Engine Failure on a published portion of an instrument approach
Power INCREASE TO MAINTAIN DESIRED AIRSPEED
Course MAINTAIN
Gear CONSIDERED
Flaps CONSIDERED
Inoperative Engine (gauges) IDENTIFIED. VERIFIED, FEATHERED
Smoke In Cockpit
Crew O2 System. CONFIRM ON
Crew DON MASKS
Microphone Switch SET TO MASK