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Pilatus PC12/47 > Emergencies > Flashcards

Emergencies Flashcards

1
Q

Hot Start

A

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

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2
Q

Hung Start

A

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

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3
Q

No Start

A

1) Condition Lever CUT-OFF / FEATHER

2) Starter RESET Inform maintenance. A Dry Motoring Run procedure will be required

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4
Q

Rejected Take-off (not engine related)

A
  1. PCL IDLE
  2. Reverse As required
  3. Braking As required
    IF AIRCRAFT CANNOT BE STOPPED ON THE REMAINING RUNWAY:
  4. PCL IDLE
  5. Condition Lever CUT-OFF - FEATHER
  6. Fuel Emergency Shut Off Press latch down and pull lever up
  7. Gangbar or (MASTER) Operate
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5
Q

Engine Failure Before Rotation

A
  1. PCL IDLE
  2. Braking As required
    IF RUNWAY OVERRUN OR COLLISION IS LIKELY, THEN:
  3. Condition Lever CUT-OFF - FEATHER
  4. Fuel Emergency Shut Off Press latch down and pull lever up
  5. Gangbar or (MASTER) Operate
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6
Q

ENGINE FAILURE AFTER ROTATION — LANDING GEAR DOWN

A
  1. If altitude is not sufficient to select a runway or field Land straight ahead, turning only to avoid obstructions
  2. Flaps 40°
  3. Final approach speed
  4. Airspeed 98 KIAS, Flaps 15°
    84 KIAS, Flaps 40°
  5. PCL IDLE
  6. Condition Lever CUT-OFF/ FEATHER
  7. Fuel Emergency Shut Off Press latch down and pull lever up
    AFTER TOUCHDOWN:
  8. Gangbar or (MASTER) Operate
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7
Q

ENGINE FAILURE AFTER ROTATION — LANDING GEAR UP (TOTAL POWER LOSS)

A
  1. Landing Gear DOWN
  2. N ESNTL Bus Override Switch OVERRIDE
  3. Flaps 40°
  4. Airspeed 98 KIAS, Flaps 15°
    84 KIAS, Flaps 40°
  5. PCL IDLE
  6. Condition Lever CUT-OFF / FEATHER
  7. Fuel Emergency Shut Off Press latch down and pull lever up
    AFTER TOUCHDOWN:
  8. Gangbar or (MASTER) Operate
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8
Q

ENGINE FAILURE IN FLIGHT — PARTIAL POWER LOSS

A
  1. PCL IDLE
  2. MOR LeverPull upwards and move slowly forward until engine responds wait and let engine stabilize.
    IF ENGINE COMPRESSOR STALLS AND-OR ITT IS EXCEEDED:
  3. MOR Lever Retard and move very slowly forward
    IF ENGINE FALLS BELOW 50% Ng:
  4. Starter Push for 2 seconds
    5.MOR Lever Move forward to required power (Ng > 80%)
    6.Land as soon as practical.
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9
Q

ENGINE FAILURE IN FLIGHT — TOTAL POWER LOSS

A
  1. PCL IDLE

2. Condition Lever CUT-OFF - FEATHER

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10
Q

ENGINE FIRE — ON GROUND

A
  1. PCL IDLE
  2. Condition Lever CUT-OFF / FEATHER
  3. ECS Emergency Shut Off PULL
  4. Fuel Emergency Shut Off Press latch down and pull lever up
  5. Radio Make Emergency Call (SOB, Fuel, DGoods)
  6. Electrical Power OFF (Use GANGBAR)
  7. Parking Brake OFF (if possible)
  8. Aircraft Evacuate
  9. Fire Extinguish (if possible)
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11
Q

ENGINE FIRE — IN FLIGHT

A
  1. Engine Power Reduce to minimum acceptable according to flight situation
  2. ECS Emergency Shut Off PULL
  3. Oxygen Masks ON
  4. Passenger Oxygen Selector ON
  5. Confirm that a Fire Exists
    If fire exist:
  6. Fuel Emergency Shut Off PULL
  7. Condition Lever CUT-OFF / FEATHER
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12
Q

PROPELLER — LOW PITCH

A
  1. PCL Ensure Forward of Idle Detent
    IF IT IS NOT POSSIBLE TO MAINTAIN SPEED AND HEIGHT:
  2. Condition Lever CUT-OFF - FEATHER
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13
Q

PROPELLER OVERSPEED

A
  1. PCL REDUCE POWER

2. AIRCRAFT SPEED REDUCE

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14
Q

PROPELLER UNDERSPEED IN FLIGHT

A
  1. PCL INCREASE POWER

2. AIRCRAFT SPEED INCREASE

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15
Q

MAXIMUM RANGE DESCENT — AFTER ENGINE FAILURE — SINGLE BATTERY

A
  1. PCL IDLE
  2. Condition Lever CUT-OFF-FEATHER (feather prop)
  3. Aircraft Configuration Landing Gear up and Flaps 0°
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16
Q

MAXIMUM RANGE DESCENT — AFTER ENGINE FAILURE — DUAL BATTERY

A
  1. PCL IDLE
  2. Condition Lever CUT-OFF-FEATHER (feather prop)
  3. Aircraft Configuration Landing Gear up and Flaps 0°
17
Q

MAXIMUM RATE DESCENT

A
  1. PCL IDLE
  2. Landing Below 177 KIAS Gear DOWN
  3. Aircraft Speed Vmo / Mmo
  4. Oxygen Masks Prepare. Put on before cabin altitude exceeds 12,500 ft
  5. Passenger Oxygen Auto.
    Check contents. Calculate oxygen duration and check flow to passengers.
18
Q

COCKPIT-CABIN FIRE, SMOKE, OR FUMES

A
  1. Oxygen Masks ON (all occupants)
  2. Crew Oxygen 100%
  3. Passenger Oxygen Selector ON
  4. If at Altitude, Initiate a Descent to below 12,500 ft.
  5. Smoke Evacuation Procedure (Refer to EMERGENCY Procedures Carry out if required (SOP Page 71).
  6. Fire Extinguisher Use if required
  7. Proceed to Nearest Airfield
19
Q

LOW FUEL PRESSURE

A
  1. Power Reduce to minimum to sustain flight

2. Fuel Pumps ON

20
Q

BATTERY HOT

A
  1. Overhead Panel Identify the battery overtemp (if second battery installed)
  2. Battery charge Check current
    IF CHARGE CURRENT IS HIGH:
  3. Battery OFF (Do not select ON again)
21
Q

BATTERY THERMAL RUNAWAY

A
  1. Overhead Panel Identify the battery overtemp (if second battery installed)
  2. Battery OFF
22
Q

INVERTER FAILURE

A
  1. Inverter switch (Overhead) Select alternate inverter
23
Q

CABIN PRESSURIZATION FAILURE

IF CABIN PRESSURE DIFF > 5.75 PSI

A
  1. Pressure Indication Check
24
Q

CABIN PRESSURIZATION FAILURE IF CABIN ALTITUDE > 10,700 ft

A
  1. Oxygen Masks ON
  2. Passenger Oxygen Selector AUTO/ON
  3. Passengers INSTRUCT to don masks
25
Q

INADVERTENT PUSHER OPERATION

A
  1. Control Wheel HOLD against Pusher action
  2. PUSHER INTR Switch PRESS and HOLD
  3. PUSHER SYS CB PULL (CB - L B3)
26
Q

INADVERTENT SHAKER OPERATION

A
  1. AOA Decrease

2. IAS Increase

27
Q

ELECTRICAL TRIM RUNAWAY

A
  1. TRIM INTERRUPT Switch INTR
  2. CB of failed trimPULL
    STAB TRIM and AILERON TRIM CB - L A1 and L B1
    STAB ALTERNATE and CB - R A1 and R B1
    RUDDER TRIM
  3. TRIM INTERRUPT Switch NORM

Pilatus PC12/47 (6 decks)

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