PC-12 EMERGENCY PROCEDURES Flashcards

0
Q

ENGINE FAILURE BEFORE ROTATION (6)

A

1 PCL - Idle
2 Braking - as required

If aircraft cannot be stopped or collision is likely

3 condition lever - cut off feather
4 Fuel emergency lever - Pull
5 Gangbar - operate
6 after aircraft has stopped - evacuate

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1
Q

REJECTED TAKE OFF ( NON ENGINE RELATED ) (8)

A

1 PCL - Idle
2 Reverse - as required
3 Braking - as required

if aircraft cannot be stopped in time

4 PCL - Idle 
5 Condition Lever - Idle 
6 Fuel Emergency lever - PULl
7 Gangbar - Operate 
8 After aircraft has stopped - Evacuate
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2
Q

ENGINE FAILURE AFTER ROTATION ( LANDING GEAR DOWN ) (8)

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 - 98/15
84/40
4 PCL - Idle
5 Condition lever - cut off feather
6 Fuel emergency shut off - pull

After touchdown

7 Gangbar - operate
8 After aircraft has stopped - evacuate

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3
Q

ENGINE FAILURE AFTER ROTATION ( LANDING GEAR UP ) (9)

A
1 Landing gear - down 
2 Non essential buss override switch - override 
3 Flaps - 40 
4 Final approach speed -  98/15 flaps 
                                          89/40 flaps 
5 PCL - Idle 
6 Condition lever - cut off feather 
7 Fuel Emergency lever - pull 

after touchdown
8 Gangbar - operate
9 after aircraft has stopped - Evacuate

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4
Q

ENGINE FAILURE IN FLIGHT ( PARTIAL POWER LOSS ) (6)

A

1 PCL - Idle
2 MOR lever - pull forward and move slowly until engine responds, wait and let engine stabilize.

If engine compressor stalls and of ITT is exceeded

3 MOR lever - retard then move forward very slowly

If engine falls below 50% NG

4 starter - push for 2 seconds
5 MOR - lever forward to required power of NG > 80%
6 Land as soon as practical

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5
Q

PROPELLER - LOW PITCH (3)

A

1 PCL - Idle

IF IT IS NOT POSSIBLE RO MAINTAIN FLIGHT

2 Condition lever - CUT OFF FEATHER
3 Carry out - Emergency decent landing or final approach.

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6
Q

PROPELLER UNDER SPEED (2)

A

1 PCL - INCREASE POWER

2 AIRCRAFT SPEED - INCREASE

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7
Q

MAXIMUM RANGE DECENT ( AFTER ENGINE FAILURE ) (7)

A

1 PCL - IDLE
2 CONDITION LEVER - CUT OFF FEATHER
3 AIRCRAFT - GEAR AND FLAPS UP
4 SPEED - BEST GLIDE SPEED 114KIAS
5 ALL OCCUPANTS - CHECK SEAT BELTS
6 OXYGEN MASKS - PREPARE TO PUT ON BEFORE CABIN ALTITUDE EXCEEDS 10 000
7 PASSENGERS OXYGEN - AUTO CHECK CONTENTS AND TIME

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8
Q

ENGINE FIRE ( ON THE GROUND ) (9)

A
1 PCL -  IDLE 
2 CONDITION LEVER - CUT OFF FEATHER 
3 ECS EMERGENCY SHUT OFF - PULL 
4 FUEL EMERGENCY SHUT OFF - PULL 
5 RADIO - MAKE AN EMERGENCY CALL
6 ELECTRICAL POWER - OFF USE GANG BAR
7 PARKING BREAK - OFF 
8 AIRCRAFT -  EVACUATE 
9 FIRE - EXTINGUISH
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9
Q

ENGINE FIRE IN FLIGHT (7)

A
1 ENGINE POWER - REDUCE TO MINIMUM ACCEPTABLE
2 ECS EMERG - PULL 
3 OXYGEN MASK -  ON ALL OCCUPANTS
4 PASSENGER OXYGEN SELECTOR - ON
5 CONFIRM FIRE EXISTS : IF FIRE EXISTS 

6 FUEL EMERG SHUT OFF - PULL
7 CONDITION LEVER - CUT OFF

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10
Q

COCKPIT/ CABIN FIRE, SMOKE FUMES AND SMOKE EVACUATION (7)

A

1 OXYGEN MASK - ON
2 CREW OXYGEN - 100%
3 PASSENGER OXYGEN SELECTOR - ON
4 PASSENGERS - INSTRUCT TO DON MASK
5 AIRCRAFT - INITIATE DECENT BELOW 10,000 OR MSA WHICHEVER IS HIGHER
6 AIRCRAFT - PROCEED TO NEAREST AIRPORT

IF SMOKE EVACUATION IS REQUIRED

ECS EMERG PULL
CABIN PRESS DUMP 
WHEN CABIN PRESSURE IS ZERO 
DV OPEN 
FANS ON 
7 FIRE EXTINGUISHER - USE IF REQUIRED
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11
Q

MAXIMUM RATE DECENT (6)

A

1 PCL - IDLE
2 LANDING GEAR - BELOW 177KIAS SELECT DOWN
3 AIRCRAFT SPEED - 236 VMO
4 ALL OCCUPANTS - CHECK SEAT BELTS
5 OXYGEN MASKS - PREPARE TO PUT ON BEFORE CABIN ALT EXCEEDS 10,000 ft
6 PASSENGER OXYGEN - AUTO CHECK CONTENTS AND DURATION

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12
Q

ELECTRICAL TRIM RUNAWAY (4)

A

1 TRIM INTERRUPT SWITCH - INTR
2 CB OF FAILED TRIM - PULL
3 TRIM INTERRUPT SWITCH - NORM
4 IF MAIN STABILIZER TRIM HAS FAILED - USE ALTERNATE TRIM

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13
Q

INADVERTENT PUSHER OPERATION (3)

A

1 CONTROL WHEEL - HOLD AGAINST PUSHER OPERATION
2 PUSHER INTERRUPT SWITCH - PRESS AND HOLD
3 PSUHER SYS CB - PULL

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14
Q

INADVERTENT SHAKER OPERATION (1)

A

1 AOA - DECREASE

2 IAS - INCREASE

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15
Q

BATTERY HOT (3)

A

1 OVERHEAD PANEL - IDENTIFY THE BATTERY OVER TEMP IF SECOND BATTERY IS INSTALLED
2 BATTERY CHARGE CURRENT - CHECK
IF BATTERY CURRENT IS HIGH
3 BATTERY - OFF

16
Q

BATTERY THERMAL RUNAWAY (2)

A

1 OVERHEAD PANEL - IDENTIFY THE BATTERY OVER TEMP ID SECOND BATTERY IS INSTALLED
2 BATTERY - OFF

17
Q

INVERTER FAILURE (1)

A

1 INVERTER SWITCH - SELECT ALTERNATE INVERTER

18
Q

LOWE FUEL PRESSURE (2)

A

1 POWER - REDUCE TO A MINIMUM

2 FUEL PUMPS - ON

19
Q

CABIN PRESSURIZATION FAILURE

A

1 PRESSURE INDICATOR - CHECK
A - IF CABIN DIFF IS > 5.75 go to checklist

B - IF CABIN ALTITUDE > 10,700

1 OXYGEN MASK - ON
2 PASSENGER OXYGEN SELECTOR - ON
3 PASSENGERS - INSTRUCT TO DON MASK

20
Q

PASSENGER AND CARGO DOOR CAWS WARNING IN FLIGHT (1)

A

1 ALL OCCUPANTS - CHECK SEAT BELTS ARE FASTENED

21
Q

STALL

CLEAN CONFIG

A

1 MAX POWER

2 ANGLE OF ATTACK DECREASE

22
Q

STALL

LANDING CONFIG - FLAPS 40, LANDING GEAR DOWN

A
1 PCL MAX POWER 
2 AMGLE OF ATTACK DECREASE
3 FLAPS 15
4 GEAR UP 
5 AIRCRAFT CLIMB TO REGAIN ANY LOSS ALTITUDE 
6 UP THROUGH 100 KIAS
23
Q

STALL

APPROACH TO LANDING FLAPS 15 , GEAR DOWN

A
1 PCL MAX POWER 
2 AIRCRAFT LVEVEL THE WINGS SIMULTANEOUS ADDING POWER  
3 ANGLE OF ATTACK DECREASE 
4 FLAPS CONFIRM 15
5 GEAR UP 
6 AIRCRAFT REGAIN ANY LOSS ALTITUDE 
7 FLAPS UP THROUGH 100 KIAS