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Pilatus PC-12 > Emergencies & Limitations > Flashcards

Emergencies & Limitations Flashcards

1
Q

MAX. CONTINUOUS

ITT & Torque

A

760 ITT

36.95 PSI

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2
Q

Engine Failure After Rotation - Landing Gear Down

A

A. If TOTAL Power Loss:

If insufficient altitude for a runway or field

  1. Land straight ahead, turning only to avoid obstructions
  2. Flaps - 40 degrees
  3. Final Approach Speed - 84 KIAS
  4. PCL - Idle
  5. Condition Lever - Cut-off/Feather
  6. FUEL EMERG SHUT OFF - Press latch down, pull lever up
    * *AFTER Touchdown:**
  7. MASTER POWER Switch - Emergency Off

**AFTER the Aircraft has Stopped **

  1. Aircraft - EVACUATE
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3
Q

Maximum Maneuvering Speed

A

126 KIAS Empty

158 KIAS at Max Gross

(Add approx 10 Kts per 1,000#)

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3
Q

Air Start - with starter

A
  1. PCL - Idle
  2. Condition Lever - Cut-off/feather
  3. Fuel Emerg shut off - Full In
  4. Electrical Loads - Reduce (may omit if time is short)
  5. ECS switch - OFF (may omit if time is short)
  6. Gen 1 and 2 - OFF
  7. Battery switch - ON
  8. Air start envelope - Check
  9. Starter switch - Push for 2 sec
  10. Ignition switch - ON
  11. Condition lever (Ng > 13%) - Ground Idle
  12. ITT and Ng - Monitor

When engine has relit and Ng > 60%

  1. Ignition switch - Auto
  2. Condition lever - Flight Idle
  3. Gen 1 and 2 switches - ON
  4. Electrical equip - As required
  5. ECS switch - Auto
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4
Q

Engine Failure In Flight - Total Power Loss

A
  1. PCL - Idle
  2. Condition Lever - Cut-off/Feather
  3. Fuel - Check
  4. Airstart (next page)
  5. If above 13,500’ - Emergency Descent
    * If Airstart is not successful*
  6. Forced Landing
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4
Q

Maximum Range Descent After Engine Failure, Single Battery

A
  1. PCL - Idle
  2. Condition Lever - Cut-off/Feather
  3. Aircraft Configuration - Landing gear up and flaps 0
  4. Speed - 114 KIAS @ 9921 (less 5kts / 1,000lbs)
    - 93 KIAS @ 6,400 (empty)
  5. Autopilot - Engage NAV or HDG and IAS Hold
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5
Q

STARTING Max ITT

A

1000 ITT MAX

(5 sec Max)

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6
Q

Max Fuel Imbalance

A

3 LCD Segments

= 26.4gal

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7
Q

Baggage Compartment

Max Wt

A

400 lbs

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8
Q

Starter Ops Limits

A

Sequence - 60 sec Off

Sequence - 60 sec Off

Sequence - 30 minutes Off

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9
Q

Engine Failure Before Rotation

A
  1. PCL - Idle
  2. Braking - As required
    * *IF runway overrun or collision likely:**
  3. Condition Lever - Cut-off/Feather
  4. FUEL EMERG SHUT OFF - Press latch down, pull lever up
  5. MASTER POWER Switch - Emergency Off
  6. Aircraft - Evacuate
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10
Q

Flaps settings -

In Icing Conditions

A

Max 15 flaps (boots working).

0 flaps (Boots Inop).

Do Not Retract flaps from 15 if residual ice exists.

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10
Q

Rejected Takeoff (Not Engine Related)

A
  1. PCL - Idle
  2. Reverse - As Required
  3. Braking - As Required
    * *If you cannot stop on remaining runway:**
  4. PCL - Idle
  5. Condition Lever - Cut-off/Feather
  6. FUEL EMERG SHUT OFF - Press latch down, pull lever up
  7. MASTER POWER Switch - Emergency Off
  8. Aircraft - Evacuate
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11
Q

Maximum landing gear extended speed - VLE

A

236 KIAS

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11
Q

Engine Fire - In Flight

A
  1. Engine Power - Reduce to minimum acceptable
  2. ECS EMERG SHUT OFF - Pull
  3. Oxygen Masks - ON (All occupants)
    1. Passenger Oxygen Selector - ON
      1. Confirm that fire exists
      2. FUEL EMERG SHUT OFF - Press latch down, pull lever up
      3. Condition Lever - Cut-off/Feather*

8. Emergency Descent and/or Emergency Landing

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12
Q

TRANSIENT Max

ITT & Torque

A

870 ITT

61.00 PSI

12
Q

TAKEOFF

Max ITT & Torque

A

800 ITT

44.34 PSI

12
Q

Engine Failure After Rotation, Landing Gear Up

A

A. If Total Power Loss:

  1. Landing Gear - Down
  2. N ESNTL Bus Switch - Override (restore Hyd Ctrl)
  3. Flaps - 40 degrees
  4. Final Approach Speed -

98 KIAS - Flaps 15

84 KIAS - Flaps 40

  1. PCL - Idle
  2. Condition Lever - Cut-off/Feather
  3. FUEL EMERG SHUT OFF - Press latch down, pull lever up
    * *AFTER Touchdown**:
  4. MASTER POWER Switch - Emergency Off
13
Q

Propeller - Low Pitch

Voice callout “Warning, Prop Low Pitch.”

Conditions: Possible excessive propeller speed or height loss. Propeller has gone to a low pitch (below minimum in flight pitch) with Aircraft not on the ground.

A
  1. PCL - Ensure forward of idle detent
  • *IF not possible to maintain speed and altitude:**
    2. Condition Lever - Cut-off/Feather
  1. Emergency Descent
  2. Emergency Landing
15
Q

Pneumatic Boots

A

Ops Range

-40C to +40C

17
Q

Pax Seating

A

Leave seats 5, 6, 7 and 8 vacant

during takeoff and landing

unless seat in front is occupied

18
Q

Autopilot Malfunction

A

Accomplish Items 1 and 2 simultaneously:

  1. Airplane Control Wheel - Grasp Firmly and regain control
  2. Autopilot Disengage Switch - PRESS
  3. Aircraft - RETRIM manually

4. Autopilot Circuit Breaker - PULL RR2

19
Q

Propeller - Underspeed - In Flight

EIS Caution, propeller digits blink 40/min

Propeller speed below 1,640 RPM

A

EIS and Master Caution, propeller lights blink 40/min
Propeller speed below 1640

  1. PCL - Increase Power
  2. Aircraft Speed - Increase
21
Q

MIN. IDLE ITT & Ng

A

750 ITT.

  1. 7 Ng (Gnd Idle).
  2. 0 Ng (Flt Idle)
22
Q

Maximum operating speed

A

236 KIAS

0.48 Mach

23
Q

Engine Fire - On Ground

A
  1. PCL - Idle
  2. Condition Lever - Cut-off/Feather
  3. ECS EMER SHUT OFF - Pull
  4. FUEL EMERG SHUT OFF - Press latch down, pull lever up
  5. Radio - Emergency Call
  6. MASTER POWER Switch - Emergency Off
  7. Parking Brake - OFF (IF possible)
  8. Aircraft - Evacuate
  9. Fire - Extinguish
24
Q

Autopilot

A

Altitude Select captures below 1000 feet AGL are prohibited.

Must be disengaged below 200 feet AGL during ILS approach

26
Q

Total Usable Fuel

A

402 gal

27
Q

Generator Limits

A

Gen 1 - 300 max cont. / 450 (2 min)

Gen 2 - 115 max cont.

28
Q

Partial Power Loss in Flight

A
  1. PCL - Idle
  2. Manual Override Lever - Pull upwards and move slowly forward, until engine responds, wait and let engine stabilize.

If engine compressor stalls and/or ITT exceeded:

  1. Manual override lever - Retard and move very slowly forward.

IF engine falls below 50% Ng or accelerates very slowly, with ITT at limit (870°C / 20 seconds) or compressor stall:

  1. Starter switch - Push for 2 seconds
  2. Manual override lever - Move forward to required power (Ng > 80%)
  3. Land as soon as practical
  4. Manual override lever - Maintain at least 75% Ng

After touch down:

  1. Condition lever - Cut-off / feather
29
Q

Maximum landing gear operating speed - VLO

A

177 KIAS

30
Q

Maximum Rate Descent

A
  1. PCL - Idle
  2. Landing Gear - Down (Below 177 kias)
  3. Aircraft Speed - Mmo/Vmo
  4. Oxygen Masks - Put on before cabin altitude exceeds 10,000 ft

**CAUTION: In turbulence reduce speed to 170 KIAS **

31
Q

Inadvertent Pusher

A
  1. Control Wheel - HOLD against pusher action
  2. PUSHER INTR Switch - PRESS and HOLD
  3. PUSHER SYS Circuit Breaker - Pull LB3 LC3
33
Q

MAX Ng

A

104

34
Q

REVERSE

Max ITT & Torque

A

760 ITT

34.25 PSI

1650 Max Np

36
Q

Maximum flap extended speed - VFE

A

163 - Flaps 15

130 - Flaps > 15

37
Q

Propeller - Overspeed

Indications: EIS caution and prop digits blinking 40/min

or EIS and Master Warning, prop digits blinking 80/min.

Propeller speed above 1,760 RPM.

A
  1. PCL - Reduce Power
  2. Airspeed - Reduce
38
Q

Trim Runaway

A
  1. TRIM INTERRUPT Switch - INTR
  2. CB of Failed Trim - Pull

STAB TRIM & AIL TRIM - LA1 LB1

STAB ALTN & RUD TRIM - RA1 RB1

  1. TRIM INTERRUPT Switch - NORM

Pilatus PC-12 (3 decks)

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