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Pilatus PC-12 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Takeoff Weight

A

10,450

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2
Q

Max Landing Weight

A

9,921

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3
Q

Max Zero Fuel Weight

A

9,039

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4
Q 
Max Cargo Weight
Baggage Area
Cabin Area
Floor loading on seat rails
Floor loading on cabin floor
A

Baggage Area: 400
Cabin Area: 3,300
Floor loading on seat rails: 205 lb/ft sq
Floor loading on cabin floor: 125 lb/ft lb

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5
Q 
Shaft Horsepower
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
Shaft Horsepower
Takeoff: 1200
Max Continuous: 1200
Cruise: 1000
Min Idle:
Starting:
Transient (20 sec): 
Max Reverse: 900
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6
Q 
Torque
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
Torque
Takeoff: 44.34
Max Continuous: 44.34
Cruise: 36.95
Min Idle:
Starting:
Transient (20 sec): 61.0
Max Reverse: 34.25
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7
Q 
Max ITT
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
Max ITT
Takeoff: 850
Max Continuous: 820
Cruise: 820
Min Idle: 750
Starting: 1000
Transient (20 sec): 870
Max Reverse: 760
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8
Q 
NG%
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
NG%
Takeoff: 104
Max Continuous: 104
Cruise: 104
Min Idle: 50.7 ground / 64 flight
Starting:
Transient (20 sec): 104
Max Reverse:
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9
Q 
NP
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
NP
Takeoff: 1700
Max Continuous: 1700
Cruise: 1700
Min Idle: 
Starting:
Transient (20 sec): 1870
Max Reverse: 1650
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10
Q 
Oil Pressure
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
Oil Pressure
Takeoff: 90-135
Max Continuous: 90-135
Cruise: 90-135
Min Idle: 60 min
Starting: 200 Max
Transient (20 sec): 40-200
Max Reverse: 90-135
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11
Q 
Oil Temp (deg C)
Takeoff:
Max Continuous:
Cruise:
Min Idle:
Starting:
Transient (20 sec):
Max Reverse:
A 
Oil Temp (deg C)
Takeoff: 10-110
Max Continuous: 10-105
Cruise: 10-105
Min Idle: (-40)-110
Starting: (-40 Min)
Transient (20 sec): (-40) x 110
Max Reverse: 10-105
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12
Q

Fuel
Approved types
Total Capacity
Usable

A

Fuel
Approved types: Jet A, A-1, B, JP-4, other fuels in Pratt & Whitney service bulletin 14004.

Total Capacity: 406.8 gal
Usable: 402 gal

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13
Q 
Airspeed Limitations
VMo / Mmo
Vfe  0 flaps
Vfe  15 flaps
Vlo
Vle
A 
Airspeed Limitations
VMo / Mmo: 240 / .48
Vfe  0 flaps: 165
Vfe  15 flaps: 130
Vlo: 180
Vle: 240
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14
Q

Generator
Max continuous load
Max load 2 minutes

A

Generator
Max continuous load: 300 amp
Max load 2 minutes: 450 amp

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15
Q

Load factor
Flaps up
Flaps down

A

Load factor
Flaps up: 3.3g -1.32g
Flaps down: 2.0g 0g

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16
Q

Outside Air Temperature
Min
Max

A

Min: -55 C
Max: + 50 C

17
Q

Cabin Pressure
Max
Landing Max

A

Max: 5.75 psi

Landing Max: 0.7 psi

18
Q

Max Rate of Climb

A 
>= 15 flaps: 85 kias
15 flaps: 95
Sea level: 130
5k: 125
15k: 125
20k: 120
30k: 120
19
Q

Max Ramp Weight

A

10,495

20
Q

Oil Quantity
Total oil capacity
Drain and Refill qty
Oil qty operating range

A

Oil Quantity
Total oil capacity: 3.6 gal
Drain and Refill qty: 2.0 gal
Oil qty operating range: 1.0 gal

21
Q 
Landing approach speed; X-wind limits
Flaps 0:   X-Wind:   KIAS:
Flaps 15:   X-wind:   KIAS:
Flaps 30:   X-wind:   KIAS:
Flaps 40:   X-wind:   KIAS:
A 
Landing approach speed; X-wind limits
Flaps 0:   X-Wind: 30KIAS: 120
Flaps 15:   X-wind: 25  KIAS: 99
Flaps 30:   X-wind: 20  KIAS: 89
Flaps 40:   X-wind: 15  KIAS: 85
22
Q

Vr, Vx, Vy

A 
Vr 15: 82
Vr 30:  76
Vx: 120
Vy: Sea Level - 5k: 130
       5k-20k: 125
       > 20k:   120
23
Q

Oxygen Pressure

A

1850-2000 psi max

Pilatus PC-12 (4 decks)

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