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PSI PC12/47E > PC-12/47E Limitations > Flashcards

PC-12/47E Limitations Flashcards

1
Q

Engine

A

Pratt and Whitney PT6A-67P

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2
Q

Engine Type

A

Reverse Flow turboprop engine with 4 axial and 1 centrifugal compressor stages, combustion chamber, Compressor Turbine, 2 Power Turbines; Reduction Gear Box

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3
Q

Thermodynamic HP

A

1605

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4
Q

Shaft HP/takeoff power

A

1200

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5
Q

Max Ng

A

38967rpm @ 104%

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6
Q

Max Np Normal

A

1700rpm +/- 30rpm

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7
Q

Takeoff torque

A

44.34psi

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8
Q

Takeoff ITT

A

850C
5 Mins MAX

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9
Q

Climb Torque

A

44.34psi

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10
Q

Climb ITT

A

780C - PlaneSense Limit
820C - if Needed
820-850C 5 mins MAX

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11
Q

Transient Torque

A

61.0psi

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12
Q

Transient ITT

A

870C

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13
Q

Reverse Torque

A

34.25psi

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14
Q

Reverse ITT

A

760C

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15
Q

Min Battery before start

A

24V

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16
Q

Max ITT before start

A

150C

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17
Q

Starting ITT up to 850C

A

no time limit

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18
Q

Starting ITT 850C to 870C

A

20 seconds

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19
Q

Starting ITT 870C to 1000C

A

5 seconds

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20
Q

Above 1000C on start

A

HOT START

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21
Q

Propeller Manufacture

A

Hartzell

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22
Q

Number of blades

A

4 Aluminum
5 Composite

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23
Q

Propeller diameter

A

105”

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24
Q

Propeller max normal Np

A

1700rpm

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25
Q

Overspeed governor

A

1802rpm

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26
Q

Nf governor

A

1853rpm

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27
Q

Max transient Np

A

1870rpm

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28
Q

Max reverse Np

A

1650rpm

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29
Q

Ground operation not permitted Np

A

350-950rpm

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30
Q

Fuel Types

A

Jet A, Jet A-1, Jet B, JP-4 all with Prist

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31
Q

Total Fuel (gal/lbs)

A

406.8 US gal / 2736.5lbs

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32
Q

Usuable Fuel (gal/lbs)

A

402 US gal / 2703.6lbs

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33
Q

Max fuel Imbalance for Takeoff

A

26.4 US gal / 178lbs
3 Bars

34
Q

Oil Capacity

A

3.6 US gal

35
Q

Max Ramp Weight

A

10495 lbs

36
Q

Max Takeoff Weight

A

10450 lbs

37
Q

Max Landing Weight

A

9921 lbs

38
Q

Max Zero Fuel Weight

A

9039 lbs

39
Q

Max Baggage

A

400 lbs

40
Q

Cabin Area Max

A

3300 lbs

41
Q

Vr 15 flaps

A

82

42
Q

Vr 30 flaps (short field)

A

76

43
Q

Vx

A

120

44
Q

Vy 0 flaps

A

130 @ Sea Level
125 @ 5000ft

45
Q

Vy 15 flaps

A

95

46
Q

Vy 30 flaps

A

85

47
Q

10000 climb speed

A

160

48
Q

20000 climb speed

A

140

49
Q

30000 climb speed

A

120

50
Q

Pusher ice climb 0 flaps

A

135

51
Q

Vmo

A

240

52
Q

Vfe flaps 15

A

165

53
Q

Vfe flaps 30/40

A

130

54
Q

Vlo

A

180

55
Q

Vle

A

240

56
Q

emergency gear extension (hydrolic/electric)

A

110/120

57
Q

Approach Speed flaps 0

A

120

58
Q

Approach Speed flaps 15

A

99

59
Q

Approach Speed flaps 30

A

89

60
Q

Approach Speed flaps 40

A

85

61
Q

Pusher ice approach speed, 15 flaps

A

105

62
Q

go around speed 15 flaps

A

98

63
Q

go around speed 30 flaps

A

89

64
Q

go around speed 40 flaps

A

86

65
Q

Max demonstrated Crosswind (contaminated)

A

30,25,20,15 (50% reduction)

66
Q

Max tailwind T.O or Land

A

10

67
Q

Max tailwind LAHSO

A

3

68
Q

Cruise Torque

A

36.9PSI

69
Q

Cruise ITT

A

820C

70
Q

Reverse Np

A

1650RPM

71
Q

Vlo

A

180Kts

72
Q

Vle

A

240Kts

73
Q

Vfe

A

15deg - 165KIAS
>15deg - 130KIAS

74
Q

Vmo

A

240 KIAS

75
Q

Vo

A

166KIAS Max Gross
123KIAS 5730lbs
other speeds in back of in-flight guide

76
Q

Generators

A

2 - 300A/ea
450A max (2 mins/hr)
Gen 2 is also Starter

77
Q

OAT Limits

A

-55C Min
-40C Boots Min
+40C Boots Max
+50C Max

78
Q

Cabin Pressure Limit

A

5.75PSI Differential
6.0PSI Yellow CAS
6.35PSI Red CAS
10,500 Red CAS

79
Q

Crosswind Limits

A

Flaps 0 - 30 KTS
Flaps 15 - 25KTS
Flaps 30 - 20KTS
Flaps 40 - 15KTS
Contaminated RWY (RCAM 3 or less)
Cut limits in half

80
Q

Vlo (emergency)

A

110KTS Hyd
120KTS Elec

81
Q

Starting Proceedure (NG)

A

Prop turning
Pressure rising (oil)
Pumps on
Ng >13%
ITT <150c
Cond Lever to Grnd Idle

PSI PC12/47E (7 decks)

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