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Tempus Jets > PC-12NG Limitations > Flashcards

PC-12NG Limitations Flashcards

1
Q

VMO- Max operating speed

A

240 KIAS

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2
Q

MMO - Max operating mach

A

0.48 M

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3
Q

VO (VA)- Max Operating Maneuvering speed

A

123 - 166 Do not make full or abrupt control movements above this speed

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4
Q

VFE - Max flap extended speed

A

00 - 150 Flap: 165 150- 400 Flap: 130

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5
Q

VLO- Max ldg gear operating speed

A

180 - Do not retract or extend landing gear above this speed

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6
Q

VLE - Max speed with leg extended

A

240 - do not exceed this speed with landing gear extended

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7
Q

Propeller Speeds

A
  • 1,700 Max normal ops
  • 1,870 Max transient (2 sec)
  • 1,650 Max reverse
  • Stabilized on ground between 350 and 950 is not permitted
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8
Q

Max Q: T/O, Continous, Climb

A

44.34 psi

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9
Q

Max Cruise Q

A

36.95 psi

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10
Q

Transient Q

A

61 psi (20 sec max)

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11
Q

Max Reverse Q

A

34.25 psi

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12
Q

Max ITT T/O

A

850 (5 min)

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13
Q

Max cont./climb ITT

A

820

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14
Q

Max ITT cruise

A

820

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15
Q

Min. Idle ITT

A

750 (50.7% - 61.4% Ng)

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16
Q

Max ITT Start

A

1000 (5 sec max)

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17
Q

Transient ITT

A

870 (20 sec max)

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18
Q

Max ITT Reverse

A

760

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19
Q

Max Ng T/O

A

104 (5 min)

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20
Q

Max Cont./Climb Ng

A

104

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21
Q

Max Ng Cruise

A

104

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22
Q

Min Idle Ng

A

50.7 (GI), 64 (FI)

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23
Q

Transient Ng

A

104

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24
Q

Max Np Takeoff

A

1700 (5 min)

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25
Q

Max Np Cont./Climb

A

1700

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26
Q

Max Np Cruise

A

1700

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27
Q

Max Np Transient

A

1870 (20 sec)

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28
Q

Max Np Reverse

A

1650

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29
Q

Oil Temp Limits

A

-40 to 105, 105 -110 limited to 10 minutes

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30
Q

Oil Temp reverse

A

10 to 105

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31
Q

Generator Loads

A

Max cont. 300, Max Load (2 min) 450

32
Q

Starter limits

A

Auto start cycle, then… 1. 60 sec off, 2. 60 sec off, 3. 30 min off

33
Q

PCL aft of idle detent is not permitted:

A
  • Engine not running
  • During flight
  • When engine is controlled by manual override
34
Q

Chip Detector

A

T/O not permitted w/ CHIP annunciator illuminated

35
Q

Oil Capacity

A
  • Total: 3.6 gal
  • Drain & Refill Qty: 2 gal
  • Oil Qty Operating Range: 1 gal
  • T/O prohibited with OIL QTY annunciator illuminated
  • Do not mix oil brands or types
  • Oil Qty check required pior to T/O
36
Q

O2 Max limit

A

1850-2000 psi

37
Q

Max Ramp Weight

A

10,495 lbs.

38
Q

Max T/O Weight

A

10,450 lbs.

39
Q

Max Landing. Weight

A

9,921 lbs.

40
Q

Max ZFW

A

9,039 lbs

41
Q

Max baggage weight

A

Baggage Area: 400 lbs Cabin Area: 3,300 lbs

42
Q

Certified Category

A

Normal

43
Q

Load Factor - Flaps Up

A

+3.4g to -1.36g

44
Q

Load Factor - Flaps Down

A

+2.0g to -0.0g

45
Q

Minimum Flight Crew

A

One

46
Q

Flight into icing conditions approved when:

A

All ice protection, and both generators serviceable. Exit icing conditions if any of the above fail.

47
Q

Severe Icing

A

Prolonged flight should be avoided

48
Q

Max Flap in icing conditions (boots operable)

A

15 deg

49
Q

Max Flap in icing conditions (boots inop)

A

0 deg

50
Q

Freezing rain/fog/drizzle and mixed conditions causing ice accretion beyond the protected areas of the boots

A

Not approved

51
Q

Ice T/O?

A

Aircraft must be clear of all deposits of snow, ice and frost adhering to the lifting and control surfaces immediately prior to t/o.

52
Q

Temperature where the operating the boots may cause permanent damage

A

+40deg C

53
Q

Left Wing inspection light

A

Must be operative at night before t/o into known/forecasted icing conditions

54
Q

Total Fuel

A

406.8 Gal / 2,736.5 lbs

55
Q

Total usable Fuel

A

402 Gal / 2,703.6 lbs

56
Q

Max Fuel Imbalance

A

26.4 Gal / 178 lbs or “3 Segments”

57
Q

Max Operating Alt.

A

30,000 ft

58
Q

Min OAT/Max OAT

A

-55 deg C / +55 deg C

59
Q

Max Cabin PSID

A
  • 5.75 psi

* 0.7 Max landing diff

60
Q

Stall Waring/Stick Pusher

A

Preflight function test required before t/o Must function properly for for FIKI

61
Q

Trim System

A

Preflight function test required before t/o Stab normal/alt, rudder trim systems must function for all flights. Triple trim indicator must function properly for t/o

62
Q

Heated Windshield

A

L/R must function properly for all flights

63
Q

Eng Ice Protection

A

Preflight Function Test is required before t/o

64
Q

Min O2 supply

A

10 min for each occupant for flight FL250

65
Q

Flap cycles per hour

A

(0-15-0, 0-15–40-0)

  • 10 up to 25 deg C,
  • 8 25-50 deg C
66
Q

AP

A

AP & YD OFF t/o or ldg Min Alt 400’ AGL Alt Sel Captures (except approaches) not approved below 1,000’ AGL ILS approach, disengage AP below 200’ AGL Max GS angle 4 deg

67
Q

VX

A

120

68
Q

VY

A

130 (125 @5,000’ MSL)

69
Q

APPROACH SPEEDS

A

FLAPS 0: 120 FLAPS 15: 100 FLAPS 30: 90 FLAPS 40: 85

70
Q

DEMONSTRATED X-WIND

A

FLAPS 0: 30 FLAPS 15: 25 FLAPS 30: 20 FLAPS 40: 15

71
Q

BEST GLIDE

A

92 - 116

72
Q

TIRE PRESSURE

A

60 PSI

73
Q

MAX TIRE SPEED

A

160

74
Q

HYDROPLANE SPEED

A

~68

75
Q

CLIMB IN ICE MODE

A

140 KIAS

76
Q

FUEL TYPES

A

JETA, JETA-1, JETB, JP-4, JP5 AVGAS (UPTO 150 HRS) *ANTI-ICE IS REQUIRED

77
Q

Cabin Pressurization Limits

A

5.75 psi

Tempus Jets (4 decks)

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