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MC-12 > OPS Limits > Flashcards

OPS Limits Flashcards

1
Q

Maneuvering Speed (VA)

A

184

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2
Q

Maneuvering Speed (VA) [ER]

A

182

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3
Q

Max Flap Extension/Extended (VFE) - Approach

A

202

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4
Q

Max Flap Extension/Extended (VFE) - Full Down

A

158

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5
Q

Max Landing Gear Operating Speed (VLO) - Extension

A

184

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6
Q

Max Landing Gear Operating Speed (VLO) - Retraction

A

166

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7
Q

Max Landing Gear Operating Speed (VLO) - Extension [ER]

A

184

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8
Q

Max Landing Gear Operating Speed (VLO) - Retraction [ER]

A

164

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9
Q

Air Min Control Speed (VMCA) - Flaps Up

A

94

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10
Q

Air Min Control Speed (VMCA) - Flaps Down

A

93

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11
Q

Air Min Control Speed (VMCA) - Flaps Up [ER]

A

101

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12
Q

Air Min Control Speed (VMCA) - Flaps Down [ER]

A

98

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13
Q

Max Operating Speed (VMO) to 21,000’

A

263 KIAS

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14
Q

Max Operating Speed (VMO) above 21,000’

A

.58 Mach

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15
Q

Max Operating Speed (VMO) to 24,000’ [ER]

A

245 KIAS

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16
Q

Max Operating Speed (VMO) above 24,000’ [ER]

A

.58 Mach

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17
Q

Two Engine Best Rate of Climb (VY)

A

140

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18
Q

Two Engine Best Rate of Climb (VY) [ER]

A

135

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19
Q

Turbulent Air Penetration

A

170

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20
Q

Max Airspeed for Windshield Anti-icing

A

226

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21
Q

Min Airspeed for Sustained Flight in Icing

A

140

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22
Q

Intentional One-Engine Inop Speed (VSSE)

A

110

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23
Q

Intentional One-Engine Inop Speed (VSSE) [ER]

A

135

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24
Q

One-Engine Inop Best Angle of Climb (VXSE)

A

125

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25
Q

One-Engine Inop Best Angle of Climb (VXSE) [ER]

A

135

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26
Q

One-Engine Inop Best Rate of Climb (VXSE)

A

125

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27
Q

One-Engine Inop Best Rate of Climb (VXSE) [ER]

A

135

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28
Q

Emergency Descent Speed

A

184

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29
Q

Emergency Descent Speed [ER]

A

182

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30
Q

Max Range Glide Speed

A

135

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31
Q

Max Torque for Takeoff

A

100%

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32
Q

Max Continuous Torque

A

100%

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33
Q

Max Transient Torque

A

156%

34
Q

Inadvertent torque excursions up to ___% are time limited to _______.

A

102%, 7 minutes

35
Q

Max Starting ITT

A

1000°C

36
Q

Max Idle ITT

A

750°C

37
Q

Max Takeoff ITT

A

820°C

38
Q

Max Continuous ITT

A

820°C

39
Q

Max Transient ITT

A

850°C

40
Q

Max Takeoff N1

A

104%

41
Q

Max Continuous N1

A

104%

42
Q

Max Cruise Climb N1

A

104%

43
Q

Max Cruise N1

A

104%

44
Q

Max Transient N1

A

104%

45
Q

N2 Idle

A

1050 RPM Min

46
Q

Max Takeoff N2

A

1700 RPM

47
Q

Max Continuous N2

A

1700 RPM

48
Q

Inadvertent propeller excursions up to ____RPM are time limited to ___ minutes.

A

1735, 7

49
Q

Sustained prop overspeeds faster than ____RPM indicate a failure of the _______ governor.

A

1700, primary

50
Q

Flight may be continued at propeller overspends up to ____RPM, provided torque is limited to __%.

A

1768, 96

51
Q

Sustained propeller overspeeds faster than ____RPM indicate failure of both the _____ and the _____. Such overspends are not approved.

A

1768, primary governor, and the secondary governor

52
Q

Autofeather must be operational for:

A

All Flight

53
Q

Autofeather must be armed for:

A

Takeoff, climb, Approach, and Landing

54
Q

Normal Oil Pressure

A

90-135 psi

55
Q

Undesirable Oil Pressure

A

<90 psi

56
Q

Under emergency conditions oil pressure below ___ psi is permitted with reduced power of ___% torque.

A

60 psi, 62%

57
Q

Unsafe oil pressure requiring shutdown or min power to land:

A

<60 psi

58
Q

Acceptable Oil Pressure Fluctuations.

A

+/- 10 psi

59
Q

Normal Oil Temperature

A

-40 to 110°C

60
Q

Normal External Power Cart Voltage

A

28-28.4 V

61
Q

Max External Power Current (sustained)

A

300 Amps

62
Q

Max External Power Current (momentary)

A

1000 Amps

63
Q

Starter Limited to:

A

30 sec ON, 5 min OFF; 30 sec ON, 5 min OFF; 30 sec ON, 30 min OFF

64
Q

Total usable fuel

A

3611 lbs

65
Q

Total usable fuel [ER]

A

5192 lbs

66
Q

Max allowable fuel imbalance

A

300 lbs

67
Q

Don’t takeoff if fuel gauges each read less than;

A

265 lbs

68
Q

Don’t put any fuel into the AUX tanks unless the ____ tanks are full.

A

MAIN

69
Q

Do not put any fuel in the ____ tanks unless both the ____ and ____ tanks are full. [ER]

A

EXTENDED RANGE, AUX, MAIN

70
Q

Max Ramp Weight

A

15,100 lbs

71
Q

Max Ramp Weight [ER]

A

16,600 lbs

72
Q

Load Factor Limitations (Flaps Up)

A

-1.24 to 3.1 G’s

73
Q

Load Factor Limitations (Flaps Down)

A

0 to 2 G’s

74
Q

Landing Gear Cycles (1 up and 1 down = 1 cycle):

A

1 every 5 minutes followed by a 15 minute cool down

75
Q

Max Cabin Pressure Differential

A

6.6 psi

76
Q

When must rudder boost be operational.

A

All flights

77
Q

Sustained Flight in icing conditions with flaps extended is ____ except for ___ and ___.

A

prohibited, approach, and landing

78
Q

When must Engine Anti-ice be ON?

A

5° C or less with visible moisture

79
Q

When must Engine Anti-ice be OFF?

A

> 10° C

80
Q
A

MC-12 (3 decks)

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