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MC-12 > Limits > Flashcards

Limits Flashcards

1
Q

[Torque] Operating Range (1000 - 1700 RPM)

A

0-100%

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2
Q

[Torque] Max TQ (Props below 1000 RPM)

A

62%

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3
Q

[Torque] Max TQ (Props above 1700 RPM)

A

96%

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4
Q

[Torque] Inadvertent Excursions

A

102% (7 minutes)

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5
Q

[Torque] Transient

A

156% (20 seconds)

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6
Q

[N1] Minimum Low Idle

A

62%

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7
Q

[N1] Normal Operating Range

A

62 - 104%

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8
Q

[N1] Max

A

104%

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9
Q

[ITT] Max Low Idle

A

750 C

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10
Q

[ITT] Max Reverse

A

760 C

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11
Q

[ITT] Recommended Cruise Climb

A

785 C

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12
Q

[ITT] Max Cruise

A

820 C

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13
Q

[ITT] Takeoff / Max Continuous

A

820 C

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14
Q

[ITT] Transient

A

850 C (20 seconds)

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15
Q

[ITT] Max Starting

A

1000 (5 seconds) C

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16
Q

[Oil Temp] Minimum Starting

A

-40 C

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17
Q

[Oil Temp] Normal Operating Range / Max Reverse

A

0 - 99 C

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18
Q

[Oil Temp] Max Low Idle

A

-40 - 110 C

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19
Q

[Oil Temp] Takeoff

A

0 - 110 C

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20
Q

[Oil Temp] Max Continuous / Cruise Climb

A

0 - 110 C

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21
Q

[Oil Temp] Max Transient

A

99 - 110 (10 minutes) C

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22
Q

[Oil Temp] Recommended for Fuel Heater Ops at T/O

A

55 C

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23
Q

[Oil Pressure] Minimum Low Idle

A

60 PSI

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24
Q

[Oil Pressure] Caution Range (TQ limited to 62%)

A

60 - 90 PSI

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25
Q

[Oil Pressure] Normal Operating Range

A

90 - 135 PSI

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26
Q

[Oil Pressure] Max Starting

A

200 PSI

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27
Q

[N2] Minimum Idle Speed

A

1050 RPM

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28
Q

[N2] Normal Operating Range

A

1450 - 1700 RPM

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29
Q

[N2] Max Reverse

A

1650 RPM

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30
Q

[N2] Max

A

1700 RPM

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31
Q

[N2] Inadvertent Excursions

A

1735 (7 minutes)

32
Q

[N2] Transient

A

1870 (20 Seconds) RPM

33
Q

Autofeather Requirements

A

Must be OPERABLE for all flights and must be ARMED for takeoff, climb, approach and landing.

34
Q

External Power Limits

A

28.0 - 28.4 volts
1000 AMPS Minimum Momentary
300 AMPS Continuous

35
Q

[Generator Load, Ground] Max (62% - 70% N1)

A

75%

36
Q

[Generator Load, Ground] Max (70% - 100% N1)

A

100%

37
Q

[Generator Load, Flight] Max (SL - FL210)

A

100%

38
Q

[Generator Load, Flight] Max (FL 210 - 260)

A

90%

39
Q

[Generator Load, Flight] Max (FL 260 - 300)

A

80%

40
Q

[Generator Load, Flight] Max (FL 300 - 320)

A

75%

41
Q

[Generator Load, Flight] Max (FL 320 - 350)

A

70%

42
Q

[Generator Load] Max Single Engine Operations

A

90%

43
Q

[Generator Load] Normal

A

27.5 - 29 VDC

44
Q

Starter Limitation

A

30 seconds ON 5 minutes OFF
30 seconds ON 5 minutes OFF
30 seconds ON 30 minutes OFF

45
Q

Max Ramp Weight

A

16,600 lbs

46
Q

Max Takeoff Weight

A

16,500 lbs

47
Q

Max Landing Weight

A

15,675 lbs

48
Q

Max Zero Fuel Weight

A

13,000 lbs

49
Q

Max Baggage Compartment Weight

A

550 lbs

50
Q

Max on Air Stair Door

A

One Person

51
Q

[Fuel] Max Imbalance

A

300 lbs

52
Q

[Fuel] Min for Takeoff

A

265 lbs (in each)

53
Q

[Fuel] Max Useable Quantity

A

5192 lbs, 775 gallons

54
Q

Fuel Crossfeed permitted only when:

A

one engine is inoperative

55
Q

Gear Cycle Limit

A

6 cycles (1 up - 1 down) at one every 5 minutes followed by a 15 minute cool down.

56
Q

G-Load Flaps UP

A

-1.21 to 3.0

57
Q

G-Load Flaps DOWN

A

0 to 2.0

58
Q

[Vacuum Gauge] Normal from SL to 15,000 feet

A

4.3 to 5.9 in. Hg

59
Q

[Vacuum Gauge] Normal from 15,000 to 35,000 feet

A

2.8 to 4.3 in. Hg

60
Q

[Propeller De-Ice] Normal Operating Range

A

26-32 AMPS

61
Q

When must rudder boost be operational?

A

For all flights

62
Q

Max Altitude Yaw Dam INOP

A

19,000 (with dual aft strakes)

63
Q

[Temperature Limits] Max from SL to 25,000 feet

A

ISA + 37

64
Q

[Temperature Limits] Max above 25,000 feet

A

ISA + 31

65
Q

Minimum Surface De-Ice Temp

A

-40

66
Q

Ice Vane Use

A

ON When ambient temperatures are +5 C and below in visible moisture

OFF for takeoff in ambient temperatures above +10 C

67
Q

[Pneumatic Pressure] Normal Operating Range

A

12-20 PSI

68
Q

[Pneumatic Pressure] Max

A

20

69
Q

Cabin Differential Limit

A

6.6 PSID

70
Q

Max Operating Altitude

A

35,000 feet

71
Q

Brake De-Ice Limit

A

Don’t use above 15 C or more than 10 minutes with wheels retracted

72
Q

Minimum Autopilot height after Takeoff

A

400 ft AGL

73
Q

Minimum Autopilot height during Cruise

A

1000 AGL

74
Q

Minimum Autopilot height during Approach

A

79 feet AGL

75
Q

Minimum Autopilot height during Steep Approach

A

160 feet AGL

76
Q

Throttle Push

A

ITT 870 for 5 minutes with a torque limit of 100%

MC-12 (4 decks)

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