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1. MC-12 Study Guide > MC-12 | Limitations > Flashcards

MC-12 | Limitations Flashcards

1
Q

Auto Pilot Limitation

AP/YD must not be used for _______ or ________.

A

Take off or Landing

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2
Q

Auto Pilot Limitation

Max Coupled intercept angles

Nav and Loc = _________*

A

< 90*

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3
Q

Auto Pilot Limitation

Max Coupled intercept angles

Nav and Loc Back Course = _________*

A

< 70*

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4
Q

Auto Pilot Limitation

Operation w/ Pitch Trip Malfunction is ______________.

A

Prohibited

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5
Q

Auto Pilot Limitations

Minimum Engage Height After Takeoff

A

400 ft. AGL

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6
Q

Auto Pilot Limitations

Minimum use height during approach

A

79 ft. AGL

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7
Q

Auto Pilot Limitations

Minimum use height during cruise

A

1000 ft. AGL

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8
Q

Auto Pilot Limitations

Minimum use height during steep approach

A

160 ft. AGL

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9
Q

AutoPilot Limitation

Rudderboost must be _____________.

A

Must be operational for all flights.

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10
Q

Brake De-Ice Limitations

Don’t use above______ * Celsius

More than ____ Minutes w/ wheels retracted

A

15* Celcius

10 Minutes

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11
Q

Climb Speed

A

135 KIAS SL - 35K

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12
Q

DC Power Limitations

Flight Operations (MEK)

34,000 - 35,0000

A

95%

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13
Q

DC Power Limitations

Flight Operations (MEK)

Sea Level - 34,000

A

100%

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14
Q

DC Power Limitations

Flight Operations (NOMEK)

21-26K

A

90%

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15
Q

DC Power Limitations

Flight Operations (NOMEK)

26-30K

A

80%

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16
Q

DC Power Limitations

Flight Operations (NOMEK)

30-32K

A

75%

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17
Q

DC Power Limitations

Flight Operations (NOMEK)

32-35K

A

70%

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18
Q

DC Power Limitations

Flight Operations (NOMEK)

Max Single Engine all Altitudes

A

90%

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19
Q

DC Power Limitations

Flight Operations (NOMEK)

SL-21K

A

100%

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20
Q

DC Power Limitations

Ground Operations (MEK)

55-70% N1

A

55%

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21
Q

DC Power Limitations

Ground OPS (NOMEK)

70-100% N1

A

100%

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22
Q

DC Power Limitations

Ground OPS -(NOMEK)

62-70% N1

A

75%

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23
Q

External Power Limits

Continuous

A

300 Amps

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24
Q

External Power Limits

Momentary

A

1000 Amps

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25
Q

External Power Limits

Normal

A

28-28.4

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26
Q

Fuel System Limitations

ER Fuel Capacity

A

118 Gal Ea (236 Total)

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27
Q

Fuel System Limitations

Max Imbalance

A

300 lbs.

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28
Q

Fuel System Limitations

Max Range

A

2300 NM or 8 Hrs

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29
Q

Fuel System Limitations

Max useable fuel quantity.

A

775 gal / 5192 lb

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30
Q

Fuel System Limitations

Max with fuel pressure light on

A

10 hrs.

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31
Q

Fuel System Limitations

Minimum in each main for takeoff.

A

265 lbs.

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32
Q

G Load Limitations

Flaps Down

A

0.0 - 2.0

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33
Q

G Load Limitations

Flaps Up

A

-1.21 - 3.01

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34
Q

Gear Cycle Limits

___ cycles at ___ every ____ Minutes

___ minutes rest after ___ cycles

A

Gear Cycle Limits

6 cycles at 1 every 5 Minutes
15 minutes rest after 6 cycles

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35
Q

Gyro Suction Gage Limits

Normal - 15K ft. - 35K Ft.

A

2.8 - 4.3 in

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36
Q

Gyro Suction Gage Limits

Normal - SL - 15K Ft.

A

4.3 - 5.9 in

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37
Q

Icing Limitations

EO/IR Turret must be __________(MC-12V)

A

Retracted

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38
Q

Icing Limitations

Vader radar & cooling sys must be ____________. (MC-12V)

A

Shut Down

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39
Q

Icing Limitations

When should you activate Engine De-Ice?

ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON
in ambient temperatures of +____°C or below, in ________ -__________.

Should also be off for Take-off above _____* C.

A

ENGINE ANTI-ICE, LEFT and RIGHT, shall be ON in ambient temperatures of +5°C or below, in visible moisture.

Should also be off for Take-off above 10* C.

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40
Q

ITT Limits (MEK & NOMEK)

Max Transient Starting

(Time Limited)

A

1000* Celcius for 5 seconds

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41
Q

ITT Limits

Cruise Climb

NOMEK | MEK

A

NOMEK 785* Celsius

MEK 840* Celsius

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42
Q

ITT Limits

Max Continuous

NOMEK | MEK

A

NOMEK 820* Celsius

MEK 840* Celsius

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43
Q

ITT Limits

Max Cruise

NOMEK | MEK

A

NOMEK 820* Celsius

MEK 840* Celsius

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44
Q

ITT Limits

Max Low Idle

NOMEK / MEK

A

NOMEK 750* Celsius

MEK 750* Celsius

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45
Q

ITT Limits

Max Reverse

NOMEK | MEK

A

NOMEK 760* Celsius

MEK 760* Celsius

46
Q

ITT Limits

Takeoff

NOMEK | MEK

A

NOMEK 820* Celsius

MEK 850* Celsius

47
Q

ITT Limits

Throttle PUSH

A

870* (100% Q for 5 minutes)

NOMEK ONLY During ENG Failure

48
Q

ITT Limits

Transient

NOMEK | MEK

(Time Limit)

A

NOMEK 850* Celsius
MEK 870* Celsius

20 seconds

49
Q

Max Operating Altitude

Normal Operations

50
Q

Oil Pressure Limits (PSI)

Caution Range (Limits Tq to ____%)

A

60-90 PSI

62% Q

51
Q

Oil Pressure Limits (PSI)

Max Starting

52
Q

Oil Pressure Limits (PSI)

Normal Operating Range

A

90-135 PSI

53
Q

Oil Pressure Limits (PSI)

Oil pressure below ___ psi is unsafe and requires engine shutdown or landing at nearest suitable airport.

*Fluctuations of +/- ____ psi are acceptable.

A

Oil pressure below 60 psi is unsafe and requires engine shutdown or landing at nearest suitable airport.

*Fluctuations of +/- 10 psi are acceptable.

54
Q

Oil Pressure Limits (PSI)

Starting, Low Idle

55
Q

Oil Temp Limits

Max Trans ( ___ Min) Ground ONLY

NOMEK | MEK

A

NOMEK 99-110* Celsius for 10 Minutes

MEK 111-115* Celsius for 10 Minutes

56
Q

Oil Temp Limits

Normal

NOMEK | MEK

A

NOMEK 0 - 99* Celsius

MEK 0 - 110* Celsius

57
Q

Oil Temp Limits

Rec for fuel heater ops at T/O

A

55* Celcius

58
Q

Oil Temp Limits

Starting, Low Idle

A

-40 - 110* Celcius

59
Q

Pneumatic Pressure Limits

Max

60
Q

Pneumatic Pressure Limits

Normal Operating Range

A

12 - 20 PSI

61
Q

Propeller De-Ice Ammeter Limitations

Normal Range

A

26 - 32 amps

62
Q

Props (N2 RPM) Limits

*All other conditions

63
Q

Props (N2 RPM) Limits

Avoid During Ground Operations

A

400 - 1050 RPM

NOMEK Only

64
Q

Props (N2 RPM) Limits

Inadvertent Excusions (Time Limited)

A

1735 RPM (7 Minutes)

NOMEK Only

65
Q

Props (N2 RPM) Limits

Max

66
Q

Props (N2 RPM) Limits

Max Reverse

67
Q

Props (N2 RPM) Limits

Max Transient (Time Limited)

A

1870 RPM for 20 Seconds

68
Q

Props (N2 RPM) Limits

Minimum Idle

A

1050 RPM (NOMEK Only)

69
Q

Props (N2 RPM) Limits

Normal Operating Range

A

1450 - 1700 RPM

70
Q

Starter Limitations

A

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

71
Q

Surface De-Ice Limits (Pneumatic Boot Operations)

No Operations Below

Activate when ice accumulates…

A

-40* C
__________

1/2 Inch

72
Q

Temp Limits

Max Above 25k ft.

A

ISA + 31* C

73
Q

Temp Limits

Max Below 25k ft.

A

ISA + 37* C

74
Q

Torque Limits

Max TQ Props above 1700 RPM

75
Q

Torque Limits

Normal Operating Range
1000-1700 rpm

76
Q

Torque Limits

Transient (NOMEK
Time LImited)

A

102% (NOMEK Only)

7 Minutes

77
Q

Torque Limits

Transient Limit
Time Limited

A

156%

20 Seconds

78
Q

Turbine Tach (N1 Speed) Limits

Max

79
Q

Turbine Tach (N1 Speed) Limits

Min Flight (MEK)

80
Q

Turbine Tach (N1 Speed) Limits

Min idle Ground (MEK)

81
Q

Turbine Tach (N1 Speed) Limits

Min Low Idle (NOMEK)

82
Q

Turbine Tach (N1 Speed) Limits

Transient

83
Q

V Speed

VX

84
Q

V Speed

Max Windshield De-Icing

85
Q

V Speed

Maximum Glide Range

86
Q

V Speed

Minimum for Reversing

87
Q

V Speed

Minimum Sustained Icing Speed
15K lbs or less

88
Q

V Speed

Minimum Sustained Icing Speed
> 15K lbs

89
Q

V Speed

Mmo (Above 24K ft.)

90
Q

V Speed

Va (Flaps Up)

91
Q

V Speed

Vb (Turbulence Penatration)

92
Q

V Speed

Vfe (Flaps Approach)

93
Q

V Speed

Vfe (Full Down)

94
Q

V Speed

Vlo (Extension)

95
Q

V Speed

Vlo (Retraction)

96
Q

V Speed

Vmca (Flaps Approach)

97
Q

V Speed

Vmca (Flaps Up)

98
Q

V Speed

Vmo (Below 24K ft.)

99
Q

V Speed

Vmo MX-15 extended (and >1,500’ AGL)

MC12V (AFMS)

100
Q

V Speed

VSSE ( Intentional OEI)

101
Q

V Speed

Vy

102
Q

V Speed

VYSe

103
Q

Weight Limits

Max Bag Compartment Weight

104
Q

Weight Limits

Max landing Weight

A

15,675 lbs.

105
Q

Weight Limits

Max Ramp Weight

A

16,600 lbs.

106
Q

Weight Limits

Max Takeoff Weight

A

16,500 lbs.

107
Q

Weight Limits

Max weight on airstair door.

A

One Person

108
Q

Weight Limits

Max Zero Fuel Weight (M, G, W)

A

13,000 lbs

109
Q

Weight Limits

Max Zero Fuel Weight (V)

A

13,430 lbs

110
Q

What is the Maximum Cabin Differential?

111
Q

Yaw Damn System ( 2 part question)

Max Altitude inoperable (Dual Strakes)

Must be on above ____________ except for
__________ & ___________.

A

19,000’ MSL

(Must be on above 19K except for takeoff and Landing)

Check REL

1. MC-12 Study Guide (16 decks)

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