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MC-12W > MC-12W > Flashcards

MC-12W Flashcards

1
Q

Maneuvering Speed (Va)

A

184

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2
Q

Maneuvering Speed ER (Va)

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) Extension ER

A

182

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7
Q

Max Landing Gear Operating Speed (Vlo) Retraction

A

166

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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 up ER

A

101

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11
Q

Air Min Control Speed (Vmca) Flaps Down

A

93

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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

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14
Q

Max Operating Speed (Vmo) To 24,000 ER

A

245

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15
Q

Max Operating Speed (Vmo) Above 21,000

A

.58M

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16
Q

Max Operating Speed (Vmo) Above 24,000 ER

A

.58M

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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 effective windshield Anti-icing

A

226

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21
Q

Min Airspeed for sustainded 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

A

184

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29
Q

Emergency Descent ER

A

182

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30
Q

Max Range Glide

A

135

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31
Q

Max Ramp Weight

A

15,100

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32
Q

Max Ramp Weight ER

A

16,600

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33
Q

Max T/O Weight

A

15,000

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34
Q

Max T/O Weight ER

A

16,500

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35
Q

Max landing weight

A

15,000

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36
Q

Max landing weight ER

A

15,675

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37
Q

Usable Fuel

A

3,611

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38
Q

Usabel Fuel ER

A

5,192

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39
Q

Planned Recovery Fuel

A

550

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40
Q

Minimum Fuel

A

400

41
Q

Emergency Fuel

A

300

42
Q

Min T/O Fuel(per side)

A

265

43
Q

Max wind (any direction)

A

50

44
Q

RCR12 and above wind limits

A

25

45
Q

Max tailwind component

A

10

46
Q

Max Cabin diff

A

6.6

47
Q

CABIN DIFF HI

A

6.9 +-.3

48
Q

CABIN ALTITUDE HI

A

12,000

49
Q

Torque-T/O,Max Cont, Cruise, Cruise Climb, Throttle Push

A

100

50
Q

Torque Transient

A

156 (20sec)

51
Q

ITT Starting

A

1000 (5sec)

52
Q

ITT Idle

A

750

53
Q

ITT- T/O, Max cont, Cruise

A

820

54
Q

ITT Cruise climb

A

785

55
Q

ITT Transient

A

850 (20sec)

56
Q

ITT Throttle Push

A

870 (5min)

57
Q

Min N1 % Idle

A

62

58
Q

N1 % -T/O,Max Cont, Cruise, Cruise Climb, Transient, Throttle Push

A

104

59
Q

Min Prop RPM N2 Idle

A

1050

60
Q

Prop RPM N2 - T/O, Max Cont, Cruise, Cruise Climb, Throttle Push

A

1700

61
Q

Prop RPM N2 Transient

A

1870 (20sec)

62
Q

Oil Press (PSI) Starting

A

0-200

63
Q

Min Oil Press (PSI) Idle

A

60

64
Q

Oil Press (PSI) - T/O, Max Cont, Cruise, Cruise Climb, Throttle Push

A

90-135

65
Q

Oil Press (PSI) Transient

A

200

66
Q

Min Oil Temp Starting

A

-40

67
Q

Oil Temp Idle

A

-40-110

68
Q

Oil Temp -T/O,Max Cont, Cruise, Cruise Climb, Transient, Throttle Push

A

0-110

69
Q

Inadvertent torque excursions up to ________ are time limited to _____ min

A

102%, 7

70
Q

Sustained prop overspeeds faster than _____ RPM indicate failure of the primary governor.

A

1700

71
Q

Flight may be continued at propeller overspeeds up to ______ RPM, provided torque is limitied to _____.

A

1768, 96%

72
Q

Sustained propeller overspeeds faster than _____ RPM indicate failure of both primary governor and the secondary governor and such overspeed are not approved.

A

1768

73
Q

Inadvertent propeller excurions up to _____ RPM are time limited to _____ min.

A

1735, 7

74
Q

Oil pressures under ____ psi are undesirable.

A

90

75
Q

Under emergency conditions, to complete a flight, a lower oil pressure limit of _____ psi is permissible at a reduced power level not to exceed _____% torque.

A

62

76
Q

Oil pressures below _____ psi are unsage and require that either the engine be shut down or a landing be made at the nearest suitable airport, using the minimum power required to sustain flight.

A

60

77
Q

Fluctuations of ____psi are acceptable.

A

+/- 10

78
Q

Starter is limited to ____sec ON, ___ min OFF, ____ON, ___ min OFF, _____sec ON, then ____ min OFF.

A

30 sec, 5min, 30 sec, 5 min, 30 sec, 30 min.

79
Q

Load Factor (G’s) Flaps up

A

-1.24 to 3.1

80
Q

Load Factor (G’s) Flaps up ER

A

-1.21 to 3.01

81
Q

Load Factor (G’s) Flaps Down

A

0 to 2.0

82
Q

Min Battery for start

A

23 volts

83
Q

Min Battery to use ext power

A

20 volts

84
Q

Ext. Power Cart

A

28-28.4 volts

85
Q

Cart - Sustained/Momentary

A

300/1000 Amps

86
Q

Landing gear cycles limited to ___ every ____ min. for ____ cycles followed by a ____ min. cool down.

A

1, 5min, 6, 15min

87
Q

Rudder boost must be ___________ for _________.

A

Operational, all flights

88
Q

Auto feather must be operable for ________, and must be armed during ________, _______, ________, and _________.

A

all flights, TO, Climb, Approach, Landing

89
Q

Engine Anti-ice must be ON for operation in ambient temperatures of _____ C or below when flight free of ________ ________ cannot be assured.

A

+5, visible moisture

90
Q

Engine Anti-ice must be off for takeoff operations when ambient temps exceed________ C.

A

+10

91
Q

The order in which the fuel tanks must be filled is ________, _________, then __________.

A

main, Aux, extended range

92
Q

Sustainde flight in icing conditions with flaps extended is prohibited except for_______ and ________.

A

Approach and landing.

93
Q

Engine Fire on Ground

A
  1. Condition Lever – Cutoff
  2. Firewall Valve – Close
  3. Starter – Starter Only
  4. Extinguisher (if fire warning persists) – Actuate
94
Q

Emergency Engine Shutdown on Ground

A
  1. Condition Levers – Cutoff
  2. Props – Feather
  3. Firewall Valves –Close
  4. Master Switch – OFF
  5. Batt Bus – Emer OFF
  6. ESIS – OFF
95
Q

Takeoff Abort

A
  1. Power – Ground Fine

2. Brakes – As Required

96
Q

Engine Failure Takeoff Continued

A
  1. Vr – Rotate
  2. Power – Max Allowable
  3. Gear – UP
  4. Airspeed – V2 To Accel height (400’ AGL min)
  5. Prop(Inop engine) – Verify Feathered
97
Q

Engine Fire / Failure in Flight

A
  1. Condition Lever – Cutoff
  2. Prop – Feather
  3. Firewall valve – Close
  4. Extinguisher (if fire warning persists) – Actuate
98
Q

Enviromental Smoke / Fumes

A
  1. Oxygen Mask – Don
  2. Mask selector switch – EMER
  3. Mic – OXY

MC-12W (1 decks)

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