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MC-12 SEMA > 5 & 9's > Flashcards

5 & 9's Flashcards

1
Q

Airspeed - Minimum for Reverse

A

40 KIAS

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2
Q

Airspeed - Vmca Flaps Approach

A

98 KIAS

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3
Q

Airspeed - Vmca Flaps Up

A

101 KIAS

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4
Q

Airspeed - Vsse Intentional One Engine INOP

A

135 KIAS

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5
Q

Airspeed - Vyse

A

135 KIAS

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6
Q

Airspeed - Vx

A

135 KIAS

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7
Q

Airspeed - Maximum Glide Range

A

135 KIAS

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8
Q

Airspeed - Vy

A

135 KIAS

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9
Q

Airspeed - Minimum Icing below 15,000 lbs

A

140 KIAS

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10
Q

Airspeed - Minimum Icing 15,000-16,500 lbs

A

150 KIAS

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11
Q

Airspeed - Vfe Full Down

A

158 KIAS

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12
Q

Airspeed - Vlo Retraction

A

164 KIAS

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13
Q

Airspeed - Vb Turbulence Penetration

A

170 KIAS

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14
Q

Airspeed - Va Flaps Up

A

182 KIAS

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15
Q

Airspeed - Vlo Extension

A

182 KIAS

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16
Q

Airspeed - Vfe Approach

A

202 KIAS

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17
Q

Airspeed - Maximum for Effective Windshield De-Icing

A

226 KIAS

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18
Q

Airspeed - Vmo Below 24,000 ft

A

245 KIAS

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19
Q

Airspeed - Mmo Above 24,000 ft

A

.58 Mach

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20
Q

Torque - Applicable within Range (1,000 - 1,700 RPM)

A

0-100%

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21
Q

Torque - Max TQ (Props below 1,000 RPM)

A

62%

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22
Q

Torque - Max TQ (Props above 1,700 RPM)

A

96%

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23
Q

Torque - Inadvertent Excursions (_ minutes)

A

102%; 7 minutes

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24
Q

Torque - Transient (__ seconds)

A

156%; 20 seconds

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25
Q

Turbine Tach (N1 Speed) - Minimum Low Idle

A

62%

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26
Q

Turbine Tach (N1 Speed) - Normal Operating Range

A

62-104%

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27
Q

Turbine Tach (N1 Speed) - Max

A

104%

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28
Q

ITT - Max Low Idle

A

750

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29
Q

ITT - Max Reverse

A

760

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30
Q

ITT - Recommended Cruise Climb

A

785

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31
Q

ITT - Max Cruise/Takeoff/Continuous

A

820

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32
Q

ITT - Transient (__ seconds)

A

850; 20 seconds

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33
Q

ITT - Max Starting (_ seconds)

A

1,000; 5 seconds

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34
Q

Oil Temp - Minimum Starting

A

-40C

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35
Q

Oil Temp - Normal Operating Range/Max Reverse

A

0C-99C

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36
Q

Oil Temp - Max Low Idle

A

-40C-110C

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37
Q

Oil Temp - Takeoff/Max Continuous/Cruise Climb

A

0C-110C

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38
Q

Oil Temp - Max Transient (__ minutes)

A

99C-110C; 10 minutes

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39
Q

Oil Temp - Recommended for Fuel Heater Ops at T/O

A

55C

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40
Q

Oil Pressure - Minimum Low Idle

A

60 psi

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41
Q

Oil Pressure - Caution Range (TQ limited __%)

A

60-90 psi; 62%

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42
Q

Oil Pressure - Normal Operating Range

A

90-135 psi

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43
Q

Oil Pressure - Max Starting

A

200 psi

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44
Q

Props (N2 RPM) - Minimum Idle Speed

A

1,050 RPM

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45
Q

Props (N2 RPM) - Normal Operating Range

A

1,450-1,700 RPM

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46
Q

Props (N2 RPM) - Max Reverse

A

1,650 RPM

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47
Q

Props (N2 RPM) - Max

A

1,700 RPM

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48
Q

Props (N2 RPM) - Inadvertent Excursions (_ minutes)

A

1735 RPM; 7 minutes

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49
Q

Props (N2 RPM) - Transient (__ seconds)

A

1,870 RPM; 20 seconds

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50
Q

Autofeather

A

Must be operable for all flights and must be armed for takeoff, climb, approach, and landing.

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51
Q

External Power - Volts

A

28.0-28.4 volts

52
Q

External Power - Minimum Momentary

A

1,000 amps

53
Q

External Power - Continuous

A

300 amps

54
Q

Generator Load - Ground Operations Max (62%-70% N1)

A

75%

55
Q

Generator Load - Ground Operations Max (70%-100%N1)

A

100%

56
Q

Generator Load - In-Flight Operations Max (SL-FL___)

A

100%; SL-FL210

57
Q

Generator Load - In-Flight Operations Max (FL210-FL___)

A

90%; FL210-FL260

58
Q

Generator Load - In-Flight Operations Max (FL260-FL___)

A

80%; FL260-FL300

59
Q

Generator Load - In-Flight Operations Max (FL300-FL___)

A

75%; FL300-FL320

60
Q

Generator Load - In-Flight Operations Max (FL320-FL___)

A

70%; FL320-FL350

61
Q

Generator Load - In-Flight Operations Single Engine Operations

A

90%

62
Q

Generator Load - In-Flight Operations VDC Normal

A

27.5-29.0

63
Q

Starter Limits

A

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

64
Q

Weight Limits - Max Ramp

A

16,600 lbs

65
Q

Weight Limits - Max Takeoff

A

16,500 lbs

66
Q

Weight Limits - Max Landing

A

15,675 lbs

67
Q

Weight Limits - Max Zero Fuel

A

13,000 lbs

68
Q

Weight Limits - Max Baggage Compartment

A

550 lbs

69
Q

Weight Limits - Air Stair Door

A

One Person

70
Q

Fuel System - Max Imbalance

A

300 lbs

71
Q

Fuel System - Min in each main for T/O (yellow arc)

A

265 lbs

72
Q

Fuel System - Max Usable QTY (___ gal)

A

5192 lbs; 775 gal

73
Q

Fuel System - Max with FUEL PRES LO Light

A

10 Hours

74
Q

Fuel System - Tank Fueling Order

A

Mains full before Aux full before ER

75
Q

Fuel System - Range w/ ER

A

approx. 2,300 NM/8 hours

76
Q

Fuel System - ER Tanks

A

236 gal total; 118 gal per side

77
Q

Fuel System - Fuel Crossfeed

A

Permitted only when one engine is inoperative

78
Q

Gear Cycle Limits

A

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

79
Q

G-Load - Flaps UP

A

3.0- -1.21

80
Q

G-Load Flaps Down

A

2.0-0

81
Q

Vacuum Gage - SL to 15,000 ft

A

4.3-5.9 inHg

82
Q

Vacuum Gage - 15,000 to 35,000 ft

A

2.8 to 4.3 inHg

83
Q

Prop De-Ice - Normal Operating Range

A

26-32 Amps

84
Q

Rudder Boost

A

Must be operation for ALL flights

85
Q

Yaw Damp System - Max Altitude INOP

A

19,000 ft

86
Q

Yaw Damp System - Must be ON above; OFF for __________ & __________

A

Above 19,000 ft; takeoff & landing

87
Q

Temperature Limits

A

ISA+37 - SL to 25,000 ft

ISA+31 - Above 25,000 ft

88
Q

Surface De-Ice

A

No operations below -40C

Activate when Ice accumulates a minimum of 1/2 inch

89
Q

Engine Anti-Ice

A

ON when ambient temperatures are +5C and below in visible moisture
OFF for takeoff in ambient temperatures above +10C

90
Q

Pneumatic Pressure Gage

A

12-20 psi - Normal Operating Range

20 psi - Max

91
Q

Cabin Altimeter/Differential Limits

A

6.6 Max

92
Q

Max Altitude

A

35,000 ft

93
Q

Brake De-Ice (if installed)

A

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

94
Q

Autopilot Limits

A
  1. During autopilot operations, a pilot must be seated at the controls with the seat belt and shoulder harness fastened
  2. An autopilot preflight check must be completed and found satisfactory prior to each flight on which the autopilot is to be used
  3. The autopilot minimum engage height after takeoff is 400 ft AGL
  4. The autopilot minimum use height during cruise is 1,000 ft AGL
  5. The autopilot minimum use height during approach is 79 ft AGL
  6. The autopilot minimum use height during steep approach is 160 ft AGL
  7. Maximum airspeed for autopilot operation is unchanged from the airplane maximum speed (Vmo/Mmo)
  8. The autopilot and yaw damper must not be used for takeoff and landing
  9. Operation of the autopilot system with a pitch trim malfunction is prohibited
  10. Do not manually override the autopilot during normal flight
  11. The maximum coupled intercept angles are:
    NAV/LOC - 90 degrees
    Back course - 70 degrees
95
Q

ENGINE FAILURE BEFORE V1 (ABORT)

A

1) POWER levers - GROUND FINE

2) Braking - As required

96
Q

ENGINE FAILURE AFTER V1

A

1) POWER - Max allowable
2) LANDING GEAR CONTROL handle - UP (positive rate of climb confirmed)
3) Airspeed - Maintain V2 until 400 ft AGL and clear of obstacles
4) Propeller - Verify feathered
5) FLAPS (after Vyse) - UP

97
Q

ENGINE FAILURE DURING FLIGHT BELOW Vmca

A

1) POWER - Reduce as required to maintain control

2) Pitch Attitude - Lower to accelerate above Vmca

98
Q

ENGINE FAILURE DURING FLIGHT

A

1) AP/YD - Disengage
2) POWER - As required
3) Failed Engine - Identify
4) Propeller - Verify feathered

99
Q

ENGINE FAILURE DURING FINAL APPROACH

A

1) POWER - As required

2) Landing gear - confirm down

100
Q

ENGINE FAILURE (SECOND ENGINE)

A

1) Airspeed - As required
2) POWER lever - IDLE
3) PROP lever - As required

101
Q

MAXIMUM GLIDE

A

1) LANDING GEAR CONTROL handle - UP
2) FLAPS - UP
3) PROP levers - FEATHER
4) Airspeed - 135 KIAS

102
Q

SINGLE-ENGINE GO AROUND

A

1) POWER - Maximum allowable
2) LANDING GEAR CONTROL handle - UP
3) FLAPS - UP
4) Airspeed - Vyse

103
Q

L OR R BLEED AIR FAIL ANNUNCIATOR ILLUMINATED

A

1) BLEED AIR VALVES switch (affected engine) - PNEU & ENVIR OFF

104
Q

EXCESSIVE DIFFERENTIAL PRESSURE (CABIN DIFF HI ANNUNCIATOR ILLUMINATED)

A

1) BLEED AIR VALVES switches - ENVIR OFF
2) Crew oxygen masks - EMER and don
3) MIC swtich - OXY
4) PASSENGER MANUAL DROP OUT handle - Pull on
5) Descend - As required

105
Q

LOSS OF PRESSURIZATION (CABIN ALTITUDE AND/OR CABIN ALT HI ANNUCIATOR ILLUMINATED)

A

1) Crew oxygen masks - EMER and don
2) MIC switches - OXY
3) PASSENGER MANUAL DROP OUT handle - Pull on
4) Descend- As required

106
Q

DOOR UNLOCK WARNING ANNUNCIATOR ILLUMINATED

A

1) All occupants - Seated with seatbelts securely fastened

107
Q

CRACKED CABIN WINDOW

A

1) Crew oxygen masks - ON

2) MIC switches - OXY

108
Q

BOTH DC GEN LIGHTS ILLUMINATED

A

1) Mission power - Off
2) INSTRUMENT EMERGENCY LIGHTS - ON (if required)
3) Generators - GEN RESETS, then ON
4) Operating generator load meter - Monitor (100% maximum)
5) ECS MODE - OFF
6) COCKPIT/CABIN BLOWER - AUTO
7) Non-essential equipment - Off

109
Q

PRIMARY AND OVERSPEED GOVERNERS FAILED (ABOVE 1768)

A

1) POWER lever (affected engine) - IDLE

2) PROP lever (affected engine) - FEATHER

110
Q

PRIMARY AND OVERSPEED GOVERNERS FAILED (ABOVE 1768 RPM)

A

1) POWER lever (affected engine) - IDLE

2) PROP lever (affected engine) - FEATHER

111
Q

ENGINE/NACELLE FIRE DURING START OR GROUND OPERATIONS

A

1) PROP levers - FEATHER
2) CONDITION levers - FUEL CUTOFF
3) F/W VALVE PUSH switch - Push to close (CLOSED annunciator illuminated)
4) EXTINGUISHER PUSH switch - PUSH
5) MASTER SWITCH - OFF
6) BATT BUS - EMER OFF

112
Q

ENGINE FIRE IN FLIGHT (IDENTIFIED)

A

1) POWER lever (affected engine) - IDLE
2) PROP lever (affected engine) - FEATHER
3) CONDITION lever (affected engine) - FUEL CUTOFF
4) F/W VALVE PUSH switch - Push to close (CLOSED annunciator illuminated)
5) EXTINGUISHER PUSH switch - PUSH

113
Q

FUSALAGE FIRE

A

1) Fight the fire

2) Land as soon as possible

114
Q

WING FIRE

A

1) Perform engine shutdown on affected side

2) Land as soon as possible

115
Q

ELECTRICAL SMOKE OR FIRE

A

1) Crew oxygen masks - EMER and don

2) MIC switches - OXY

116
Q

ENVIRONMENTAL SYSTEM SMOKE OR FUMES

A

1) Crew oxygen masks - EMER and don

2) MIC switches - OXY

117
Q

EMERGENCY DESCENT

A

1) POWER levers - IDLE
2) PROP levers - High
3) Flaps (202 KIAS max) - APPROACH
4) LDG GEAR CONTROL handle (182 KIAS max) - DN
5) Airspeed - 182 KIAS maximum

118
Q

UNSCHEDULED RUDDER BOOST ACTIVIATION

A

1) AP/TRIM MASTER switch - Press to first detent and hold
2) RUDDER BOOST switch - OFF
3) AP/TRIM MASTER switch - Release
If condition persists
4) YD/AP DISC switch (on flight guidance panel) - Pull down

119
Q

UNSCHEDULED ELECTRIC ELEVATOR TRIM

A

1) Airplane attitude - Maintain using elevator control

2) AP/TRIM MASTER switch - Depress fully and hold

120
Q

AUTOPILOT MISTRIM [E] OR [A]

A

1) Flight controls - Hold firmly

2) Autopilot - Disengage

121
Q

AUTOPILOT MISTRIM [TRIM]

A

1) Flight controls - Hold firmly

2) Autopilot - Disengage

122
Q

UNEXPECTED AUTOPILOT DISENGAGEMENT

A

1) Aircraft control - Maintain

2) Autopilot/trim disconnect switch - Press to first level to cancel horn

123
Q

STALLS (DEPARTURE FROM CONTROLLED FLIGHT)

A

1) Autopilot and yaw damper - Disengage
2) Aircraft pitch - Apply control to reduce angle of attack
3) Aircraft bank - Wings level
4) POWER - As required
5) Execute a smooth recovery

124
Q

SPINS

A

1) Autopilot and yaw damper - Disengage
2) Control wheel - Full forward, ailerons neutral
3) Full rudder - Opposite the direction of spin
4) POWER levers - IDLE
5) RUDDER - Neutralize when rotation stops
6) Execute a smooth recovery

125
Q

Throttle Push

A

Single use emergency power available for single engine operations in high density altitude conditions. 100% TQ with max of 870C ITT at 1,700 RPM for 5 minutes.

MC-12 SEMA (1 decks)

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