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C-12 > Limits > Flashcards

Limits Flashcards

1
Q

Va Maneuvering Speed (Clean) at 12,500lbs

A

181 KIAS

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2
Q

Max Flap Speeds at 12,500 lbs

A

App: 200 KIAS
Full Down: 157 KIAS

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3
Q

Max LDG Gear Speeds

A

Retraction: 163 KIAS
Extension: 181 KIAS
Extended: 181 KIAS

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4
Q

Vmca at 12,500lbs

A

86 KIAS

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5
Q

Vmo/Mmo

A

259 KIAS/0.52 Mach

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6
Q

Solid Red Bar Marking based on Max Wt

A

Vs1 (Flaps up and idle power): 99 KIAS
Vs1 (Flaps approach and idle power): 85 KIAS
Vs0 (Flaps down and idle power): 75 KIAS

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7
Q

Power Levers

A

Do not lift power levers in flight. Lifting the power levers in flight, or moving the power levers in flight below the flight idle position, could result in a nose-down pitch and descent rate leading to aircraft damage and injury to personnel.

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8
Q

Max Takeoff and Continuous Torque (FT-LB)

A

2230 ft-lb

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9
Q

Max Transient Torque

A

2230-2750 ft-lb for 5 sec

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10
Q

Max Start ITT

A

1000°C for 5 secs

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11
Q

Normal Cruise and Climb ITT

A

770°C

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12
Q

During autopilot operations, a pilot must

A

be seated at the controls with seatbelts fastened.

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13
Q

The autopilot shall not be used with flaps past

A

The approach position

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14
Q

Minimum altitude for the autopilot

A

a) Takeoff - 400’ AGL.
b) Cruise - 1000’ AGL.
c) Approach - 200’ AGL.

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15
Q

Minimum altitude for yaw damper engagement

A

200’ AGL.

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16
Q

Auto Pilot disengagement checks shall

A

be conducted and found satisfactory prior to each flight on which the autopilot is used.

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17
Q

Autopilot or yaw damper use during takeoff or landing

A

Warning: autopilot or yaw damper use during takeoff or landing may result in loss of directional control.

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18
Q

Max sink rate @ touchdown

A

300 fpm

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19
Q

Max Tailwind

A

10 kts

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20
Q

Max Speed with Flaps down

A

157 KIAS

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21
Q

Min Oil Pressure

A

60 PSI on the ground

85 to 100 below 21,000ft (amber)
100 to 135 below 21,000ft (green)

60 to 85 at or above 21,000ft (amber)
85 to 135 at or above 21,000ft (green)

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22
Q

Takeoff and Max Continuous Oil Pressure

A

100 to 135 PSI

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23
Q

Normal and Amber Cruise Oil Pressure

A

Amber: 85-100 PSI below 21,000 ft
100-135 PSI below 21,000ft
85-135 above 21,000ft

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24
Q

(Max-Reverse) Oil Pressure Range

A

100-135 PSI. Limited to 1 min

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25
Q

Minimum Oil Temperature

A

-40°C for engine starts, low and high idle

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26
Q

Normal Oil Temperature Range

A

0-99°C

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27
Q

Transient Oil Temperature

A

100-104°C for 5 minutes

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28
Q

Max Torque

A

2230 ft-lbs for takeoff, climb and cruise
Transient: 2230-2750 ft-lbs for 5 seconds (see note on windshear EP)

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29
Q

(N/W/C) Engine Failure after Takeoff

A

• Maximum climb performance can be achieved by raising the failed engine 3
to 5° up and displacing the slip skid indicator one-half to three-quarters of a ball width toward the good engine.
• If the auto feather system is being used, retarding the POWER lever below
approximately 90 percent N1 before the feathering sequence is complete will deactivate the auto feather circuit and prevent automatic feathering.

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30
Q

Max Oil Temp

A

99°C

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31
Q

Max Oil Pressure on start

A

200 PSI

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32
Q

Max Oil Pressure Fluctuations

A

+/- 10 PSI

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33
Q

Vx Best angle of climb

A

100 KIAS

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34
Q

Vy Best rate of climb

A

121 KIAS

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35
Q

Vsse Minimum safe 1 inop

A

104 KIAS

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36
Q

Vyse Best rate of climb single engine

A

121 KIAS

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37
Q

Vxse Best angle of climb single engine

A

115 KIAS

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38
Q

Vlr Max Landing Gear Retraction

A

163 KIAS

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39
Q

Vle Max Landing Gear Extension

A

181 KIAS

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40
Q

Vmcg Min controllable speed on ground

A

85 KIAS

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41
Q

Max range glide

A

140 KIAS

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42
Q

Turbulent Air Penetration Speed

A

170 KIAS

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43
Q

Max Tire Speed

A

139 Groundspeed

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44
Q

DC Gen Voltage

A

27.5 - 29 VDC. Within 1 VDC of each other.

45
Q

Min battery voltage for GPU start

46
Q

Max Gen Load Allowable Difference

47
Q

Min Battery voltage for BATT start

48
Q

Max Generator Load on Ground

49
Q

Min N1 for Gen Load on the ground

A

(Load : N1)
70-75% : 56%
75-80% : 60%
80-85% : 65%

50
Q

Max Generator Load in Air

A

100% < FL310 < 88%

51
Q

Starter Limit

A

40 sec, 60 sec
40 sec, 60 sec
Then 40 sec, 30 min

52
Q

ITT Normal Operating Range

A

400-800°C

53
Q

Max Continuous ITT

54
Q

Max Reverse ITT

A

750°C for 1 min

55
Q

Max Low Idle ITT

56
Q

Max Transient ITT

A

800-850°C for 5 sec

57
Q

Torque Normal Operating Range

A

400-2230 ft-lbs

58
Q

Max Torque w/ Prop 1600-2000 RPM

A

2230 ft-lbs

59
Q

Max wt on air stair door

60
Q

Max landing gear cycles

A

10 per hour/ 1 per min

61
Q

N1 Normal Operating Range

62
Q

N1 Low Idle Range

63
Q

N1 Hi Idle

A

Approx 70%

64
Q

N1 Max Reverse

A

88% for 1 min

65
Q

N1 Max Acceleration/Transient

A

101.6 to 102.6% for 10 sec

66
Q

N1 Max Continuous

67
Q

N2/Prop RPM Normal Operating Range

A

1600-2000 RPM

68
Q

N2/Prop RPM Max Reverse

A

1900 RPM for 1 min

69
Q

N2/Prop RPM Max during Acceleration/Transient

A

2000-2200 RPM for 5 seconds.
Torque must be limited to 1800ft-lbs for sustained operations above 2000RPM

70
Q

N2/Prop RPM Avoid during ILS

A

1750-1850 RPM

71
Q

Max Ramp Weight (Normal)

A

12,595 lbs

72
Q

Max Takeoff Weight (Normal)

A

12,500 lbs

73
Q

Max Ramp Weight (Restricted)

A

13,595 lbs

74
Q

Max Takeoff Weight (Restricted)

A

13,500 lbs

75
Q

Max Landing Weight

A

12,500 lbs

76
Q

Max ZFW

A

11,000 lbs

77
Q

Time limit on suction lift

78
Q

Time Limit on AVGAS

79
Q

Max Fuel Imbalance

80
Q

Fuel Tank Capacity/Usable

A

549/544 Gal

81
Q

ST-190 Imbalance/Capacity

A

300 lbs/190 gal

82
Q

Min fuel for takeoff/landing per side

83
Q

Min OAT for wing de-ice boots

84
Q

Max OAT for engine anti-ice protection

85
Q

Max OAT for brake deice use

86
Q

Min N1 for brake deice use

87
Q

Max Time for brake deice use gear retracted

88
Q

Cruise Climb Airspeeds

A

Sea Level to 10k - 160 kts
10k-FL210 - 140 kts
FL200-FL250 - 130 kts

89
Q

Max Operating Altitude

90
Q

Max Operating Altitude Unpressurized

91
Q

Max Alt Inoperative Yaw Dampener

92
Q

Min Alt for Yaw Damp/Autopilot Takeoff

A

200/400 FT AGL

93
Q

Min Altitude for Autopilot Cruise

94
Q

Min Alt for Autopilot Approach

A

200 FT AGL

95
Q

Max Sink Rate on Landing

96
Q

Max Crosswind

97
Q

Max Tailwind

98
Q

Max Crosswind on icy runway

99
Q

Max Crosswind on soft field

100
Q

Pneumatic Pressure Normal Operating Range

101
Q

Max Cabin Pressure Differential

102
Q

Max Cabin Pressure Differential with Cracked Windshield Inner Pane

103
Q

Max Cabin Pressure Differential with Cracked Cabin Window

104
Q

Gyro Suction Normal Operating Range

A

2.8-5.9 inHg

105
Q

Prop Deicer Ammeter Normal Operation

106
Q

Va Maneuvering Speed (Flaps DOWN) @ 12,500 lbs

107
Q

Damage to the landing gear may result from the following:

A
  1. Landing on arresting gear cables.
  2. Braking during cable rollover.
  3. Wheel contact with cable risers or boots.
  4. Cable rollover above normal taxi speeds.
108
Q

Prohibited Maneuvers

A
  1. Abrupt control movement.
  2. Unusual g loading.
  3. Bank angle greater than 60° (normal category).
  4. Bank angle greater than 35° (restricted category).
  5. Pitch attitude more than 30° above or below the horizon.
  6. Intentional spins.

C-12 (3 decks)

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