Limitations Flashcards

1
Q

Minimum for Reverse

A

40

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2
Q

Vmca (Flaps Approach)

A

86

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3
Q

Vmca (Flaps Up)

A

92

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4
Q

Vsse (Intentional One Engine Inop.)

A

110

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5
Q

Va (Flaps approach or down)

A

111

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6
Q

Vyse (15000 lbs)

A

122

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7
Q

Vxse (15000 lbs)

A

124

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8
Q

Maximum Glide Range (15000 lbs)

A

134

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9
Q

Max Tire Speed

A

139

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10
Q

Minimum in icing conditions

A

140

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11
Q

Vfe (81-157 White Arc)

A

157

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12
Q

VLo (Retraction)

A

163

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13
Q

Vb (Turbulence Penetration)

A

170

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14
Q

Va (Flaps Up)

A

181

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15
Q

VLo (Extension)

A

181

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16
Q

Vfe (Approach)

A

200

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17
Q

Max Windshield de-icing

A

226

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18
Q

Vmo (Below 21000 ft)

A

259

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19
Q

Mmo (Above 21000 ft)

A

.58

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20
Q

Torque Limitations (Gas)- Normal operating range (1000-1700 rpm)

A

0-100%

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21
Q

Torque Limitations (Gas)- Max transient (20 sec)

A

156%

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22
Q

Torque Limitations (Gas)- Max TQ Oil pressure 60-90 psig

A

62%

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23
Q

Torque Limitations (Gas)- Max TQ props above 1700 RPM

A

96%

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24
Q

N1 Speed- min low idle

A

62%

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25
Q

N1 Speed- Max

A

104%

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26
Q

N1 Speed- Max transient

A

104%

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27
Q

ITT Limit- Max idle

A

750 C

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28
Q

ITT Limit- Max reverse

A

760 C

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29
Q

ITT Limit- Cruise climb

A

785 C

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30
Q

ITT Limit- Takeoff/max continuous/max cruise

A

820 C

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31
Q

ITT Limit- Transient (20 sec)

A

850 C

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32
Q

ITT Limit- Max transient starting (5 sec)

A

1000 C

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33
Q

Oil temp- Starting/idle

A

-40 C- 110 C

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34
Q

Oil temp- Normal/reverse

A

0- 99 C

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35
Q

Oil temp- Max transient (10 min)

A

99 C- 110 C

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36
Q

Oil temp- Max

A

110 C

37
Q

Oil pressure- Min low idle

A

60 psi

38
Q

Oil pressure- Caution range (Torque limited to 62%)

A

60-90 psi

39
Q

Oil pressure- Normal operating

A

90-135 psi

40
Q

Oil pressure- Transient

A

40-200 psi

41
Q

Oil pressure- Max starting

A

200 psi

42
Q

DC Power- Max (62%-70% N1)

A

75%

43
Q

DC Power- Max (Below 34000 ft)

A

100%

44
Q

DC Power- Max (Above 34000 ft)

A

95%

45
Q

DC Power- Normal VDC

A

27.5-29.0

46
Q

AC Power- Hz (Frequency)

A

390-410

47
Q

AC Power- Normal VAC

A

110-120

48
Q

Climb speeds- Up to 10000 ft

A

160 KIAS

49
Q

Climb speeds- 10000-20000 ft

A

140 KIAS

50
Q

Climb speeds- 20000-25000 ft

A

130 KIAS

51
Q

Climb speeds- 25000-35000 ft

A

120 KIAS

52
Q

N2 rpm- min idle

A

1050

53
Q

N2 rpm- normal operating range

A

1450-1700

54
Q

N2 rpm- max reverse

A

1650

55
Q

N2 rpm- max

A

1700

56
Q

N2 rpm- transient (5 sec)

A

1870

57
Q

Weight (normal)- max ramp wt

A

15100 lbs

58
Q

Weight (normal)- max t/o wt

A

15000 lbs

59
Q

Weight (normal)- max ldg wt

A

14000 lbs

60
Q

Weight (normal)- zero fuel wt

A

11500 lbs

61
Q

Weight (normal)- max baggage cmpt wt

A

550 lbs

62
Q

Weight (normal)- max airstair door wt

A

300 lbs

63
Q

Auto pilot limitations

A
  1. Airspeed 259 KIAS/.58 Mac max
  2. Don’t use below 200’ AGL
  3. Seated and seatbelts
  4. Preflight first flight of the day
64
Q

Brake de-ice limitations

A
  1. Below 85% N1 with surface de-ice
  2. Above 15 C
  3. More than 10 min w/ wheels retracted
  4. Single engine operations
65
Q

Fuel system- max imbalance

A

300 lbs

66
Q

Fuel system- min in each main for t/o

A

265 lbs

67
Q

Fuel system- max w/ fuel press light

A

10 hrs

68
Q

Fuel system- ttl usable fuel qty

A

539 gal

69
Q

Fuel system- In fuel in aux’s

A

Mains must be full

70
Q

Gear cycle limitations

A
  1. 6 cycles at one cycle every 5 min

2. 15 min rest after 6 cycles

71
Q

G load- Flaps up

A

-1.24 to +3.10

72
Q

G load- Flaps approach or down

A

0.0 to +2.0

73
Q

CG- @ 15000lbs at t/o

A

185.0-192.1

74
Q

CG- @ 14000lbs at ldg

A

182.5-192.1

75
Q

CG- @ 11800lbs or less

A

177.0-192.1

76
Q

Pneumatic pressure- normal op range

A

12-20 psi

77
Q

Pneumatic pressure-max

A

20 psi

78
Q

Gyro suction gage- normal SL to 15000 ft

A

4.3-5.9 in

79
Q

Gyro suction gage- normal 15000 to 35000 ft

A

2.8-4.3 in

80
Q

Prop de-ice ammeter- normal range

A

26-32 amps

81
Q

Temp- Max SL to 25000’

A

ISA +37

82
Q

Temp- max above 25000’

A

ISA +31

83
Q

Pneumatic boot limit

A

No operations below -40 C

84
Q

Rudder boost

A

must be operative

85
Q

Yaw damp

A

May be inoperative for a/c with Raisbeck Dual Aft Body Strakes provided flight is conducted at or below 18500’ PA.

86
Q

Autofeather

A

Must be operational for all flights and armed for t/o, climb, and approach

87
Q

Two engine best rate of climb Vy

A

137 kts

88
Q

Two engine best angle of climb

A

122 Vx