Limits Flashcards

1
Q

Vmo/Vne

A

Max dive/level flight do not exceed speed (up to 15,500’)

227 KIAS

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2
Q

Vmca

A

Minimum controllable airspeed

86 KIAS

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3
Q

Vx

A

Best angle of climb

102 KIAS

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4
Q

Vy

A

Best rate of climb

108 KIAS

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5
Q

Vsse

A

Minimum safe 1 engine inop speed

91 KIAS

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6
Q

Vxse

A

Best angle of climb single engine

102 KIAS

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7
Q

Vyse

A

Best rate of climb single engine

110 KIAS

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8
Q

Vfe (full)

A

Max flap extension/extended speed (full)

140 KIAS

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9
Q

Vfe (appr)

A

Maximum flap extension/extended speed (appr)

174 KIAS

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10
Q

Vlr

A

Max landing gear retraction speed

145 KIAS

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11
Q

Vle

A

Max landing gear extension speed

155 KIAS

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12
Q

Va

A

Maneuvering speed

153 KIAS

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13
Q

Vmcg

A

Minimum controllable speed on the ground

63 KIAS

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14
Q

Max range glide

A

130 KIAS

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15
Q

Max endurance glide

A

102 KIAS

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16
Q

DC electrical voltage

A

28.25 +/- .8 VDC

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17
Q

Minimum battery voltage for APU(GPU) charge

A

18 VDC

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18
Q

Minimum battery voltage APU(GPU) start

A

20 VDC

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19
Q

Minimum battery voltage for BATT start

A

22 VDC

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20
Q

Starter limit cycle

A

40 secs on, 60 secs off x2, 40 secs on, 30 minutes off

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21
Q

ITT Normal operating range

A

400-790 deg C

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22
Q

ITT Max allowable

A

790 deg C

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23
Q

ITT Max continuous

A

790 deg C

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24
Q

ITT Max reverse

A

790 deg C

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25
Q

ITT Max acceleration (up to 2 sec)

A

850 deg C

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26
Q

ITT Max low idle

27
Q

ITT Max cruising

28
Q

ITT Max cruise climb

29
Q

ITT Max start ___(cutoff), ___(2 sec)

A

925 deg C, 1090 deg C

30
Q

Torque Normal operating range

A

400-1315 ft-lb

31
Q

Torque Max @ 1900 rpm

A

1520 ft-lb

32
Q

Torque Max @ 2200 rpm

A

1315 ft-lb

33
Q

Torque Max acceleration

A

2100 ft-lb

34
Q

N1 normal operating range

35
Q

N1 Low idle range

36
Q

N1 High idle

37
Q

N1 Max reverse

38
Q

N1 Max acceleration

39
Q

N1 Max continuous

40
Q

Np Normal operating range

A

1800-2200 rpm

41
Q

Np Max reverse

42
Q

Np Max during acceleration

43
Q

Oil temp normal operating range

A

10-99 deg C

44
Q

Oil temp Max

45
Q

Oil pressure normal operating range

A

85-100 psi

46
Q

Oil pressure Max

47
Q

Oil pressure Min

48
Q

Max ramp weight

49
Q

Max takeoff weight

50
Q

Max landing weight

51
Q

Vmo (above 15,500’)

A

Max dive/level flight speed decreases from 227 KIAS at 4 KIAS per 1000’ above 15,500’

52
Q

Acceleration G limits

A

At Max flying weight

Clean: +3g to -1g

Full flaps: +2g to 0g

53
Q

Pneumatic pressure normal operating range

54
Q

Max sink rate on landing

55
Q

Max crosswind

56
Q

Max cabin pressure differential

57
Q

Gyro suction normal operating range

A

4.3-5.9 psi

58
Q

Min oxygen requirements

A

Local: 1000 psi

XC: 1500 psi

59
Q

Prop deicer ammeter normal operation

A

14-18 amps

60
Q

Minimum crew

A

PIC and copilot

61
Q

Minimum crew with passengers

A

Aircraft Commander and 2p, IUT, PUI, SNA

62
Q
  1. N1 51-54%. Ground operations above ___ foot pressure altitude (PA) may produce idle speeds as high as __ % N1 with condition levers at low idle.
A

3,500’

83%

63
Q
  1. Normal oil pressure is __ to ___ PSIG at power settings above 27,000 rpm (72%) N1, oil pressure below __ PSIG is undesirable, and may be used only for completion of flight, and then at a reduced power setting. Low oil pressure should be corrected prior to next flight. During ground operations oil pressures below __ PSIG require engine shutdown; during flight, oil pressure below __ PSIG is unsafe and requires and requires either engine shutdown or use of minimum power until a landing can be made.
A

85-100
85
40
40

64
Q
  1. This value is limited to two seconds. If ITT is likely to exceed ___ deg C, discontinue start.
A

Max ITT on engine start (1090 deg C for 2 seconds)

925 deg C