Limitations Flashcards

1
Q

Max T/O wt

A

85,517

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2
Q

Max landing wt

A

74,957

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3
Q

Max zero fuel wt

A

69,886

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4
Q

Max Ramp weight

A

85,870

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5
Q

Max aft cargo

A

2,535

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6
Q

Max fwd cargo

A

3,306

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7
Q

Min rwy width SKW

A

100 ft

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8
Q

Wing span

A

93’11”

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9
Q

Aircraft length

A

103’11”

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10
Q

Main to main distance

A

17’1”

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11
Q

Tail height

A

32’4”

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12
Q

Max operating altitude

A

41,000

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13
Q

Max T/O and landing altitude

A

8,000 ft

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14
Q

Max temp T/O & landing

A

ISA + 35C

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15
Q

Min. Temp T/O and landing

A

-40C

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16
Q

Rwy slope

A

+/- 2%

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17
Q

Max tail wind

A

15kt

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18
Q

Max altitude single pack

A

31,000

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19
Q

Vmo SL-8,000ft

A

300

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20
Q

Vmo 10,000 -Mach transition

A

320

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21
Q

Mmo

A

.82

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22
Q

Va

A

240

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23
Q

Vlo ext

A

250

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24
Q

Vle ret

A

250

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25
Q

Vle

A

250

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26
Q

V tire

A

195

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27
Q

V rat deploy max

A

Vmo/Mmo

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28
Q

Vmin rat

A

130

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29
Q

Vb below 10,000

A

250

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30
Q

Vb above 10,000

A

270/.76 Mach whichever is lower

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31
Q

V wiper max

A

250 SKW

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32
Q

V window

A

160

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33
Q

Vfe 1

A

230

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34
Q

Vfe 2

A

215

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35
Q

Vfe 3

A

200

36
Q

Vfe 4

A

180

37
Q

Vfe 5

A

180

38
Q

Vfe full

A

165

39
Q

Dry runway max crosswind

A

38kt

40
Q

Wet runway max cross wind

A

31kt

41
Q

Runway with compacted snow max cross wind

A

20kt

42
Q

Runway with standing water/slush/wet snow/dry snow max cross wind

A

18 kt

43
Q

Runway with ice max cross wind

A

12kt

44
Q

Max crosswind static take off

A

30 kt

45
Q

Max alt flaps/slats extended

A

20,000ft

46
Q

Enroute ops flaps/slats

A

Prohibited

47
Q

Min spoiler speed

A

180 kt

48
Q

Cat. II approach

A

Mandatory flaps 5

49
Q

Landing flaps full

A

Go-around flaps 4

50
Q

Landing flaps 5

A

Go-around flaps 2

51
Q

Min battery voltage

A

22.5

52
Q

Max engine start temp

A

815C

53
Q

Min temp engine start

A

-40C

54
Q

Min oil pressure start

A

25 psi

55
Q

Starter limit 1 & 2

A

90s on, 10 sec off

56
Q

Starter limit 3-5

A

90s on, 5 min off

57
Q

Starter limit inflight 1 & 2

A

120s on, 10s off

58
Q

Starter limit inflight 3-5

A

120s on, 5 min off

59
Q

Dry motoring attempt 1

A

90s on, 5 min off

60
Q

Dry motoring limit 2-5

A

30s on, 5 min off

61
Q

Start with tailwind must be….

A

Manually aborted

62
Q

ATTCS off is…..

A

Not authorized

63
Q

Max fuel capacity

A

20,935

64
Q

Max fuel imbalance

A

794 pounds

65
Q

Min fuel tank temp

A

-40C

66
Q

Crossfeed must be…..

A

Off for take-off and landing

67
Q

Apu start attempt 1 & 2

A

60s off

68
Q

Apu starter duty cycle attempt

A

5 min off

69
Q

APU start temperature range

A

-54C to ISA + 35

70
Q

APU max start altitude

A

30,000ft

71
Q

APU continuous temp range

A

-54C to ISA + 35C

72
Q

APU continuous max altitude

A

33,000ft

73
Q

APU continuous electric gen use

A

33,000ft

74
Q

Apu max continuous altitude bleed use

A

15,000ft

75
Q

APU continuous altitude engine start

A

21,000ft

76
Q

Max differential pressure up to 37,000ft

A

7.8

77
Q

Max differential pressurization above 37,000ft

A

8.34

78
Q

Max differential over pressure

A

8.77

79
Q

Max diff neg pressure

A

-.5

80
Q

Max diff press t/o and lnd

A

.2

81
Q

Min reservoir temp for eng start

A

-18C

82
Q

Temp 5 to 10 OAT

A

Eng must be selected if moisture below 1,700 ft or

Contaminated surfaces

83
Q

Temp below 5C OAT

A

All must be selected with moisture below 1,700 AFE or

Contaminated surfaces

84
Q

In flight with either 1 or 2 ice detectors failed

A

Temp below 10 TAT A/I on

85
Q

Min autopilot engagement height

A

400ft

86
Q

Min autopilot use height

A

50ft

87
Q

Min autopilot us non-precision appoach

A

MDA