Limitations Flashcards

1
Q

Max ramp weight

A

84,450 lb (LL) 85,870 lb (LR)

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2
Q

Max T/O weight

A

85,098 lb (LL), 85,517 lb (LR)

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3
Q

Max Landing weight

A

74,957 lb

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4
Q

Max Zero Fuel weight

A

69,467 lb (LL), 69,886 lb (LR)

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5
Q

Min Runway Width

A

100 ft (SKW)

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6
Q

Min Taxiway Width

A

50 ft (SKW)

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7
Q

Wing Span

A

93 ft 11 in

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8
Q

Aircraft Length

A

103 ft 11 in

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9
Q

Tail Height

A

32 ft 4 in

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10
Q

Max Ops Alt

A

41,000 ft

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11
Q

Max T/O & Land Alt

A

10,000 ft

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12
Q

Max Temp T/O & Land

A

ISA +35C (52C)

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13
Q

Min Temp T/O & Land

A

-40*C

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14
Q

Runway Slope

A

+/- 2%

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15
Q

Max tailwind

A

15 knots

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16
Q

Max single pack operations (altitude)

A

31,000 ft

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17
Q

Vmo SL - 8000’

A

300 knots

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18
Q

Vmo 10,000 ft - Mach Transition

A

320

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19
Q

Mmo

A

0.82

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20
Q

Va

A

240

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21
Q

Vlo ext

A

250

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22
Q

Vle ret

A

250

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23
Q

Vle

A

250

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24
Q

Vtire

A

195

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25
Q

V rat deploy max

A

Vmo/Mmo

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26
Q

Vmin (to provide electrical power)

A

130

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27
Q

Vb (below 10,000 ft)

A

250

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28
Q

Vb (10,000 ft and above)

A

270/0.76M (whichever is lower)

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29
Q

V wiper ops max

A

250 (SKW)

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30
Q

Vwindow

A

160

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31
Q

Vfe 1

A

230

32
Q

Vfe 2

A

215

33
Q

Vfe 3

A

200

34
Q

Vfe 4

A

180

35
Q

Vfe 5

A

180

36
Q

Vfe FULL

A

165

37
Q

Crosswind limitation; dry runway

A

38 kt (SKW)

38
Q

Crosswind limitation; wet

A

31 kt (SKW)

39
Q

Crosswind limitation; compact snow

A

20 kt (SKW)

40
Q

Crosswind limitation T/O; dry snow, wet snow, slush, standing water

A

18 kt (SKW)

41
Q

Crosswind limitation T/O; ice and wet ice

A

12 kt (SKW)

42
Q

Max Alt Flaps/Slats Extended

A

20,000 ft

43
Q

CAT II Approach flap setting

A

Mandatory Flaps 5

44
Q

Min battery voltage

A

22.5V

45
Q

Engine Start Max ITT

A

815*C

46
Q

Starter cranking limits: Engine start on the ground

A

Start 1&2: 90 seconds ON, 10 seconds OFF. Start 3-5: 90 seconds ON, 5 minutes OFF.

47
Q

Starter cranking limits: engine start in flight

A

Start 1&2: 120 seconds ON, 10 seconds OFF. Start 3-5: 120 Seconds ON, 5 minutes OFF.

48
Q

Dry motoring duty cycle limits

A

Motoring #1: 90 seconds ON, 5 minutes OFF. Motoring #2-5: 30 seconds ON, 5 minutes OFF. After this the process may be repeated following a 15 minute cool down period.

49
Q

Max fuel capacity

A

20,935 lb.

50
Q

Max fuel imbalance

A

794 lb

51
Q

Min fuel tank temperature

A

-37* C

52
Q

How long to wait before starting the APU after EICAS is energized?

A

30 seconds.

53
Q

Simultaneous use of the APU bleed and the HP cart?

A

Prohibited.

54
Q

APU starter duty cycle

A

Start attempt 1&2: 60 seconds OFF. Start attempt 3: 5 minutes OFF.

55
Q

APU min and max temp: start

A

-54*C -/ ISA+35

56
Q

APU start max altitude

A

30,000 ft

57
Q

APU continuous operation min/max temp

A

-54C / ISA+35 (52C)

58
Q

APU continuous operation max altitude

A

33,000 ft

59
Q

APU continuous operation electrical generator use max altitude

A

33,000 ft

60
Q

APU continuous operation engine start max altitude

A

21,000 ft

61
Q

APU continuous operation max altitude bleed use

A

15,000 ft

62
Q

Max Differential Pressure

A

8.4 psi

63
Q

Max Differential Overpressure

A

8.8 psi

64
Q

Max Differential Negative Pressure

A

-0.5 psi

65
Q

Max Differential Pressure for T/O and Landing

A

0.2 psi

66
Q

Min hydraulic reservoir temp for engine start

A

-18*C

67
Q

Go-around after deployment of thrust reversers?

A

Prohibited

68
Q

When must the TO DATASET MENU be set to ENG?

A

OAT is from 5C to 10C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ENG.

69
Q

When must TO DATASET MENU on the MCDU must be set to ALL?

A

OAT is less than 5*C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ALL.

70
Q

AP minimum engagement height

A

400 ft

71
Q

AP minimum use height

A

50 ft

72
Q

AP minimum use height - Non-Precision Approach

A

MDA

73
Q

When are TAS, TAT and SAT information valid?

A

Only valid above 60 knots

74
Q

When is the standby magnetic compass indication not valid?

A

While transmitting in VHF1.

75
Q

What to verify prior to joining a published segment of an instrument approach?

A

Verify the NAVAID identification visually displayed matches the chart being used. When the identification is not visually displayed, very that the ID matches the chart being used.