Limitations Flashcards

1
Q

Max Ramp Weight

A

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

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2
Q

Max Takeoff Weight

A

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

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3
Q

Max Landing Weight

A

74,957 lb (LL/LR)

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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

Minimum Runway Width

A

100 ft

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6
Q

Minimum Taxiway Width

A

50 ft

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7
Q

Aircraft Wing Span

A

93’ 11”

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8
Q

Aircraft Length

A

103’ 11”

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9
Q

Aircraft Tail Height

A

32’ 4”

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10
Q

Max Operation Altitude

A

41,000 ft

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11
Q

Max Takeoff & Landing Altitude

A

10,000 ft

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12
Q

Max Temperature T/O & Landing

A

ISA +35C (52C)

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13
Q

Min Temperature T/O & Landing

A

-40C

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14
Q

Runway Slope

A

+/- 2%

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15
Q

Max Tailwind

A

15 kt

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16
Q

Max Single Pack Operations

A

31,000 ft

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17
Q

Vmo (Sea Level - 8,000’)

A

Velocity Maximum Operating Speed
300 kt

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18
Q

Vmo (10,000’ - Mach Transition)

A

Velocity Maximum Operating Speed
320 kt

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19
Q

Mmo

A

Mach Maximum Operating Speed
0.82

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20
Q

Va

A

Maneuvering Speed
240 kt

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21
Q

Vlo (ext)

A

Landing Gear Extension Speed
250 kt

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22
Q

Vle (ret)

A

Landing Gear Retraction Speed
250 kt

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23
Q

Vle

A

Max Speed Operable with L/G Extended
250 kt

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24
Q

Vtire

A

195 kt

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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 kt

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27
Q

Vb (below 10,000 ft)

A

250 kt

28
Q

Vb (10,000 ft and above)

A

270/0.76M, whichever is lower

29
Q

V(wiper ops max)

A

250 kt

30
Q

V(window)

A

160 kt

31
Q

Vfe 1

A

230 kt

32
Q

Vfe 2

A

215 kt

33
Q

Vfe 3

A

200 kt

34
Q

Vfe 4/5

A

180 kt

35
Q

Vfe FULL

A

165 kt

36
Q

Maximum Crosswind Components

A

RCC 6 : 38 kt
RCC 5 : 31 kt
RCC 4 : 20 kt
RCC 3 : 15 kt
RCC 2 : 12 kt
RCC 1 : 8 kt
RCC 0 : PROHIBITED

37
Q

Max Altitude Flaps Extended

A

20,000 ft

38
Q

CAT II Approach Mandatory Flaps Setting

A

Flaps 5

39
Q

Flaps Full - Go Around Flaps

A

Flaps 4

40
Q

Flaps 5 - Go Around Flaps

A

Flaps 2

41
Q

Minimum Battery Voltage

A

22.5 V

42
Q

Maximum Engine Start ITT Temp Limit

A

815 C

43
Q

Starter Cranking Limits (Ground)

A

Starts 1 & 2
90 seconds ON - 10 seconds OFF

Starts 3 - 5
90 seconds ON - 5 minutes OFF

44
Q

Starter Cranking Limits (In Flight)

A

Starts 1 & 2
120 seconds ON - 10 seconds OFF

Starts 3 - 5
120 seconds ON - 5 minutes OFF

45
Q

Dry Motoring Cycle Limits

A

1

90 seconds ON - 5 minutes OFF

30 seconds ON - 5 minutes OFF

46
Q

Max Fuel Capacity

A

20,935 lb

47
Q

Max Fuel Imbalance

A

794 lb

48
Q

Min Fuel Tank Temperature

A

-37C

49
Q

Max Time Allowable Unattended with APU Running (SKW)

A

5 minutes

50
Q

APU Starter Duty Cycle

A

Start Attempt 1 & 2
60 seconds OFF

Third Attempt
5 minutes OFF

51
Q

APU Start/Continuous Min Temp

A

-54C

52
Q

APU Start/Continuous Max Temp

A

ISA +35C (52C)

53
Q

APU Max Start Altitude

A

30,000 ft

54
Q

APU Max Continuous Operation Altitude

A

33,000 ft

55
Q

APU Max Altitude for Continuous Electrical Generator Use

A

33,000 ft

56
Q

APU Max Altitude for Engine Start

A

21,000 ft

57
Q

APU Max Altitude for Bleed Use

A

15,000 ft

58
Q

Max Differential Pressure

A

8.4 PSI

59
Q

Max Differential Overpressure

A

8.8 PSI

60
Q

Max Differential Negative Pressure

A

-0.5 PSI

61
Q

Max Differential Pressure for T/O and Landing

A

0.2 PSI

62
Q

Min Hydraulic Reservoir Temp for Engine Start

A

-18C

63
Q

ENG A/I OAT Temp from 5C - 10C Requirements

A
  • When there is any possibility of encountering visible moisture up to 1,700 ft AFE
  • When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
64
Q

ALL A/I OAT Temp Less than 5C Requirements

A
  • When there is any possibility of encountering visible moisture up to 1,700 ft AFE
  • When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
65
Q

Min AP Engagement Height

A

400 ft

66
Q

Min AP Use Height on Approach

A

50 ft HAT