Limitations Flashcards

1
Q

Max Ramp Weight (LR)

A

85,870

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2
Q

Aircraft Length

A

103’ 11”

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3
Q

APU Max Altitude

A

33,000’

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4
Q

APU Max Altitude for Bleed Use

A

15,000’

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5
Q

APU Max Generator Altitude

A

33,000’

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6
Q

APU Max Starting Altitude

A

30,000’

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7
Q

APU Max Starting Temperature

A

ISA + 35C

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8
Q

APU Maximum Altitude (Engine Start)

A

21,000’

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9
Q

APU Minimum Starting Temperature

A

-54C

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10
Q

APU Starter Duty Cycle

A

1 & 2: 60 Seconds OFF
3rd: 5 Minutes OFF

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11
Q

Autopilot Minimum Use Height (Non-Precision Approach)

A

MDA

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12
Q

Battery Minimum Voltage

A

22.5V

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13
Q

CAT II Approach Flaps

A

Mandatory Flap 5

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14
Q

Cranking Limits (Dry Motor)

A

1st Attempt: 90 seconds ON, 5 minutes OFF
2-5: 30 seconds ON, 5 minutes OFF

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15
Q

Cranking Limits (Ground)

A

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

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16
Q

Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than ____

A

25 knots

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17
Q

Landing Crosswind Limitation (RCC 0)

A

Prohibited

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18
Q

Landing Crosswind Limitation (RCC 1)

A

8 knots

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19
Q

Landing Crosswind Limitaiton (RCC 2)

A

12 knots

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20
Q

Landing Crosswind Limitation (RCC 3)

A

15 knots

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21
Q

Landing Crosswind Limitation (RCC 4)

A

20 knots

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22
Q

Landing Crosswind Limitation (RCC 5)

A

31 knots

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23
Q

Landing Flaps FULL Go-Around Flaps

A

Flaps 4

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24
Q

Max Altitude Flaps/Slats Extended

A

20,000’

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25
Q

Max Differential Negative Pressure

A

-0.5 PSI

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26
Q

Max Differential Overpressure

A

8.8 PSI

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27
Q

Max Differential Pressure

A

8.4 PSI

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28
Q

Max Differential Pressure for Takeoff & Landing

A

0.2 PSI

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29
Q

Max Fuel Capacity

A

20,935 lbs

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30
Q

Max ITT Start

A

815C

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31
Q

Max Landing Weight (LR)

A

74,957 lbs

32
Q

Max Ramp Weight (LL)

A

85,450 lbs

33
Q

Max Tailwind

A

15 knots

34
Q

Max Takeoff Weight (LR)

A

85,517 lbs

35
Q

Max Takeoff/Landing Altitude

A

10,000’

36
Q

Max Temperature for T/O & Landing

A

ISA + 35 (52C)

37
Q

Max Zero Fuel Weight (LL)

A

69,467 lbs

38
Q

Max Zero Fuel Weight (LR)

A

69,886 lbs

39
Q

Max Fuel Imbalance

A

794 lbs

40
Q

Max Operating Altitude

A

41,000’

41
Q

Max Single Pack Operations

A

31,000’

42
Q

Max Takeoff Weight (LL)

A

85,098 lbs

43
Q

Minimum Autopilot Engagement Height

A

400’ AGL

44
Q

Minimum Autopilot Use Height on Approach

A

50’ HAT (Precision)

45
Q

Minimum Fuel Tank Temperature

A

-37C

46
Q

Minimum Reservoir Temperature for Engine Start

A

-18C

47
Q

Minimum Runway Width

A

100’

48
Q

Minimum Taxi Width

A

50’

49
Q

Minimum Temperature for T/O & Landing

A

-40C

50
Q

Mmo

A

.82M

51
Q

Runway Slope

A

+/- 2%

52
Q

Set A/I ALL when…

A

OAT is below 5 degrees and visible moisture at 1,700’ AFE or below, OR ground is wet/contaminated

53
Q

Set A/I ENG when….

A

OAT is 5-10 degrees and visible moisture at 1,700’ AFE or below, OR ground is wet/contaminated

54
Q

Tail Height

A

32’4”

55
Q

Takeoff Crosswind Limitation (Compacted Snow)

A

20 knots

56
Q

Takeoff Crosswind Limitation (Dry snow, wet snow, slush, or standing water)

A

18 knots

57
Q

Takeoff Crosswind Limitation (Dry)

A

38 knots

58
Q

Takeoff Crosswind Limitation (Ice)

A

12 knots

59
Q

Takeoff Crosswind Limitation (Wet Ice)

A

12 knots

60
Q

Takeoff Crosswind Limitation (Wet)

A

31 knots

61
Q

Va

A

240 knots

62
Q

Vb

A

Below 10,000’: 250 knots
At or above 10,000’: 270 knots or .76M, whichever is lower

63
Q

Vfe 1

A

230 knots

64
Q

Vfe 2

A

215 knots

65
Q

Vfe 3

A

200 knots

66
Q

Vfe 4

A

180 knots

67
Q

Vfe full

A

165 knots

68
Q

Vlo

A

250 knots

69
Q

Vmin (to provide electrical power)

A

130 knots

70
Q

Vmo

A

SL - 8,000’ : 300 knots
10,000’ - Mach Transition : 320 knots

71
Q

Vrat Deploy Max

A

Vmo/Mmo

72
Q

Vtire

A

195 knots

73
Q

Vwindow

A

160 knots

74
Q

Vwiper Ops

A

250 knots

75
Q

Wing Span

A

93’11”