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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
Max Differential Negative Pressure
-0.5 PSI
26
Max Differential Overpressure
8.8 PSI
27
Max Differential Pressure
8.4 PSI
28
Max Differential Pressure for Takeoff & Landing
0.2 PSI
29
Max Fuel Capacity
20,935 lbs
30
Max ITT Start
815C
31
Max Landing Weight (LR)
74,957 lbs
32
Max Ramp Weight (LL)
85,450 lbs
33
Max Tailwind
15 knots
34
Max Takeoff Weight (LR)
85,517 lbs
35
Max Takeoff/Landing Altitude
10,000'
36
Max Temperature for T/O & Landing
ISA + 35 (52C)
37
Max Zero Fuel Weight (LL)
69,467 lbs
38
Max Zero Fuel Weight (LR)
69,886 lbs
39
Max Fuel Imbalance
794 lbs
40
Max Operating Altitude
41,000'
41
Max Single Pack Operations
31,000'
42
Max Takeoff Weight (LL)
85,098 lbs
43
Minimum Autopilot Engagement Height
400' AGL
44
Minimum Autopilot Use Height on Approach
50' HAT (Precision)
45
Minimum Fuel Tank Temperature
-37C
46
Minimum Reservoir Temperature for Engine Start
-18C
47
Minimum Runway Width
100'
48
Minimum Taxi Width
50'
49
Minimum Temperature for T/O & Landing
-40C
50
Mmo
.82M
51
Runway Slope
+/- 2%
52
Set A/I ALL when...
OAT is below 5 degrees and visible moisture at 1,700' AFE or below, OR ground is wet/contaminated
53
Set A/I ENG when....
OAT is 5-10 degrees and visible moisture at 1,700' AFE or below, OR ground is wet/contaminated
54
Tail Height
32'4"
55
Takeoff Crosswind Limitation (Compacted Snow)
20 knots
56
Takeoff Crosswind Limitation (Dry snow, wet snow, slush, or standing water)
18 knots
57
Takeoff Crosswind Limitation (Dry)
38 knots
58
Takeoff Crosswind Limitation (Ice)
12 knots
59
Takeoff Crosswind Limitation (Wet Ice)
12 knots
60
Takeoff Crosswind Limitation (Wet)
31 knots
61
Va
240 knots
62
Vb
Below 10,000': 250 knots At or above 10,000': 270 knots or .76M, whichever is lower
63
Vfe 1
230 knots
64
Vfe 2
215 knots
65
Vfe 3
200 knots
66
Vfe 4
180 knots
67
Vfe full
165 knots
68
Vlo
250 knots
69
Vmin (to provide electrical power)
130 knots
70
Vmo
SL - 8,000' : 300 knots 10,000' - Mach Transition : 320 knots
71
Vrat Deploy Max
Vmo/Mmo
72
Vtire
195 knots
73
Vwindow
160 knots
74
Vwiper Ops
250 knots
75
Wing Span
93'11"

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