Limitations Flashcards

(75 cards)

1
Q

Max Ramp Weight

A

85,870

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2
Q

Max Takeoff Weight

A

85,517

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3
Q

Max Landing Weight

A

74,957

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4
Q

Max Zero Fuel Weight

A

69,886

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5
Q

FWD Baggage Compartment Capacity

A

3,306

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6
Q

AFT Baggage Compartment Capacity

A

2,534

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7
Q

Max Flap Extension Altitude

A

20,000FT

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8
Q

VLO/VLE

A

250kts

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9
Q

Max Speed to Open Direct Vision Window

A

160kts

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10
Q

MMo

A

.82M

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11
Q

VMo between 10,000-FL290

A

320kts

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12
Q

VMo between 0-8,000ft

A

300kts

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13
Q

VMo between 8,000-10,000ft

A

300-320kts increasing linear

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14
Q

VFE

A
Flaps 1-230kts
Flaps 2-215kts
Flaps 3-200kts
Flaps 4-180kts
Flaps 5-180kts
Full-165kts
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15
Q

Max Tire Groundspeed

A

195kts

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16
Q

Max Tailwind Component

A

10kts

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17
Q

Max Recommended X-Wind

A

Dry Runway-38kts
Wet Runway-31kts
Compacted snow-20kts
Standing Water/Slush/Wet Snow/Dry Snow-18kts
Ice including Wet Ice-12kts
Static Takeoff Due To Compressor Stall-25kts

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18
Q

Kinds of Operation

A

Day/Night
IFR/VFR
Icing
CAT 1 and 2

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19
Q

Minimum Crew

A

Pilot and Copilot

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20
Q

Maneuvering Flight Load Factors

A

Flaps up-2.5 to -1Gs

Flaps down-2 to 0Gs

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21
Q

Max Runway Slope

A

+- 2% paved

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22
Q

Max N1 with Brakes Applied

A

60%

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23
Q

Max Usable Fuel Quantity Per Tank

A

10,392.5lbs

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24
Q

Unusable Quantity Per Tank

A

75lbs

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25
Max Fuel Capacity
20,935lbs
26
Max Fuel Imbalance
794lbs
27
Minimum Fuel Tank Temperature
-37C
28
X-Feed Selector must be off......
Takeoff/Landing
29
APU Brand
Sundstrand APS 2300
30
Minimum Temperature for APU start
-54C
31
Max APU Start Altitude
30,000ft
32
Max APU Operating Altitude
33,000ft
33
Max Altitude for APU GEN
33,000ft
34
Max APU Altitude for Bleed Air
15,000ft
35
Max APU Altitude for Engine Start
21,000ft
36
Max APU Rotor Speed
108%
37
Max APU EGT for Start
1,032C
38
Max APU Continuous EGT
717C
39
APU Starter Limits
Attempt 1-2 60 seconds off | Attempt 3- 5 minutes off
40
What Type of Engines
GE CF34-8E5
41
T/O Thrust Limited to.....
10 minutes
42
Max N1
99.5%
43
Min and Max N2
58.5/99.4%
44
Max ITT Engine Start
815C
45
Max ITT for TOGA
990C
46
Max Continuous ITT
960C
47
Min and Max Oil Pressure
25/95PSI
48
Max Continuous Oil Temperature
155C
49
Max transient Oil Temperature
163C
50
Dry Motoring Start Cycle Limits
Attempt 1- 90 seconds on 5 minutes off Attempt 2-5- 30 seconds on 5 minutes off *May repeat sequence after 15 minute cool down
51
Starting Cycle Limits
Attempt 1-2- 90 seconds on ground 120 seconds in flight 10 second cool down Attempt 3-5- 90 seconds on ground 120 seconds in flight 5 minutes cool down
52
Max Flex Thrust Reduction
25%
53
Max Differential Pressure up to FL370
7.8PSI
54
Max Pressure Differential above FL370
8.34PSI
55
Max Differential Over Pressure
8.77PSI
56
Max Differential Negative Pressure
-.5PSI
57
Max Differential Pressure for T/O and Landing
.2PSI
58
Max Altitude Single Pack
FL310
59
T/O Dataset on MCDU must be set to Engine.......
OAT between 5-10C Visible Moisture up to 1,700AFE Operating on Contaminated Surface
60
T/O Dataset on MCDU must be set to All.....
OAT is below 5C Visible moisture up to 1,700AFE Operating on contaminated surface
61
Max Wiper Speed
253kts
62
Minimum Autopilot Engagement Height
1,000ft AGL
63
TAS,TAT,SAT are not valid below.....
60kts
64
Max Latitude for IRS Stationary Alignment
78.25 N/S
65
CAT II Landing Flap Setting
5
66
RVSM Required Equipment
1 Autopilot 1 Transponder 2 ADCs 1 Altitude Alerting System
67
Max T/O and Landing Altitude
8000'
68
Minimum T/O and Landing Altitude
-1000'
69
Max Temperature for T/O
54C
70
EJET Height
32'3"
71
Wing Span
93'11"
72
Fuselage Length
103'11"
73
Minimum Turning Radius
54'4"
74
Nose Wheel Steering Travel
76 degrees
75
Rudder Pedal Travel
7 degrees