Limitations Flashcards

1
Q

Max Takeoff Weight

A

114,150 lbs

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2
Q

Max Landing Weight

A

97,000 lbs

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3
Q

Max Zero Fuel Weight

A

90,150 lbs

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4
Q

Maximum wind for takeoff and landing

A

50 knots

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5
Q

Maximum crosswind (including gusts) for takeoff and landing

A

28 knots

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6
Q

Maximum headwind for CAT 2/3 approaches

A

25 knots

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7
Q

Maximum crosswind including gusts for autoland

A

15 knots

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8
Q

Maximum crosswind with landing visibility less than 3/4 or 4000 RVR

A

15 knots

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9
Q

Maximum takeoff and landing tailwind component

A

10 knots

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10
Q

Maximum runway slope (uphill, downhill)

A

+2.0%, -2.0%

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11
Q

Maximum runway slope for autolands (uphill, downhill)

A

+1.0%, -1.0%

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12
Q

Flap maneuvering load acceleration limits flaps up

A

-1.0 to +2.5 G

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13
Q

Flap maneuvering load acceleration limits flaps down (1,2,3,4,5, and Full)

A

0.0 to +2.0 G

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14
Q

Maximum operating altitude

A

41,000 feet

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15
Q

Maximum take off and landing altitude

A

8000 feet

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16
Q

Maximum SAT for take off, landing, and ground start

A

52°C

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17
Q

Maximum altitude with flaps extended

A

20,000 feet

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18
Q

Minimum SAT for take off, landing, and ground start

A

-40°C

In the event of a landing below -40°C, the airplane may not take off without further maintenance inspection.

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19
Q

Maximum operating airspeed

A

Vmo

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20
Q

Maximum operating Mach number

A

.82 (Mmo)

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21
Q

Maximum airspeed for RAT operation

A

Vmo/Mmo

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22
Q

Turbulent airspeed (below 10,000 feet)

A

250 KIAS

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23
Q

Turbulent airspeed (at or above 10,000 feet)

A

270 KIAS/.76M

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24
Q

Tire limit groundspeed

A

195 knots

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25
Maximum airspeed for windshield wiper operation
250 KIAS
26
Maximum airspeed for windshield wiper operation failed in the non-parked position
320 KIAS
27
Maximum airspeed to open flight deck window
160 KIAS
28
Maximum gear extension speed (Vlo)
265 KIAS
29
Maximum gear extended speed (Vle)
265 KIAS
30
Maximum gear retraction speed (Vlo)
235 KIAS
31
Maximum flap operating speeds
``` Flaps 1 - 230 Flaps 2 - 215 Flaps 3 - 200 Flaps 4 - 180 Flaps 5 - 180 Full - 165 ```
32
Design maneuvering speed
240 KIAS Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds below
33
Definition of icing conditions
OAT (on the ground and for take takeoff) or TAT (in-flight) is 10°C or below, and Visible moisture in any form is present such as clouds, fog with visibility of 1 mile or less, rain, snow, sleet and ice crystals, or When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by engines, freeze on engines, nacelles, or engine sensor probe.
34
During taxi out and take off, the MCDU TO DATASET MENU REF | A/I must be set to
ALL when OAT is 10°C or below and icing conditions exist or are anticipated
35
Approved Fuels
Jet A and A-1 When using Jet A type fuel with ambient temperatures of -30°C or below, the fuel temperature prior to flight must be verified to be above -29°C
36
Maximum usable fuel is
14,440 lbs per tank
37
Maximum unusable fuel is
101.5 lbs per tank
38
Minimum fuel temperature
-40°C
39
Maximum permissible fuel imbalance between left and right main tanks during all phases is
800 lbs
40
The XFEED selector must be set to ... during takeoff and landing
OFF
41
Maximum altitude for a single pack operation
31,000 feet
42
Maximum relief differential pressure up to 37,000 feet
7.8
43
Maximum relief differential pressure above 37,000 feet
8.3
44
Maximum differential Overpressure
8.7
45
Maximum negative differential pressure
-0.5
46
Maximum differential pressure for takeoff and landing
0.2
47
Brakes cooling limitation
Do not take off with amber brake temperature indicators
48
Max Ramp Weight
114,500 lbs
49
Do not hold in icing conditions with
Flaps/Slats extended
50
Maximum altitude with flaps/slats extended is
20,000 feet
51
During takeoff or go around, do not turn the autopilot on until above
400 feet AGL
52
During landing, unless executing an auto landing with AUTOLAND 1 engaged, turn off the autopilot
Prior to 50 feet AGL
53
Autoland weight limitations
Minimum 69,500 lbs | Maximum 97,000 lbs
54
FMS Speed is
Not authorized for takeoff
55
Engine type
CF-34-10E
56
Starter duty cycle 1st and 2nd
Maximum 90 seconds ON (ground) 120 seconds ON (in flight) Followed by 10 seconds OFF
57
Starter duty cycle 3rd through 5th
Maximum 90 seconds ON (ground) 120 seconds ON (in flight) Followed by 5 minutes OFF
58
Dry-Motoring Cycle 1st
Maximum 90 seconds ON Followed by 5 minutes OFF
59
Dry-Motoring Cycle 2nd-5th
Maximum 30 seconds ON Followed by 5 minutes OFF After 5 motorings, a cycle may be repeated following a 15 minute cool down period
60
Maximum reverse thrust is not permitted at airspeeds
Below 60 KIAS Below 60 KIAS reduce to IDLE
61
APU Starter Limits 1st and 2nd
APU Control Master START/ON | Followed by 60 seconds OFF
62
APU Starter Limits 3rd cycle
APU Control Master START/ON | Followed by 5 minutes OFF
63
APU Operational limit temperature
Minimum -54°C | Maximum ISA + 35°C
64
APU Maximum altitude for Start
30,000 feet
65
APU Maximum altitude for operation Electrical
33,000 feet
66
APU Maximum altitude for operation Bleed
15,000 feet
67
APU Maximum altitude for operation to assist engine start
21,000 feet
68
Resetting a .... or .... circuit breaker is prohibited
Fuel boost pump or fuel indication system
69
On ground, primary altimeters must be within .... feet of each other and within .... feet of field elevation
75 feet of both
70
Maximum in flight difference between primary altimeters for RVSM
200 feet
71
Minimum Turning Width
70 ft 3 in
72
Maximum crosswind braking action medium.
20 knots
73
Maximum crosswind braking action poor.
10 knots
74
Aircraft Wingspan
94’3”
75
Aircraft Length
118’11”