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+4)+"@## > Limitations > Flashcards

Limitations Flashcards

1
Q

Max ramp weight crj200

A

53250lbs

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2
Q

Max takeoff weight crj200

A

53000lbs

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3
Q

Max landing weight crj200

A

47000lbs

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4
Q

Max zero fuel weight crj200

A

44000lbs

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5
Q

Max aft cargo crj200

A

3500lbs

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6
Q

Vmo/Mmo crj200

A

335KIAS/.85M

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7
Q

Vma/Mma crj200

A

280KIAS/.75M

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8
Q

Vfe/Vfo

8, 20, 30, 45

Crj200

A

200/230, 200/230, 185, 170

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9
Q

Vle/Vlo/Vlr

Crj200

A

250, 250, 200

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10
Q

Xwind t/o and ldg limits

dry, wet, contaminated

crj200

A

27, 22, 15kts

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11
Q

Cat 2/3 xwind limits

A

13kts

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12
Q

Max tailwind takeoff and ldg

A

10kts

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13
Q

Max headwind, cat 2/3

A

19kts

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14
Q

Max fuel imbalance

A

800lbs

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15
Q

Max fuel imbalance for takeoff crj900

A

300lbs

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16
Q

Min go around fuel per side

Crj200

A

450lbs

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17
Q

Hydraulic pressure range

A

2800-3200psi

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18
Q

Hydraulic quantities crj200

A

45-85%

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19
Q

Max ramp weight crj900

A

85000lbs

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20
Q

Max takeoff weight crj900

A

84500lbs

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21
Q

Max ldg weight crj900

A

75100lbs

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22
Q

Max zero fuel weight crj900

A

70750lbs

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23
Q

Max aft cargo crj900

A

2892lbs

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24
Q

Max foreword cargo crj900

A

1700lbs

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25
Q

Vmo/Mmo/rvsm crj900

A

335KIAS/.842M/.82M

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26
Q

Vma/Mma crj900

A

280KIAS/.75M

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27
Q

Vfe

1,8,20,30,45

Crj900

A

230, 230, 220, 185, 170KIAS

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28
Q

Vle/Vlo/Vlr

Crj900

A

220KIAS

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29
Q

Max xwind takeoff

Dry, wet, contaminated

Crj900

A

35, 27, 15kts

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30
Q

Max xwind ldg

Dry, wet, contaminated

Crj900

A

32, 27, 15kts

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31
Q

Max tire speed crj200

A

182KIAS

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32
Q

Max tire speed crj900

A

195KAIS

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33
Q

Min go around fuel per side

Crj900

A

600lbs

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34
Q

Min hydraulic quantities

Crj900

A

34, 29, 31%

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35
Q

APU max operating altitude crj200

A

37000’

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36
Q

APU max starting altitude crj200

A

30000’

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37
Q

APU min start temp crj200

A

-40C

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38
Q

Max APU bleed altitude crj200

A

15000’

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39
Q

Max APU door speed crj200

A

300KIAS

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40
Q

Max single pack ops crj200

A

25000’

41
Q

Min altitude for spoilers

A

300’agl

42
Q

Min autopilot altitude (agl) on takeoff, visual, precision, A mode, and single engine (900)

A

600’, 400’, 80’, 650’, 110’

43
Q

Max temp for takeoff crj200

A

50C

44
Q

Max temp for takeoff crj900

A

ISA+35C

45
Q

Min temp for takeoff

A

-40C

46
Q

Max APU altitude crj900

A

41000’

47
Q

Max APU start altitude crj900

A

37000’

48
Q

Max APU bleed altitude crj900

A

25000’

49
Q

Max APU door speed APU off, crj900

A

220KIAS

50
Q

Max single pack

More than 82 occupants

Crj900

A

25000’

51
Q

Max single pack ops

Less than 83 occupants

Crj900

A

31000’

52
Q

Flap retraction speed on flaps 8 takeoff

Crj200

A

V2+12

53
Q

Flap retraction speeds on flaps 20 takeoff

Crj200

A

V2+12 flaps 8

V2+20 flaps 0

54
Q

Flap retraction speeds on flaps 8 takeoff

Crj900

A

V2+12 flaps 1

Vt-15 flaps 0

55
Q

Flap retraction speeds on flaps 20 takeoff

Crj900

A

V2+12 flaps 8

V2+20 flaps 1

Vt-15 flaps 0

56
Q

Max glideslope angle for autopilot

A

3.5

57
Q

HGS glideslope limits

Primary and vmc

A

2.5-4.5

58
Q

HGS glideslope limits A1 mode

A

2.5-3.5

59
Q

HGS glideslope limits

AIII mode

A

2.5-3.0

60
Q

HGS modes available for use with abnormal landing flap configurations

A

Primary only

61
Q

Fuel tanks quantities pressure refueling

Crj200

A

Wings-4760lbs each
Center-4998lbs
Total-14518lbs

62
Q

Fuel tanks quantities when pressure refueling

Crj900

A

Wings 7492lbs
Center 4610lbs
Total 19594lbs

63
Q

Glideslope angle limits for scda

A

2.9-3.5

64
Q

Min fuel temp for takeoff

A

+5

65
Q

No more than 500lbs fuel in center tank unless

A

Wings are each above 4400

OR

Wings are above 2000 and max zero fuel weight is reduced by the amount above 500lbs in the center tank

66
Q

Bleeds will be set on ________ for takeoff with anti-ice on.

Crj200

A

APU

67
Q

Max windshield wiper speed crj200

A

220KIAS

68
Q

Max windshield wiper speed

Crj900

A

250KIAS

69
Q

On the ground with an OAT of 10C or below in visible moisture

A

cowl anti ice must be on.

70
Q

On ground with temps below 5C in any condition

A

wing anti ice must be on for taxi, except after deicing.

71
Q

On ground with an OAT of 5 or below and visible moisture

A

wing and cowl anti-ice must be on.

72
Q

Icing conditions exist in flight when

A

TAT is 10C or below and SAT is above -40C or the ice message appears on the EICAS.

73
Q

Wing anti ice can be turned off in icing conditions if

A

IAS is above 230 and there is no ice message on EICAS.

74
Q

On the crj200 wing anti-ice must be on

A

when descending with a TAT of 10C or below regardless of conditions until deployment of flaps for final approach.

75
Q

Crank limits crj200

A

Attempt 1 - 60s on, 10s off
Attempt 2 - 60s on, 10s off
Attempt 3+ - 60s on, 5 minutes off

76
Q

Crank limits crj900

A

Attempt 1 - 90s on 10s off
Attempt 2 - 90s on 10s off
Attempts 3-5 - 90s on 5 minutes off

77
Q

Max ITT for engine start in air/on ground

A

120/90C

78
Q

Dry motor limits for crj200

A

Attempt 1 - 90s on, 5 minutes off

Attempts 2+ - 30s on 5 minutes off

79
Q

Dry motor limits crj900

A

Attempt 1 - 2 minutes on 10s off

Attempts 2-5 - 1 minute on 5 minutes off

80
Q

Max crosswind landing from right seat

A

20kts

81
Q

If cold soaked below -30C for 8 hours before starting you must

A

dry motor for 1 minute to verify N1 rotation.

82
Q

After starting a cold soaked airplane (8 hours below -30C) you must

A

Actuate the reversers until deploy and stow times are 5 seconds (crj200) or 2 seconds (crj900).

83
Q

Continuous ignition is required if (7)

A

In heavy precipitation
In the vicinity of thunderstorms
In moderate or heavy turbulence
In windshear conditions
When departing from a contaminated runway
When departing after being deiced
For takeoff in crosswinds above 15kts (crj200)

84
Q

In the crj900 for winds between 5 and 30kts that are more than 30 degrees off the nose

A

rolling takeoffs or standing takeoffs are permitted.

For standing takeoff N1 can not exceed 75% before brake release.

85
Q

In the crj900 for winds above 30kts that are more than 30 degrees off the nose

A

standing takeoffs are prohibited.

86
Q

Standing takeoffs are required when

A

necessary for performance or below 1200rvr.

87
Q

The minimum RVR for the first officer to conduct a takeoff is

A

1200.

88
Q

Max time with only DC power on ground

A

5 minutes

89
Q

What happens at 500’ on an AIII approach

A

Approach warn becomes active

90
Q

After ________ AIII mode will not arm

A

800’

91
Q 
Standard approach maneuvering speeds for flaps,
0
1(900)
8
20-45
A

200
190
180
Ref+10

92
Q

For Lnav or Lnav/Vnav approaches in a 900ng you must select _______

A

Baro in the arrival data page

93
Q

Minima for a circling approach is

A

1000’ and 1sm above the min vis for the approach being flown

If the plated minima is above 1000’ and 3sm then increase the required vis by 1sm

Calculated vis should not exceed 3sm

94
Q

Stabilized approach factors are

A 
Configured for landing
Ref +10, -5kias
<1000fpm (should)
<1200fpm (shall)
No turns to final below 500agl (except for sidestep)
95
Q

After starting the APU you must wait _______ before bleed air extraction.

A

2 minutes

96
Q

When initiating an emergency landing the captain shall notify the flight attendants by,

A

Calling “incharge to the interphone, incharge to the interphone”

97
Q

The interrupted start procedure is

A

Affected thrust lever - shutoff
Ignition off (200)
Dry motor until crank limit or below ITT 120C
Press eng stop switch

98
Q

In the event of a double flameout you of shall target and airspeed of

A

240kias to avoid core lock

Try to maintain at least 4% N1

99
Q

In the 900ng before each flight, what must be done with the IRS?

A

It must undergo a rapid realignment by selecting off (no more than 5 seconds) then nav.

+4)+"@## (19 decks)

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