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CRJ 200-700-900 > CRJ 200 Limitations > Flashcards

CRJ 200 Limitations Flashcards

1
Q

Max Ramp Wt ________lbs.

A

53,250

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2
Q

Max T/O Wt ________lbs.

A

53,000

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3
Q

Max Lnd Wt______lbs.

A

47,000

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4
Q

Max Zero Fuel Wt _______lbs.

A

44,000

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5
Q

Min Flight Wt _______lbs.

A

30,000

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6
Q

Wing Span

A

69ft 8in

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7
Q

Aircraft Length

A

87ft 10in

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8
Q

Tail Height

A

20ft 8in

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9
Q

Max Ops Alt_______ft.

A

37,000(SW)

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10
Q

Max T/O & Lnd Altitude_______ft.

A

10,000

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11
Q

Max Temp T/O & Lnd_______°C

A

ISA+35

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12
Q

Min Temp T/O_______°C

A

-40

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13
Q

Max Tailwind T/O & Lnd____kts.

A

10

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13
Q

Max Tailwind T/O & Lnd____kts.
10

A
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14
Q

Crosswind Limitation: Takeoff or Landing

A

27kt (SW)

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15
Q

Crosswind Limitation: Takeoff or Landing with RCC 1 or 2 or Poor BA, >1/8” Standing Water, > 1/8” Slush, Ice

A

10kt (SW)

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16
Q

Crosswind Limitation: Takeoff or Landing with Wet ice, Slush over Ice, Water over Compact Snow, Dry Snow over Ice, Wet Snow over Ice

A

Prohibited

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17
Q

VMO_____KIAS

A

335

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18
Q

MMO_______M

A

0.85

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19
Q

VLO EXT______KIAS(SW)

A

220

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20
Q

VLO RET______KIAS

A

200

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21
Q

VLE_____KIAS

A

220

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22
Q

VTire______kts.(GS)

A

182

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23
Q

VTire______kts.(GS)

A

182

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24
Q

V ADG DEPLOY MAX (Wet)______KIAS

A

250

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25
Q

V ADG DEPLOY MAX (Dry)

A

VMO/MMO

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26
Q

VB______KIAS

A

280

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27
Q

MB______M

A

0.75

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28
Q

V WIPER OPS Max______KIAS

A

220

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29
Q

VFO 8____KIAS

A

200

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30
Q

VFO 20____KIAS

A

200

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31
Q

VFE 8 ____KIAS

A

215

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32
Q

VFE 20 ____KIAS

A

215

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33
Q

VFE 30____KIAS

A

185

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34
Q

VFE 45____KIAS

A

170

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35
Q

Max Flaps Alt______ft.

A

15,000

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36
Q

Use of flaps is_______ for enroute ops.

A

prohibited

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37
Q

Min spoiler speed

A

Appr. speed + 20
(Appr. speed is current flaps maneuvering or straight-in speed)

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38
Q

Min Alt. Spoilers

A

1,000 ft. HAT(SW)

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39
Q

Spoilers use with flaps at____ prohibited

A

45°

40
Q

Minimum Runway Width____ft.

A

100

41
Q

Minimum Taxiway Width____ft.

A

35 (SW)

42
Q

STANDING WATER Takeoff/Landing

A

0.50 in./0.75 in.

43
Q

SLUSH Takeoff/Landing

A

0.50 in./ 0.88 in.

44
Q

WET SNOW Takeoff/Landing

A

1.00 in./1.50 in

45
Q

DRY SNOW Takeoff/Landing

A

3.00 in./3.75 in.

46
Q

When operating on runways contaminated with ice, dispatch with one thrust reverser is_____.

A

prohibited

47
Q

The taxi lights must be switched OFF whenever______.

A

the airplane is stationary in excess of 10 minutes

48
Q

FMS - The temperature compensation function should not be used at any time. It should be selected______.

A

OFF

49
Q

FMS - The temperature compensation function should not be used at any time. It should be selected______.

A

OFF

50
Q

Operations are prohibited on routes where ozone concentrations exceed limits in __________________________________.

A

Quick Reference Handbook (QRH) Volume 1

51
Q

APU Min Temp Start______°C

A

-40

52
Q

APU Max Ops Alt_______ft.

A

37,000

53
Q

APU Max Start Alt_______ft.

A

30,000

54
Q

APU Max Alt Bleed use_______ft.

A

15,000

55
Q

APU Max Alt Eng Start_______ft.

A

13,000

56
Q

Max Door Open with APU not operating_____KIAS

A

300

57
Q

APU Starter Duty Cycle

A
58
Q

Autopilot must be engaged above_______ unless otherwise permitted by the MEL.

A

FL200

59
Q

IAS MODE is ______ during approach

A

prohibited

60
Q

DES MODE (F/D or A/P coupled) is ______ during approach

A

prohibited

61
Q

APPR MODE is _____ for ___ approaches

A

prohibited
VOR

62
Q

ADC SOURCE coupled to active autopilot must be _______ to ATC transponder during flight in RVSM airspace.

A

the same as that coupled

63
Q

AUTOMATIC FC SYSTEM(AFCS)

A
64
Q

Ground Ops DC ONLY

A

5 min

65
Q

Max continuous DC TRU

A

100 A

66
Q

APU generator (maximum load)

A

to FL370-30kVA

67
Q

CARGO FIREX-Flight time to suitable airport

A

45 min

68
Q

Total - Pressure Refueling______lbs.

A

14,518

69
Q

Total - Gravity Refueling_______lbs.

A

13,906

70
Q

Max Imbalance for T/O____lbs.

A

800

71
Q

Min for GA per wing______lbs.

A

500
(Assumes a maximum airplane climb attitude of 10° nose up)

72
Q

Min Bulk Fuel Temp for T/O______°C

A

-30

73
Q

Min Bulk Fuel Temp in flight______°C

A

-40

74
Q

Takeoff with fuel in excess of ____ lbs. in the center tank is not permitted unless: Each main wing tank is above ______lb., or :Each main wing tank is above ______lb., and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lb., and the allowable center of gravity (CG) in this configuration is verified to be within allowable CG envelope.

A

500
4,400
2,000

75
Q

Powered crossflow and gravity crossflow must be ___ for takeoff.

A

off

76
Q

Powered crossflow and gravity crossflow must be ___ for takeoff.

A

off

77
Q

When fuel other than Jet-A is to be used, consult _______________ for limitations.

A

QRH Volume 1

78
Q

Min Reduced Thrust 3A1:____%

A

85

79
Q

Min Reduced Thrust 3B1:____%

A

83.5

80
Q

Automatic Performance Reserve (APR) must be used when takeoff performance is predicated upon use of ______.

A

APR

81
Q

The APR system must be selected ___ when an APR INOP caution message is displayed on EICAS.

A

off

82
Q

APR OFF Performance must be used when an ________ caution message is displayed.

A

APR INOP

83
Q

The APR system must be selected OFF for takeoff and APR OFF performance must be used when the ambient temperature is _____ and below, and pressure altitude is less than ______ft. (3A1 engines only)

A

-18°C
1000

84
Q

Engine Start(Ground)

A
85
Q

Dry Motoring(Ground)

A
86
Q

Max wind milling/starter-assisted cross-bleed relight altitude:______

A

FL210

87
Q

Until oil pressure reaches green band:______

A

Do not exceed idle

88
Q

Do not exceed 75% N1 until:______or_________,whichever is longer.

A

2 minutes, all operating indications in green band

89
Q

Ground idle N2 split:_______

A

≤2%

90
Q

During 2nd engine APU bleed start:_____

A

Operating engine ≤70%N2

91
Q

With OAT ≥-20°C, thrust levers at idle,N2:_______

A

> 57%. If N2 is ≤57% with OAT of -20°C or greater, do not advance thrust levers above idle. Contact Maintenance.

92
Q

Engines must not be shutdown until:______

A

2 minutes at idle/near idle thrust. Note- Taxi time counts towards this limitation.

93
Q

SkyWest prohibits the use of thrust reversers__________

A

during taxi operations

94
Q

Max OIL PRESSURE after cold start:_______

A

Engine must remain at idle until oil psi returns to normal range. Must be in normal range within 10 min.

95
Q

Single Pack Ops to FL______

A

250

96
Q

Max Ramp Wt ________lbs.

A

53,250

97
Q

Max T/O Wt ________lbs.

A

53,000

CRJ 200-700-900 (19 decks)

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