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CRJ 200 > CRJ 200 Limitations > Flashcards

CRJ 200 Limitations Flashcards

0
Q

Max T/O weight

A

53,000 lbs

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1
Q

Max ramp weight

A

53,250 lbs

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2
Q

Max landing weight

A

47,000 lbs

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3
Q

Max zero fuel weight

A

44,000 lbs

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4
Q

Max aft cargo

A

3,500 lbs

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5
Q

Max operating alt (SkyWest)

A

37,000’

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6
Q

Max T/O and landing alt

A

10,000’

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7
Q

Max temp T/O and land

A

ISA + 35C

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8
Q

Minimum temp T/O

A

-40C

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9
Q

Max runway slope

A

+/-2%

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10
Q

Max tailwind

A

10 kts

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11
Q

Vmo

A

335 KIAS

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12
Q

Mmo

A

0.85 M

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13
Q

Vfo8

A

200 KIAS

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14
Q

Vfo20

A

200 KIAS

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15
Q

Vfe8

A

215 KIAS

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16
Q

Vfe20

A

215 KIAS

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17
Q

Vfe30

A

185 KIAS

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18
Q

Vfe45

A

170 KIAS

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19
Q

Vlo ext

A

220 KIAS

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20
Q

Vlo RET

A

200 KIAS

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21
Q

Vle

A

220 KIAS

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22
Q

Vtire

A

182 kts GS

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23
Q

Vadg deploy max

A

250 KIAS

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24
Q

Vb

A

280 KIAS

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25
Q

Mb

A

.75 M

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26
Q

Vwiper ops max

A

220 KIAS

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27
Q

Anti-skid

A

> 35 kts or WOW +5 sec

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28
Q

Anti-skid inop below

A

10 kts

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29
Q

Max alt slats/flaps

A

15,000’

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30
Q

Minimum spoiler speed

A

Approach speed +17

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31
Q

Minimum alt spoilers

A

300’ AGL

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32
Q

Min reduced thrust

A

3B1: 83.5%
3A1: 85%

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33
Q

N2 Start

A

20% (green)

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34
Q

N2 idle

A

56.5-68% (green)

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35
Q

Engine start (ground)

A

60 sec on/10 sec off
60 sec on/10 sec off
60 sec on/5 min off
60 sec on/5 min off

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36
Q

At initiation of thrust lever movement from…

A

…shut off to idle, ITT must be 120C or less for all ground starts.

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37
Q

Dry motoring

A

90 sec on - 5 min off

30 sec on - 5 min off

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38
Q 
Usable fuel
L Main (pressure refueling)
A

4,760 lbs

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39
Q 
Usable fuel
R Main (pressure refueling)
A

4,760 lbs

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40
Q

Usable fuel

Center (pressure refueling)

A

4,998 lbs

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41
Q

Usable fuel

Total

A

14,518 lbs

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42
Q

Usable fuel

Max imbalance

A

800 lbs

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43
Q

Max fuel imbalance for T/O

A

800 lbs

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44
Q

Minimum fuel for GA per wing

A

450 pounds (amber)

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45
Q

Minimum fuel temp for T/O

A

+5C

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46
Q

Main Gen

A

To 35,000’: 30 KVA

> 35,000’: 25 KVA

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47
Q

APU Gen

A

To 37,000’: 30 KVA

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48
Q

Electric

Ground ops DC only

A

5 minutes

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49
Q

AFCS mode prohibited during approach

A

IAS mode

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50
Q

AFCS mode prohibited for VOR approaches

A

APPR mode

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51
Q

AFCS T/O minimum alt

A

600’ AGL

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52
Q

AFCS non-precision/visual approach minimum alt

A

400’ AGL

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53
Q

AFCS precision approach glide path angle/minimum alt

A

</=3.5, 80 AGL

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54
Q

Max press diff

A

8.7 psi

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55
Q

Max negative pressure diff

A

-0.5

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56
Q

Single pack ops to

A

FL250

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57
Q

Pack overheat

A

88C

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58
Q

Pack over pressure

A

> 53 psi

59
Q

APU max op alt

A

37,000’

60
Q

APU max start alt

A

30,000’

61
Q

APU max alt bleed use

A

15,000’

62
Q

APU max alt eng start

A

13,000’

63
Q

APU Start Aircraft Battery

A

2x30 seconds on - 20 minutes off

2x30 seconds on - 40 minutes off

64
Q

APU Start DC External

A

2x15 seconds on - 20 minutes off

2x15 seconds on - 40 minutes off

65
Q

Engine (blank) at ground idle power should not be greater than (blank) split

A

N2, 2%

66
Q

If (blank) is (blank) or less with an OAT of (blank), do not accelerate above (blank). This indicates a mechanical problem with the engine.

A

N2, 57%, -20C or warmer, idle

67
Q

After all (blank), do not exceed (blank) for (blank) after start, or until all operating indications are in normal range, whichever is longer.

A

Starts, 75% N1, two minutes

68
Q

Before the first flight of the day, when the airplane is (blank) at a temperature of (blank) for more than (blank) hours, the engines must be motored for (blank) seconds and fan rotation verified before engine start is initiated.

A

Cold soaked, -30C or below, 8 hours, 60 seconds

69
Q

During preflight checks of the thrust reversers after being cold soaked for more than (blank) hours, the (blank) must be actuated until the deploy and stow cycles are less than (blank) seconds.

A

8 hours, thrust reversers, 5 seconds

70
Q

Continuous ignition must be used… (5 conditions)

A 
Contaminated runways
Crosswind >10 kts (200 only)
Moderate or heavier rain
Moderate or heavier turbulence
Vicinity of thunderstorms
71
Q

During landing, allocation of (blank) is (blank) at airspeeds (blank) KIAS. Below (blank) KIAS, reverse thrust must be reduced to (blank). Not above (blank)

A

Reverse thrust, not permitted, below 75 KIAS, 60 KIAS, idle, 30% N1

72
Q

The engine oil level must be checked within (blank) to (blank) of every engine shutdown.

A

3 minutes to 2 hours

73
Q

If use of the oil replenishment system is required, then the engine(s) should be replenished within (blank) to (blank) after engine shutdown.

A

15 minutes to 2 hours

74
Q

Maximum refill allowable is (blank) quarts without dry motoring the engine

A

Two

75
Q

If both engines are to be started using the (blank), then the operating engine’s thrust must not exceed (blank)

A

APU bleed air, 70% N2

76
Q

(Blank) must be switched off any time the aircraft is stationary for more than (blank) minutes (SkyWest procedure)

A

All landing and taxi lights, 10 minutes

77
Q

(Blank) with a fuel load in excess of (blank) in the (blank) tank is not permitted unless each (blank) tank is above (blank)

A

Takeoff, 500 lbs, center, main, 4,400 lbs

78
Q

Takeoff with engine fuel temperature indications (blank) is (blank)

A

Below +5C, prohibited

79
Q

Bulk fuel takeoff limit

A

-30C

80
Q

Bulk fuel freezing point

A

-40C

81
Q

Tuning (blank) and (blank) from the FMS is (blank)

A

Transponder 1, transponder 2, prohibited

82
Q

Minimum climb speed: reference long range cruise/minimum speed/holding speed chart in the (blank)

A

Performance cards

83
Q

Maximum climb speed profile above (blank) - (blank)

A

10,000’, 290 KIAS to .70 M

84
Q

(Blank) will be the minimum (blank) speed once transition is made from IAS to MACH speed

A

.70 Mach, climb

85
Q

Maximum authorized altitude

A

FL370

86
Q

Reduced thrust takeoffs are prohibited when… (6 items)

A 
Cowl and/or wing anti-ice ON
Runway is contaminated
Tailwind in excess of 5 kts
Warnings of windshear/downdrafts
Anti-skid is inoperative
T/O behind heavy aircraft
87
Q

Reduced thrust takeoff on (blank) are (blank)

A

Wet runways, permitted

88
Q

The appropriate additions to (blank) using the laminated flight deck (blank) must be made if (blank) performance is not available.

A

V1 and Vr, flip cards, ACARS

89
Q

Conditions conducive to icing exist on the (blank) when the (blank) is (blank), when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes.

A

Ground and for takeoff, OAT, 10C or below

90
Q

Icing conditions exist in (blank) when the (blank) is (blank) and (blank) in any form is encountered (such as clouds, rain, snow, sleet, or ice crystals), except when the (blank) is (blank) or below.

A

Flight, TAT, 10C or below, visible moisture, SAT, -40C(-40F)

91
Q

The cowl anti-ice system must be on when the (blank) is (blank) and (blank) in any form (blank) (such as fog with visibility of one mile or less, rain, snow, sleet and ice crystals)

A

OAT, 10C or below, visible moisture, is present

92
Q

The cowl anti-ice system must also be on when the (blank) is (blank) when operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush is present.

A

OAT, 10C or below

93
Q

Turn (blank) anti-ice on for final taxi unless (blank) or (blank) anti-ice fluids have been applied.

A

Wing, Type II, Type IV

94
Q

The L or R WING A/ICE caution messages may be displayed during taxi but the WING/COWL A/I ON advisory message must be displayed (blank)

A

Prior to takeoff

95
Q

If APU is not operating, a (blank) caution message will be displayed. This is a normal indication for this configuration; however, the message must be extinguished prior to takeoff. During this condition, takeoff N1 values will not be displayed on EICAS.

A

Bleed misconfig

96
Q

The term “final taxi” has caused some confusion. Bombardier defines final taxi as that period following (blank) or about (blank) prior to takeoff.

A

2nd engine start, 2 minutes

97
Q 
T/O OAT 5C or colder 
Turn the (blank) anti-ice (blank) just prior to (blank)
A

Wing, off

98
Q

The wing anti-ice system must be on for T/O when

A

Visible moisture below 400’ AGL is reported

99
Q

Operate the anti-ice system during takeoff and take the associated weight penalty, only if the above actually exist (blank)

A

At the time of takeoff

100
Q

(Blank) - the (blank) anti-ice system must be ON:
A) when in (blank), or
B) when (blank) by the ice detection system

A

Cowl, engine cowl, icing conditions, ICE is annunciated

101
Q

(Blank) - the (blank) anti-ice system must be ON:
A) when (blank) by the ice detection system, or
B) when in (blank) and the airspeed is less than (blank)

A

Wing, wing, ICE is annunciated, icing conditions, 230 KIAS

102
Q

(Blank) takeoff on a contaminated runway is (blank) for the CRJ200/700/900

A

Flaps 8, authorized

103
Q

Usable Fuel L Main (Gravity Refueling)

A

4488 lbs

104
Q

Usable Fuel R Main (Gravity Refueling)

A

4488 lbs

105
Q

Usable Fuel Center (Gravity Refueling)

A

4930 lbs

106
Q

Usable Fuel Total (Gravity Refueling)

A

13,906 lbs

107
Q

APU Max RPM

A

107%

108
Q

APU Max Continuous EGT

A

743 C

109
Q

APU Max EGT Start

A

974 C

110
Q

APU Min Temp Start

A

-40 C

111
Q

APU Max Gen Load

A

30 KVA

112
Q

Max Speed Door Open with APU not operating

A

300 KIAS

113
Q

Engine ITT

Max APR not operating operating/normal T/O

A

First 2 min: 900 C

Next 3 min: 884 C

114
Q

Engine ITT

Max APR Operating

A

First 2 min: 928 C

Next 3 min: 900 C

115
Q

Engine ITT

Max Cont Thrust

A

3B1: 874 C (860 C 3A1)

116
Q

Engine ITT

Max Start

A

900 C

117
Q

Oil Temp

Min Start

A

-40 C

118
Q

Oil Temp

Max Cont

A

155 C

119
Q

Oil Temp

Max (15 Min)

A

163 C

120
Q

Oil Pressure

Min Start/Idle

A

25 psi

121
Q

Oil Pressure

Max T/O Thrust

A

45 psi

122
Q

Oil Pressure

Max Cont

A

115 psi

123
Q

Oil Pressure

Max after cold start

A

130 psi at idle for max of 10 min

Engine must remain at idle until oil psi returns to normal range

124
Q

Max oil consumption

A

.05 GPH (1 qt/5 hours)

125
Q

Engine thrust normal T/O

A

8729 lbs

126
Q

Engine thrust APR

A

9220 lbs

127
Q

Min Flight Weight

A

30,000 lbs

128
Q

CRJ 200: flight time to suitable airport

A

45 minutes

129
Q

Max Cont DC TRU

A

100 amps

130
Q

Max press diff taxi, T/O, landing

A

.1 psi

131
Q

No man ops (pressurization)

A

To -1500 ft

132
Q

Cabin alt caution

A

8,500’ to 10,000’

133
Q

Cabin alt warning

A

> 10,000’

134
Q

CPAM drops O2 masks

A

14,000 +/- 500’

135
Q

CPAM

No smoking/seatbelt signs on

A

10,000’

136
Q

Emergency depress maintains

A

14,250 +/- 750’

137
Q

Normal brake pressure

A

1000-3200 psi

138
Q

Nose steering

A

Rudder: 5 degrees L/R
Tiller: 70 degrees L/R

139
Q

Minimum runway width

A

100’

140
Q

Hydraulics

Norm psi

A

2950-3050 psi

141
Q

Hydraulics

Low psi

A

<1800 psi

142
Q

Hydraulics

Pressure relief

A

> 3750 psi

143
Q

Hydraulics

Accumulator pressure

A

1500 psi

144
Q

Hydraulics

Norm level

A

45-85%

145
Q

Hydraulics

High temp caution

A

93-96 degrees C

CRJ 200 (2 decks)

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