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Limitations & ER Procedures > Limitations & Emergency Procedures > Flashcards

Limitations & Emergency Procedures Flashcards

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1
Q

CR2 memory items for Double Engine failure

A

Ignition, CONT - ON

Airspeed - Not less than 240 kts

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2
Q

When should you use continuous ignition?

A 
TO & LNDs on contaminated runway
Crosswind >10kts CRJ200
Mod or greater Turbulence
Mod or greater Rain
Vicinity of thunderstorm
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3
Q

With OAT <=-20C, thrust lever at idle N2 should be _______

A

> 57%

If N2 is <=57% with OAT -20C or greater do not advance thrust lever above idle Contact Maintenance

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4
Q

Spoiler usage with _______ are __________ .

A

Flaps 45

Prohibited

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5
Q

CR7/9 memory items for Double Engine Failure?

A

Igntion, CONT - ON
If engines continue to run-down (N2<40%)
Thrust Levers (Both) - SHUT OFF
ADG Manual Deploy Handle - PULL

When ADG power is established:
Stab Trim, CH2 - CONFIRM ENGAGED
Target airspeed - Establish
    Above F340  - 0.7 MACH
    Below F340  - 240 kts
Maintain airspeed until ready to restart engines
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6
Q

CR7 Vfe 45

A

170

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7
Q

CR2 Engine start times

A

60 seconds ON / 10 seconds OFF
60 seconds ON / 10 seconds OFF
60 seconds ON / 5 minutes OFF
60 seconds ON / 5 minutes OFF

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8
Q

CR7 Max ramp weight

A

75,250

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9
Q

CR7/9 Max continuous DC TRU

A

120 A

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10
Q

CR2 Mmo

A

0.85

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11
Q

Ground Idle N2 split

A

2%

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12
Q

CR9 Vmo

A

335

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13
Q

CR2 APU Max Ops Alt

A

37,000ft

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14
Q

CR9 APU Max Alt Eng Start

A

21,000ft

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15
Q

CR7 Pressure refueling / gravity

A

19,594 / 14,580

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16
Q

CR9 Vlo RET

A

200

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17
Q

CR2 Max landing weight

A

47,000

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18
Q

CR7 Max door open with APU not operating

A

220 kts

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19
Q

What altitude the AFCS must be turn on by?

A

F200

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20
Q

CR9 Max Operating Altitude

A

37,000 ft (Skywest limit)

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21
Q

CR9 Mb

A

0.75

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22
Q

CR9 Vwiper ops max

A

250

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23
Q

CR9 Max zero fuel weight

A

70,750

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24
Q

CR2 Min fuel for GA per wing

A

450lb

Assumes max pitch up of 10 degrees

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25
Q

CR2 Vmo

A

335

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26
Q

When should taxi lights must be switched OFF when in a stationary period?

A

10 minutes

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27
Q

What is consider a contaminated runway?

A

More than 25% of runway has 1/8 inch of standing water, slush, wet or dry snow or slush

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28
Q

CR2 memory items for stabilizer trim runaway?

A

Control Wheel - Assume manual control and override runaway
Both Stab Trim Disc - Press, Hold, and Release
Airplane control - Transfer to Pilot (LH) side
Stab CH 1 and CH 2 HSTCU
Circuit breakers (2F5 and 4A1) - OPEN

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29
Q

CR7 APU Max Start Alt

A

37,000ft

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30
Q

CR7 APU Max Alt Eng Start

A

21,000ft

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31
Q

Crosswind Limitation. Takeoff or landing with wet ice, slush over ice, water over compacted snow, dry snow over ice, wet snow over ice

A

Prohibited

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32
Q

What is the min spoilers altitude?

A

1,000 ft HAT (SW)

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33
Q

CR2 Cargo FIREX time to suitable airport

A

45 min

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34
Q

CR7 Mb

A

0.75

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35
Q

CR2 Vadg deploy Max

A

250 (Wet)

Vmo/Mmo (Dry)

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36
Q

CR9 Vfe 45

A

170

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37
Q

Max Ground Ops with DC only

A

5 minutes

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38
Q

What it’s the CRJ200 memory items for No Light OFF?

A

Affected Thrust Lever - Shutoff
Ignition - OFF
Dry Motor - Until starter time limit
Affected Engine - STOP

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39
Q

CR2 Vfe 20

A

215

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40
Q

CR7/9 APU generator

A

To FL410

40kVA

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41
Q

CR2 Max door open with APU not operating

A

300 kts

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42
Q

CR2 Vfe 8

A

215

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43
Q

CR7/9 Max fuel imbalance for T/O

A

300lb

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44
Q

CR2 AFCS min altitude use TO / Non-precision / Precision

A

TO - 600ft
NP - 400ft
P - 80ft

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45
Q

CR7/9 memory items for stabilizer trim runaway?

A

Control Wheel - Assume manual control and override runaway

Stab trim disc - Select

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46
Q

CR7 Max zero fuel weight

A

62,300

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47
Q

CPAM PAX O2

A

14,000 +/-500ft

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48
Q

IAS Mode is _______ during approach

A

Prohibited

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49
Q

CR2 Maximum runway contaminant depth

A 
Takeoff / Landing
Standing water 0.5 / 0.75
Slush 0.50 / 0.88
Wet snow 1.00 / 1.50
Dry snow 3.00 / 3.75
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50
Q

CR2 APU Max Alt Eng Start

A

13,000ft

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51
Q

Crosswind limitation CRJ700 Takeoff

A

28kt(SW)

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52
Q

DES Mode F/D or A/P coupled is ________

During approach

A

Prohibited

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53
Q

CR2 Max T/O and Landing Altitude

A

10,000ft (Skywest limit)

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54
Q

Crosswind Limitation CRJ900 landing

A

32kts (SW)

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55
Q

CR2 Vwiper Ops Max

A

220

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56
Q

Until oil pressure reaches the green band. _______. Do not exceed 75% N1 until ______ or ________, whichever is longer.

A

Do not exceed idle

2 minutes OR
All Indications in the green

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57
Q

CR2 Max Temperature for T/O and Landing

A

ISA + 35C

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58
Q

CR2 Pressure refueling / gravity

A

14,518 / 13,906

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59
Q

CR2 APU Max Start Alt

A

30,000ft

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60
Q

CR7 Vadg deploy max

A

Vmo/Mmo

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61
Q

Crowing limitation. CRJ200 takeoff or landing

A

27kt (SW)

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62
Q

What is approached speed considered?

A

Approach speeds is current flaps

Maneuvering or straight-in

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63
Q

CR7 Vfe 30

A

185

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64
Q

EMERGENCY DEPRESS switch ______ is prohibited

A

Above 15,000ft

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65
Q

CR9 Vadg deploy max

A

Vmo/Mmo

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66
Q

CR2 Max fuel imbalance for T/O

A

800 lb

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67
Q

CR9 Vb

A

280

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68
Q

CR9 AFCS Min altitude use TO / Non-precision / Precision

A

TO - 600ft
NP - 400ft
P - Glide <=3.5 degrees - 80ft
P - Single engine - 110ft Airport Elevation >4,000ft Prohibited
Single engine Cat 2 - DH set to published DH or 110ft whichever is
Higher

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69
Q

CR9 Total pressure refueling / gravity

A

19,594 / 14,810

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70
Q

CR7/9 Operation in windy conditions.

> 30 either direction of nose & >30 knots wind speed

A

Apply Max of idle/taxi thrust before brakes released, then TOGA thrust. RLNG Takeoff procedure

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71
Q

CR2 Vfo 20

A

200

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72
Q

CR7/9 Limit climb to less than _______ above ______.

A

1,500 FPM

above F300

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73
Q

CR2 Vfe 45

A

170

74
Q

CR7 Max T/O weight DL/AS

A

74,999

75
Q

CR2 Max ramp weight

A

53,250

76
Q

CR9 Vfe 8

A

230

77
Q

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

A

Prohibited

78
Q

CR2 Dry Motor limits

A

90 seconds ON - 5 minutes OFF

30 seconds ON - 5 minutes OFF

79
Q

Powered cross flow and gravity cross flow must be _________ for takeoff

A

Off

80
Q

CR7 Max Operating Altitude

A

37,000 ft (Skywest limit)

81
Q

Max Flaps operating

A

15,000

82
Q

CR2 Automatic performance reserve must be used when takeoff performance is predicated upon use of

A

APR

83
Q

CR2 APU Starter Duty Cycle

A

Start 1 - 30 seconds - 2 minute delay
Start 2 - 30 seconds - 20 minutes off
Start 3 - 30 seconds - 2 minute delay
Start 4 - 30 seconds - 40 minutes off

84
Q

CR2 Max zero fuel weight

A

44,000

85
Q

CR2 Min spoiler speed

A

Appr speed + 20

86
Q

CR7 Max Temperature for T/O and Landing

A

ISA + 35C

ISA + 40C (AE)

87
Q

CR2 APU Max Alt Bleed Use

A

15,000ft

88
Q

APPR mode is ______ for ______ approaches

A

Prohibited

VOR approaches

89
Q

CR7 Vtire

A

182 (GS)

90
Q

CR7/9 Min fuel for GA per wing

A

600 lb

91
Q

CR9 APU Max Alt Bleed Use

A

25,000ft

92
Q

CR7 Mmo

A

0.85 (0.83 RVSM)

93
Q

CR7/9 Operation in windy conditions.

> 30 either direction of nose & 5 to 30 knots wind speed

A

Apply Max of 75% N1 before brakes released, then TOGA thrust

NML Takeoff procedure

94
Q

During 2nd engine start with the APU the operating engine _____

A

<70%

95
Q

Where can you find the maximum crosswind performance for takeoff, landing and contamination criteria? Is this data considered a pilot limitation?

A

See Company manuals > Weather section

Yes, All crosswind data provided is considered a pilot limitation

96
Q

CR9 Vle

A

220

97
Q

CR2 Min Temperature for T/O

A

-40C

98
Q

CR7/9 Single Pack Ops Alt limit

A

F310

99
Q

CR7 Vmo

A

335

100
Q

CRJ200 Wing Span

A

69ft 8in

101
Q

CR9 Mmo

A

0.84 (0.82 RVSM)

102
Q

CR7/9 Cargo FIREX time to suitable airport

A

60 min

103
Q

Min reduced thrust

A

3A1 - 85%

3B1 - 83.5%

104
Q

CR7 Max landing weight

A

67,000

105
Q

CR2 When fuel over than Jet A is to be used, consult ______ for limitations.

A

QRH Vol 1

106
Q

What is the CRJ200 memory items for hot start, interrupted start, N2 stagnation?

A

Affected thrust lever - Shutoff
Ignition - OFF
Dry motor - Until ITT less than 120C respecting starter time limits
Affected Engine - STOP

107
Q

CR9 Vfe 20

A

220 **

108
Q

Oil pressure should be in the normal range after cold start within

A

10 minutes

109
Q

CR7 Vfe 20

A

230

110
Q

CR7/9 Engine start times

A 
90 seconds ON / 10 seconds OFF
90 seconds ON / 10 seconds OFF
90 seconds ON / 5 minutes OFF
90 seconds ON / 5 minutes OFF
90 seconds ON / 5 minutes OFF
111
Q

CR2 APU generator

A

To FL370

30kVA

112
Q

CR9 Min spoiler speed

A

APPR speed + 10

113
Q

Crosswind Limitation CRJ700 landing

A

30kts (SW)

114
Q

CR9 APU Max Ops Alt

A

39,000ft (SW)

115
Q

CRJ200 Aircraft Length

A

87ft 10in

116
Q

CR9 APU Max Start Alt

A

37,000ft (SW)

117
Q

CR9 Max T/O weight

A

84,500

118
Q

CR2 Mb

A

0.75

119
Q

CR2 Single pack Ops Alt limit

A

F250

120
Q

CR2 Min flight weight

A

30,000

121
Q

CR2/7/9 Max Tailwind for TO & LND

A

10 kts

122
Q

CR9 Max door open with APU not operating

A

220 kts

123
Q

CR9 Vfe 30

A

185

124
Q

CR9 Max Temperature for T/O and Landing

A

ISA + 35C

125
Q

CR7 Max T/O weight

A

75,000

126
Q

CR2 Min reduced thrust for 3A1

A

85.0

127
Q

CR7 Min spoiler speed

A

APPR speed + 10

128
Q

CR7/9 Dry Motor limits

A 
90 seconds ON / 5 minutes OFF
30 seconds ON / 5 minutes OFF
30 seconds ON / 5 minutes OFF
30 seconds ON / 5 minutes OFF
30 seconds ON / 5 minutes OFF
129
Q

CR7 Vwiper Ops max

A

250

130
Q

CR2 Max continuous DC TRU

A

100 A

131
Q

CR2 Vfe 30

A

185

132
Q

CRJ memory items for excessive asymmetry or loss of braking during landing?

A

Wheel brakes - Release Momentarily
Anti-skid - OFF
Wheel brakes - Re-apply, as required

133
Q

CR7 Min flight weight

A

42,000

134
Q

CR2 Vle

A

220

135
Q

CR7 APU Max Ops Alt

A

39,000ft (SW)

136
Q

CR2 APU Min start temperature

A

-40C

137
Q

CR9 Min flight weight

A

45,000

138
Q

CR2 Vlo RET

A

200

139
Q

When must the APR system be selected off?

A

When APR caution message exists

When temp is -18C and below and pressure altitude less than 1,000 (3A1 engines only)

140
Q

Min bulk fuel temp for T/O and in flight

A

T/O: -30C

In flight: -40C

141
Q

CR2 Vtire

A

182 (GS)

142
Q

CR7 Vfe 8

A

230

143
Q

CR2 Vb

A

280

144
Q

CR2 Vfo 8

A

200

145
Q

CR7 Vlo RET

A

200

146
Q

Enroute slats / flaps / spoilers are ____________ .

A

Prohibited

147
Q

CR9 Max landing weight

A

75,100

148
Q

Engine Cool down

A

2 minutes near idle thrust

149
Q

CR9 Min Temperature for T/O

A

-40C

150
Q

ADC source coupled to active autopilot must be ______ to the ATC transponders during flight in RVSM airspace.

A

The same as coupled

151
Q

CR9 Vtire

A

195 (GS)

152
Q

Operations are prohibited on routes with ozone concentrations exceed limits in

A

QRH vol 1

153
Q

Crosswind Limitation. Takeoff or landing with RCC 1 or 2 or Poor BA with >1/8in standing water, slush, ice

A

10kt SW

154
Q

Min runway width

A

100ft

155
Q

CR7 APU Min start temp

A

-40C

156
Q

CR7/9 Maximum runway contaminant depth

A 
Takeoff / Landing
Standing water 0.5 / 0.75
Slush 0.59 / 0.88
Wet snow 0.59 / 0.88
Dry snow 3.00 / 3.75
157
Q

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

A

Prohibited

158
Q

When is flex not allowed

A 
W-Windshear warnings reported or forecasted
W-Wing or Cowl A/I ON
A-Anti-skid INOP
T-Tailwind > 5 kts
C-Contaminated Runway
H-Heavy takeoff behind 
Flaps 8 TO CRJ200
159
Q

CR9 APU Min start temp

A

-40C

160
Q

CR7/9 Operation in windy conditions.

30 either direction from nose & No wind speed limit
OR
>30 either direction from nose & <5kts wind speed

A

No limitations

TOGA thrust may be applied before brakes released

161
Q

CR7 Vlo EXT

A

220 (220)

162
Q

CR9 Max T/O and Landing Altitude

A

9,600 (Skywest limit)

163
Q

CR9 Max ramp weight

A

85,000

164
Q

CR7 Vle

A

220

165
Q

CRJ200 Tail height

A

20ft 8in

166
Q

Crosswind limitations CRJ900 Takeoff

A

35kts (SW)

167
Q

CR2 Max Operating Altitude

A

37,000 ft (Skywest limit)

168
Q

CR2 Max windmilling starter assisted cross bleed relight altitude ?

A

F210

169
Q

CR7 Vb

A

280

170
Q

CR7 AFCS Min altitude use TO / Non-precision / Precision

A 
TO - 600ft
NP - 400ft
P - Glide <=3.5 degrees - 80ft
P - Glide >3.5 to <=4.0 - 120ft   Airport Elevation >4000ft Prohibited
P - Glide >4.0 - Prohibited
171
Q

CR7 APU Max Alt Bleed Use

A

25,000ft

172
Q

CR7 Max T/O and Landing Altitude

A

9,600 (Skywest limit)

173
Q

CR2 Max T/O weight

A

53,000

174
Q

CR9 Vlo EXT

A

220 (SW)

175
Q

Takeoff with fuel > 500 in center tank is prohibited unless the main tank is above _______ or _________

A

4,400 OR
2,000 and allowable saw is reduced by weight of fuel in center tank in excess of AND
CG is within limits

176
Q

CE7/9 APU Starter Duty Cycle

A

No more than three starts/start attempts in 1 hour

A two minute delay must be observed between cranking attempts

177
Q

What is the CR7/9 memory items for Start abort message, Hot start?

A

Affected thrust lever - Shutoff
Dry Motor - Untill ITT deuces below 120C, respecting starter time limit
Affected Engine - Stop

178
Q

CR7 Min Temperature for T/O

A

-40C

179
Q

CR2 Min reduced thrust for 3B1

A

83.5

180
Q

CR2 Vlo EXT

A

220 (SW)

Limitations & ER Procedures (1 decks)

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