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2014 AQP Study Guide > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight CRJ 200

A

53,250 lbs

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2
Q

Max Ramp Weight CRJ 700

A

75,250 lbs

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3
Q

Max Ramp Weight CRJ 900

A

85,000 lbs

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4
Q

Max Take Off Weight CRJ 200

A

53,000 lbs

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5
Q

Max Take Off Weight CRJ 700

A

75,000 lbs

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6
Q

Max Take Off Weight CRJ 900

A

84,500 lbs

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7
Q

Max Take Off Weight for Delta / Alaska 700’s

A

74,999 lbs

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8
Q

Max Landing Weight CRJ 200

A

47,000 lbs

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9
Q

Max Landing Weight CRJ 700

A

67,000 lbs

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10
Q

Max Landing Weight CRJ 900

A

75,100 lbs

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11
Q

Max Zero Fuel Weight CRJ 200

A

44,000 lbs

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12
Q

Max Zero Fuel Weight CRJ 700

A

62,300

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13
Q

Max Zero Fuel Weight CRJ 900

A

70,750 lbs

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14
Q

Max Aft Cargo CRJ 200

A

3500 lbs

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15
Q

Max Aft Cargo CRJ 700

A

3740 lbs

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16
Q

Max Aft Cargo CRJ 900

A

3740 lbs

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17
Q

Max Aft Cargo WiFi Equipped CRJ 700 / 900’s

A

3650 lbs (90 lbs less)

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18
Q

Max Aft Cargo Alaska CRJ 700

A

4375 lbs

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19
Q

Max Fwd Cargo CRJ 700

A

1000 lbs

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20
Q

Max Fwd Cargo CRJ 900

A

1700 lb total 850/850 split bin

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21
Q

Max Flight Time to Suitable Airport CRJ 200

A

45 Minutes ( limitation based on cargo fire bottle time )

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22
Q

Max Flight Time to Suitable Airport CRJ 700 / 900

A

60 Minutes

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23
Q

Max Temp for Take Off and Land

A

ISA + 35C

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24
Q

Max Temp for Take Off and Land Phoenix

A

Approx 48 degs C or 118 degrees F

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25
Q

Max Temp for Take Off in Denver

A

Approx 40 degrees C or 104 degrees F

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26
Q

Vmo all variants

A

335 Kts

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27
Q

Mmo CRJ 200

A

.85 Mach

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28
Q

Mmo CRJ 700

A

.85 Mach

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29
Q

Mmo CRJ 700 in RVSM

A

.83 Mach in RVSM

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30
Q

Mmo CRJ 900

A

.84 Mach

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31
Q

Mmo CRJ 900 in RVSM

A

.82 Mach RVSM

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32
Q

Vtire CRJ 200

A

182 Kts GS

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33
Q

Vtire CRJ 700

A

182 Kts GS

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34
Q

Vtire CRJ 900

A

195 Kts GS

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35
Q

Vwiper max CRJ 200

A

220 KIAS

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36
Q

Vwiper max CRJ 700 / 900

A

250 KIAS

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37
Q

Hydraulic Normal psi CRJ 200

A

2950 - 3050 psi

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38
Q

Hydraulic Low psi CRJ 200 / 700 / 900

A

< 1800 psi (amber)

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39
Q

Hydraulic High psi CRJ 200

A

> 3200 psi (white)

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40
Q

Hydraulic Pressure Relief CRJ 200

A

> 3750 psi (white)

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41
Q

Hydraulic Accumulator Pressure CRJ 200

A

1500 psi

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42
Q

Hydraulic Normal Level CRJ 200

A

45 - 85 % (green)

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43
Q

Hydraulic High Temp Caution CRJ 200

A

93 - 96 degrees C

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44
Q

Hydraulic Normal psi CRJ 700 / 900

A

3000 psi

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45
Q

Hydraulic Temp Caution CRJ 700 / 900

A

94 - 96 degrees C

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46
Q

Normal Brake Pressure CRJ 200

A

1000 - 3200 psi (green)

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47
Q

Normal Brake Pressure CRJ 700 / 900

A

1800 - 3200 psi (green)

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48
Q

Anti Skid available

A

Wheel Speed > 35 KTS, WOW for +5 Sec

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49
Q

Anti Skid inop below what speed

A

10 KTS

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50
Q

Min Spoiler Speed CRJ 200

A

Approach Speed + 17 KTS

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51
Q

Min Spoiler Speed CRJ 700 / 900

A

Approach Speed + 10 KTS

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52
Q

Min Alt for Spoilers

A

300’ AGL

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53
Q

Max ITT for Engine Start CRJ 200

A

900 Degrees C

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54
Q

Max ITT for Engine Start CRJ 700 / 900

A

815 degrees C

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55
Q

Max Continuous Thrust CRJ 200

A

3A1 : 860 degrees C

3B1 : 874 degrees C

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56
Q

Max ITT APR not operating / Normal T/O CRJ 200

A

928 degrees C for the first 2 minutes

884 degrees C for the next 3 minutes

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57
Q

Max ITT APR not operating / Normal T/O CRJ 700

A

920 degrees C for 5 minutes

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58
Q

Max ITT APR not operating / Normal T/O CRJ 900

A

947 degrees C for 5 minutes

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59
Q

Max ITT APR operating CRJ 900

A

990 degrees C for 5 minutes ( + 43 degrees C )

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60
Q

Max ITT APR operating CRJ 700

A

960 degrees C for 5 minutes

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61
Q

Max ITT APR operating CRJ 200

A

928 degrees C for first 2 minutes

900 degrees C for next 3 minutes

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62
Q

Min Oil Temp for Start all 3 variants

A
  • 40 degrees C
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63
Q

Max Continuous Oil Temp all 3 variants

A

155 degrees C

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64
Q

Max Oil Temp allowed for 15 minutes

A

163 degrees C

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65
Q

Min Oil Pressure for Start / Idle CRJ 200

A

25 psi ( red )

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66
Q

Min Oil Pressure for Start / Idle CRJ 700 / 900

A

25 to 60 psi ( green )

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67
Q

Min Oil Pressure for Take Off CRJ 200

A

45 psi ( green )

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68
Q

Min Oil Pressure for Take Off CRJ 700 / 900

A

45 - 95 psi ( green )

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69
Q

Max Continuous Oil Pressure CRJ 200

A

115 psi ( green )

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70
Q

Max Continuous Oil Pressure CRJ 700 / 900

A

45 - 95 psi ( green )

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71
Q

Max Oil Pressure after Cold Start CRJ 200

A 
156 psi  ( amber ) 
130 psi at idle for max of 10 minutes
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72
Q

Max Oil Pressure after Cold Start CRJ 700 / 900

A 
182 psi  ( amber )
116 psi max after 10 minutes  ( 95 psi for CRJ 900 )
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73
Q

Max Oil Consumption

A

.05 GPH or 1 Qt for every 5 hours

74
Q

What Engines are on the CRJ 200 and how much thrust do they produce

A

CF 34 - 3B1

Take Off Thrust 8729 lbs

75
Q

What Engines are on the CRJ 700 and how much thrust do they produce

A

CF 34 - 8C1

Take Off Thrust 12,670 lbs

76
Q

What Engines are on the CRJ 900 and how much thrust do they produce

A

CF 34 - 8C5

Take Off Thrust 13,535 lbs

77
Q

Engine Start Limitations CRJ 200

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

78
Q

Engine Start Limitations

A 
90 Sec On - 10 Sec Off
90 Sec On - 10 Sec Off
90 Sec On - 5 Min Off
90 Sec On - 5 Min Off
90 Sec On - 5 Min Off
79
Q

Dry Motoring Limitations CRJ 200

A

90 Sec ON - 5 Min OFF

30 Sec ON - 5 Min OFF

80
Q

Dry Motoring CRJ 700 / 900

A 
90 Sec ON - 5 Min OFF
30 Sec ON - 5 Min OFF
30 Sec ON - 5 Min OFF
30 Sec ON - 5 Min OFF
30 Sec ON - 5 Min OFF
81
Q

Left / Right Main Tank Useable Fuel CRJ 200
( Pressure Refueling )
( Gravity Refueling )

A

4760 lbs with single point pressure refueling

4488 lbs with over wing / gravity refueling

82
Q

Left / Right Main Tank Useable Fuel CRJ 700 900
( Pressure Refueling )
( Gravity Refueling )

A

7492 lbs with single point pressure refueling

7290 lbs with over wing / gravity refueling

83
Q

Center Tank Useable Fuel CRJ 200
( Pressure Refueling )
( Gravity Refueling )

A

4998 lbs with single point pressure refueling

4930 lbs with over wing / gravity refueling

84
Q

Center Tank Useable Fuel CRJ 700 / 900
( Pressure Refueling )
( Gravity Refueling )

A

4610 lbs Pressure Refueling

N/A

85
Q

What is the difference between total useable on the CRJ 700 and the CRJ 900?

A

They have the same useable fuel quantities.

86
Q

What is the Total Useable Fuel of the CRJ 200
( Pressure Refueling )
( Gravity Refueling )

A

14,518 lbs with single point pressure refueling

13,906 with over wing / gravity refueling

87
Q

What is the Total Useable Fuel of the CRJ 700 / 900
( Pressure Refueling )
( Gravity Refueling )

A

19,594 lbs with single point pressure refueling
14,580 lbs with over wing / gravity refueling CRJ 700
14,810 lbs with over wing / gravity refueling CRJ 900

88
Q

Max Fuel Imbalance all 3 variants

A

800 lbs

89
Q

Max Fuel Imbalance for Take Off CRJ 200

A

800 lbs

90
Q

Max Fuel Imbalance for Take Off CRJ 700 / 900

A

300 lbs

91
Q

Minimum Fuel for Go Around per Wing CRJ 200

A

450 lbs ( amber )

92
Q

Minimum Fuel for Go Around per Wing CRJ 700 / 900

A

600 lbs

93
Q

Min Fuel Temp for Take Off

A

+ 5 degrees C

94
Q

Nose Wheel Steering Limits on CRJ 200

A

Tiller 70 degrees L/R

Rudder 5 degrees L/R

95
Q

Nose Wheel Steering Limits on the CRJ 700 / 900

A

Tiller 80 degrees L/R

Rudder 8 degrees L/R

96
Q

Minimum Altitude for use of the AFCS ( Auto Pilot )

A

Take Off 600 ft AGL
Non Precision Approach 400 ft AGL
Precision Approach 80 ft AGL
(no more than 3.5 degree glideslope)

97
Q

General Altitude Restrictions for use of the AFCS

A

50 ft below the MDA or 400 ft AGL which ever is higher for for Non Precision Approaches
And 50 ft above the terrain for precision approaches

98
Q

Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope equal to or less than 3.5 degrees
4000 ft Field Elevation and below

A

Approved

Minimum Altitude for Use is 80 ft AGL

99
Q

Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater than 3.5 to 4.0 degrees
4000 ft Field Elevation and below

A

Approved

But the Minimum Altitude for Use is 120 ft AGL

100
Q

Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater 4.0 degrees
4000 ft Field Elevation and below

A

Prohibited

101
Q

Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater 4.0 degrees
Field Elevation Higher than 4000 ft

A

Prohibited

102
Q

Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater than 3.5 to 4.0 degrees
Field Elevation higher than 4000 ft

A

Prohibited

103
Q

What is the Max Precision Approach Glide Slope Limitation for the CRJ 700

A

Max of 3.5 degree glide slope for all airports
3.5 to 4.0 degree glide slope for airports up to 4000’ field elevation. ( Above 4000 feet field elevation is prohibited )
Above 4.0 degree glide slope is prohibited

104
Q

What is the Max Precision Approach Glide Slope Limitation for the CRJ 900

A

Max of 3.5 degree glide slope

If Single Engine there is an additional limitation of a max airport field elevation of 4000 feet.

105
Q

Max APU RPM CRJ 200

A

107% ( red )

106
Q

Max APU Continuous EGT

A

743 degrees C ( red )

107
Q

Max APU EGT Start

A

974 degrees C

108
Q

Max APU EGT on the ground for the CRJ 700 / 900

A

789 degrees C

109
Q

Max APU EGT in flight for the CRJ 700 / 900

A

807 degrees C ( red )

110
Q

Max APU EGT for the CRJ 700 / 900

A

1038 degrees C

111
Q

Min Temp for APU Start

A
  • 40 degrees C
112
Q

Max APU Ops Altitude for the CRJ 200

A

37,000 ft

113
Q

Max APU Start altitude for the CRJ 200

A

30,000 ft

114
Q

Max altitude for APU bleed use CRJ 200

A

15,000 ft

115
Q

Max altitude for APU use in engine start CRJ 200

A

13,000 ft

116
Q

Max Airspeed for the APU Door open when not operating CRJ 200

A

300 KIAS

117
Q

APU Start Limitations with AC Battery CRJ 200

A

2 x 30 Sec ON - 20 Min Off

2 x 30 Sec ON - 40 Min Off

118
Q

Max Altitude for Single Pack Ops CRJ 200

A

FL 250

119
Q

Pack Overheat Temp CRJ 200

A

88 degrees C

120
Q

Pack Overpressure CRJ 200

A

> 53 psi

121
Q

CPAM drops the Pax O2 at what cabin altitude

A

14,000 + / - 500 ft ( CRJ 200 )

Equal to or greater than 14,000 ft on the CRJ 700 / 900

122
Q

CPAM turns on the Passenger NO SMOKING FASTEN SEATBELT sign at what cabin altitude

A

10,000 ft

123
Q

On the CRJ 700 / 900 Use of the EMER DEPRESS switch is prohibited above what altitude

A

15,000 ft

124
Q

On the CRJ 700 / 900 Limit Climb to ____ fpm above what altitude

A

Limit Climb to 1500 fpm above FL300

125
Q

Do not accelerate above idle under what conditions

A

If N2 is 57% or less with an outside temp of -20 degrees C or warmer

126
Q

Do not exceed 75% N1 for…

A

2 minutes after start or until all engine indications are normal

127
Q

Definition of Cold Soaked

A

-30 degrees C or colder for more than 8 hrs.

128
Q

Max APU EGT on the Ground CRJ 700 / 900

A

789 degrees C

129
Q

Max APU EGT in flight CRJ 700 / 900

A

807 degrees C

130
Q

Max APU EGT CRJ 700 / 900

A

1038 degrees C ( red )

131
Q

Max APU Start Altitude CRJ 700 / 900

A

37,000 ft

132
Q

Max Altitude APU Bleed Use CRJ 700 / 900

A

25,000 ft

133
Q

Max Altitude APU for Engine Start CRJ 700 / 900

A

21,000 ft

134
Q

Max Airseed with APU not operating with the APU Door Open CRJ 700 / 900

A

220 KIAS

135
Q

APU Start Limits CRJ 700 / 900

A

Do not perform more than 3 starts in one hour…

A two minute delay must be observed between cranking attempts to allow for cooling and APU drainage.

136
Q

Max Altitude for Single Pack Ops CRJ 700

A

31,000 ft

137
Q

Max Altitude for Single Pack Ops CRJ 900

A

25,000 ft

138
Q

With an outside temp of _____ , what is the engine limitation that indicates a mechanical problem with the engine?

A

If the N2 is 57% or less with an OAT of -20 degrees C or warmer, do not accelerate the engines above idle as the mechanical problem.

139
Q

When the aircraft is cold soaked at a temp of ____ , what needs to happen on the FFOD?

A

When the aircraft is cold soaked at a temp of -30 degrees C for more than 8 hours, dry motor the engines and verify N1 fan rotation.

140
Q

When the aircraft is cold soaked at a temp of ____ , what needs to happen with the Thrust Reversers?

A

The Thrust Reversers must be actuated until the deploy and stow cycles are less than 5 seconds.
On the CRJ 700 / 900 the deploy cycle is 2 seconds and the stow cycle is an additional 2 seconds.

141
Q

CRJ 700 900 Takeoff Operating Procedure due to Wind

A

Within 30 degrees, no limitation

More than 30 degrees from 5 to 30 KTS:

142
Q

CRJ 700 900 Takeoff Operating Procedure due to Wind

Wind more than 30 degrees from 5 to 30 KTS

A

Apply Maximum of 75% N1 before brake Release, then TOGA thrust: NML TAKEOFF PROCEDURE

143
Q

CRJ 700 900 Takeoff Operating Procedure due to Wind

Wind more than 30 degrees and greater than 30 KTS

A

Apply Maximum of idle / taxi thrust before brake release, then TOGA thrust: RLNG TAKEOFF PROCEDURE

144
Q

When is Continuous Ignition to be used?

A
  1. Takeoffs and landings on contaminated runways
  2. Takeoffs with high crosswind components >10KT (200 only)
  3. Flight through Moderate or Heavier Rain
  4. Flight through Moderate or Heavier Turbulence
  5. Flight in the vicinity of thunderstorms
145
Q

What is the APR limitation for Takeoff with 3A1 Engines

A

The APR system must be selected off when the ambient temperature is -18 degrees C and below with pressure altitudes less than 1000 ft.

146
Q

What does the SOP say about checking engine oil?

A

It’s been deleted

147
Q

CRJ 200 APU Start Limits

A

Max of 60 seconds below 50% rpm

148
Q

When do you get the AVAL Light on the APU

A

When the RPM is 99% for 4 seconds

149
Q

Limitation for Take Off with fuel in the center tank

A

Takeoff with more than 500 lbs in the center tank is not permitted unless there is more than 4,400 lbs in each main tank.

150
Q

What is the exception to the center tank fuel limitation for takeoff

A

Each wing tank is above 2000 lbs and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lbs. and the CG is verified

151
Q

Take Off with Engine Fuel temp below _____ is prohibited

A

+5 degrees C

152
Q

What is the Bulk Fuel Temperature Limit for Take Off

A

-30 degrees C

153
Q

The Bulk Fuel Temperature must remain at or above ____ during flight

A

-40 degrees C

154
Q

Is Reduced Thrust allowed for Flaps 8 Take Off on the CRJ 200

A

NO

155
Q

When must a Cold Weather PreFlight Inspection be completed

A
  1. When the OAT is 5 degrees C or less
  2. When the wing fuel temp is 0 degrees C or less
  3. Icing conditions exist
  4. AC has been exposed to contaminants on an overnight
  5. On any through flight where the AC has residual ice form the inbound flight
  6. Cold Soaked Ice is suspected in the fuel tank area
156
Q

The aircraft wing surfaces must be checked for ice when what conditions exist?

A

Frost is detected below the wing tank area

or when the surface temperature is near freezing with high humidity ( temp / dewpoint spread 3 degrees C )

157
Q

Are Flaps 8 takeoffs authorized on contaminated runways?

A

Yes… for all 3 variants

158
Q

Max Standing Water Depth for Take Off CRJ 200

A

.50 inches

159
Q

Max Standing Water Depth for Take Off CRJ 700 / 900

A

.50 inches

160
Q

Max Wet Snow Depth for Take Off CRJ 200

A

1.0 inches

161
Q

Max Slush Depth for Take Off CRJ 200

A

.50 inches

162
Q

Max Dry Snow for Take Off

A

3.0 inches… all 3 varients

163
Q

When is it possible to have clear ice on the wings?

A

When the fuel temperature is 0 degrees C or below even if the OAT is above freezing.

164
Q

When might wing frost occur on the upper wing surface with the OAT above freezing?

A

When the fuel content exceeds 2297.2 lbs, it is in contact with the upper wing surface.

165
Q

At what temp must the Cowl Anti-Ice be selected ON while on the ground

A
  1. OAT is 10 degrees C and visible moisture is present
    Visibility 1 mile or less, fog, rain, snow etc.
  2. While on ramps or taxiways when there are contaminants present.
166
Q

OAT is 5 degrees and the visibility is 10 miles with a ceiling of 300 overcast… what anti-ice is required
CRJ 200?
CRJ 700 / 900?

A

Engine Cowl Anti-Ice selected on for Take Off for the CRJ 200
No anti-ice is required for the CRJ 700 / 900

167
Q

When is a runway considered to be wet?

A

When there is sufficient moisture on the runway to cause it to appear reflective with a water depth of less than 1/8” covering 100 % of the runway.

168
Q

If the runway has dry spots with no standing water, is it still considered to be wet?

A

NO

169
Q

When is a runway considered to be contaminated

A

When more than 25% of the runway surface within the required length and width to be used is covered by more than 1/8th inch of standing water or its equivalent in slush or wet snow or dry snow.

170
Q

If the runways expected to be used are contaminated with ice, what is the limitation?

A

Both Thrust Reversers must be operative prior to dispatch.

171
Q

Are Reduced Thrust Take Offs permitted on wet runways?

A

Yes

172
Q

Are Reduced Thrust Take Offs permitted with flaps 8

A

Yes on the CRJ 700 / 900, but not allowed on the CRJ 200

173
Q

What is the tail wind component limitation for take off using reduced thrust

A

5 KTS

174
Q

If windshear is reported, can you take off?

A

Yes, but normal thrust must be used.

175
Q

Can you use reduced thrust if the runway is contaminated?

A

NO

176
Q

What preflight duty must be completed when the OAT is 5 degrees or less?

A

a Cold Weather Preflight Inspection must be completed

177
Q

What Appendix is the O2 requirements for a jumpseater found?

A

Appendix A

178
Q

Supplemental Operating Procedures are found in what Appendix?

A

Appendix A

179
Q

What Appendix addresses tire wear criteria?

A

Appendix H

180
Q

Contact Mx Control if the tire is worn to the bottom of any groove to 1/8th the circumference of which variant?

A

CRJ 200

2014 AQP Study Guide (8 decks)

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