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2013 AQP Study Guide > Knowledge Validation > Flashcards

Knowledge Validation Flashcards

1
Q

CRJ 200 Max Ramp Weight

A

53,250 lbs

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2
Q

CRJ 200 Max Take Off Weight

A

53,000 lbs

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3
Q

CRJ 200 Max Landing Weight

A

47,000 lbs

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4
Q

CRJ 200 Max Aft Cargo

A

3500 lbs

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5
Q

CRJ 200 Max Ops Altitude

A

37,000 ft

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6
Q

Max Tail Wind all 3 variants

A

10 kts

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7
Q

CRJ 200 Mmo

A

.85 Mach

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8
Q

CRJ 200 Vlo Ext

A

220 KIAS

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9
Q

CRJ 200 Vlo Ret

A

200 KIAS

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10
Q

CRJ 200 Vtire

A

182 kts GS

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11
Q

CRJ 200 V adg Deploy

A

250 KIAS

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12
Q

CRJ 200 Vb

A

280 KIAS

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13
Q

CRJ 200 Mb

A

.75 Mach

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14
Q

CRJ 200 V wiper ops Max

A

220 KIAS

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15
Q

CRJ 200 Hydraulics Norm PSI

A

2930 - 3050 PSI (Green)

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16
Q

CRJ 200 Hydraulics Norm Level

A

45% to 85% (Green)

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17
Q

CRJ 200 Min Spoiler Speed

A

Vref + 17

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18
Q

CRJ 200/700/900 Min Alt Spoilers

A

300 ft AGL

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19
Q

CRJ 200 Max ITT Cont Thrust 3A1 Engines

A

860 degrees C

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20
Q

CRJ 200 Max ITT Continuous Thrust 3B1 Engines

A

874 degrees C

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21
Q

CRJ 200 Max Start

A

900 degrees C

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22
Q

CRJ 200 Max Oil Pressure after cold start

A

Engine must remain at idle thrust until oil PSI returns to normal range.

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23
Q

CRJ 200 Max Refill without motoring

A

2 qt.

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24
Q

CRJ 200 Engine Start Limitations

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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25
Q

CRJ 200 Max Fuel Imbalance

A

800 lbs.

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26
Q

CRJ 200 Max Fuel Imbalance for Take Off

A

800 lbs.

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27
Q

CRJ 200 Min for Go Around per wing

A

450 lbs (Amber)

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28
Q

IAS Mode during approach

A

Prohibited

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29
Q

CRJ 200 Max Glide Path Angle on Precision Approach using AFCS (Auto Pilot)

A

equal to or less than 3.5 degrees

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30
Q

CRJ 200 Minimum altitude use of AFCS (Auto Pilot) after Take Off

A

600 ft AGL

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31
Q

CRJ 200 Use of AFCS on Non Precision Approach AFE of 4000 ft and below

A

Approved

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32
Q

CRJ 200 Use of AFCS on Non Precision Approach above AFE of 4000 ft

A

Approved

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33
Q

CRJ 200 Minimum altitude of use of AFCS on Non Precision Approach

A

400 ft AGL

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34
Q

AFCS

A

Auto Pilot - Auto Flight Control System

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35
Q

CRJ 200 Minimum altitude of use of AFCS on Precision Approach

A

80 ft AGL

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36
Q

CRJ 200 APU Max Continuous EGT

A

743 degrees Celsius (Red)

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37
Q

CRJ 200 APU Max Start Altitude

A

30,000 ft.

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38
Q

CRJ 200 APU start times using AC Battery

A

2x30 sec ON followed by 20 Min OFF

2x30 sec ON followed by 40 Min OFF

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39
Q

CRJ 200 Max Pressure Differential

A

8.7 psi

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40
Q

CRJ 200 Emergency Depressurization Switch depressurizes AC Cabin to

A

14,250 ft. +/- 750 ft.

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41
Q

Max N2 Split on ground at idle thrust

A

2% N2

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42
Q

If N2 is 57% or less when OAT is -20C

A

DO NOT ADVANCE THRUST LEVERS ABOVE IDLE

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43
Q

After all starts, do not advance thrust levers above idle thrust

A

For 2 minutes after start, or until all engine operating indications are normal, whichever is longer

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44
Q

CRJ 200 When the AC is cold soaked for longer than 8 hours at a temperature of -30C and less (engines)

A

The engines must be dry motored for 60 seconds and fan rotation verified

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45
Q

When the AC is cold soaked for longer than 8 hours at a temperature of -30C and less (thrust reverse)

A

The Thrust Reverse must be actuated until the deploy and stow cycles are less than 5 seconds.

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46
Q

Continuous Ignition must be used during the following

A

Takeoffs and Landings on Contaminated Runways
Takeoffs with Crosswinds greater than 10 KTS (200 Only)
Flight through Moderate or Heavier Intensity Rain Flight through Moderate or Heavier Turbulence
Flight in the vicinity of Thunderstorms

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47
Q

Restriction on CRJ 200 when both engines are to be started using APU bleed air

A

Operating Engines Thrust must not exceed 70% N2

48
Q

Take Off Restriction when more than 500 lbs of fuel in the center tank

A

Prohibited unless each main tank is more than 4400 lbs

49
Q

CRJ 200 Min O2 Pressure for Take Off

A

1410 PSI

50
Q

CRJ 200 Min 02 Pressure for International Ops

A

1650 PSI

51
Q

CRJ 700 / 900 Minimum O2 for Dispatch

A

960 PSI

52
Q

CRJ 700 / 900 Minimum O2 for International Ops

A

1650 PSI

53
Q

Reduced Thrust Take Off Limitations

A

APR OFF Performance will be used to determine the assumed Temperature
Prohibited when:
Cowl Anti Ice or Wing Anti Ice is selected ON
Take Off Runway is contaminated with standing water, slush, snow or ice.
Tailwind Component in excess of 5 KTS
Warnings of wind shear or down drafts have been FORECAST or REPORTED
ANTI-SKID is inoperative
Takeoff behind a Heavy Aircraft
Flaps 8 Takeoff (200 Only)

54
Q

Are Reduced Thrust Takeoffs approved on Wet Runways?

A

YES

55
Q

Definition of Wet Runway

A

Enough moisture to cause it to appear reflective, with a water depth less than 1/8th inch, covering 100% of the runway surface

56
Q

If there are dry spots on the runway, is it considered to be wet?

A

NO

57
Q

Contaminated Runway Definition

A

When more than 25% of the runway surface is covered by more than 1/8 inch standing water or it’s equivalent of dry snow, slush or wet snow

58
Q

CRJ 700 Max Ramp Weight

A

75,250 lbs.

59
Q

CRJ 900 Max Ramp Weight

A

85,000 lbs.

60
Q

CRJ 700 Max Take Off Weight

A

75,000 lbs.

61
Q

CRJ 900 Max Take Off Weight

A

84,500 lbs.

62
Q

CRJ 700 Max Landing Weight

A

67,000 lbs.

63
Q

CRJ 700 Max Aft Cargo Weight

A

3740 lbs.

64
Q

CRJ 700 Max Aft Cargo for Alaska Ops

A

4375

65
Q

CRJ 700 Max Forward Cargo Weight

A

1000 lbs.

66
Q

CRJ 700 Max Aft Cargo for WiFi Equipped AC

A

3650 lbs.

67
Q

CRJ 900 Max Landing Weight

A

75,100 lbs.

68
Q

CRJ 900 Max Aft Cargo Weight

A

3740 lbs.

69
Q

CRJ 900 Max Forward Cargo Weight

A

1700 lbs. Total with a 850/850 lb split

70
Q

CRJ 700/900 When the AC is cold soaked for longer than 8 hours at a temperature of -30C and less (engines)

A

Thrust Reversers must be actuated until the deploy cycle is 2 seconds with an additional 2 seconds for the stow cycle.

71
Q

With the engines running and the bleeds configured for takeoff, N1 value must the crew verify?

A

That the target N1 values correspond with the takeoff data in the TLR +/- 1.0%N1

72
Q

What is the minimum altitude below the MDA the AFCS may be used

A

50 ft below the MDA or 400 ft AGL whichever is higher

73
Q

CRJ 700 Mmo

A

.85 Mach and .83 Mach in RVSM

74
Q

CRJ 900 Mmo

A

.84 Mach and .82 Mach in RVSM

75
Q

Vlo Extended all 3 variants

A

220 KIAS

76
Q

Vle Retraction all 3 variants

A

200 KIAS

77
Q

Vtire 700

A

182 KIAS

78
Q

Vtire 900

A

195 KIAS

79
Q

CRJ 700/900 Vadg Deploy Max

A

Vmo/Mmo

80
Q

Vb All 3 Variants

A

280 KIAS

81
Q

Mb all 3 Variants

A

.75 Mach

82
Q

CRJ 700/900 Vwiper Ops Max

A

250 KIAS

83
Q

CRJ 700/900 Normal Hydraulic psi

A

3,000 psi

84
Q

CRJ 700/900 Normal Hydraulic Level

A

> 45% to <85%

85
Q

CRJ 700/900 Minimum Speed with Spoilers Extended

A

Vref + 10 KTS

86
Q

CRJ 700 Max Continuous Thrust ITT

A

927 degrees C (Red)

87
Q

CRJ 900 Max Continuous Thrust ITT

A

960 degrees C (Red)

88
Q

CRJ 700 Max ITT for Engine Start

A

815 degrees C (Red)

89
Q

CRJ 900 Max ITT for Engine Start

A

815 degrees C (Red)

90
Q

CRJ 200 Engines

A

CF 34 / 3B1 some with 3A1

91
Q

CRJ700 Engines

A

CF 34 8C1 some with 8C5B1

92
Q

CRJ 900

A

CF 34 8C5

93
Q

CRJ 700/900 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
94
Q

Max Fuel Imbalance all 3 variants

A

800 lbs.

95
Q

CRJ 700/900 Max Imbalance for Take Off

A

300 lbs.

96
Q

CRJ 700/900 Minimum Fuel for Go Around per wing

A

600 lbs.

97
Q

CRJ 700 Use of AFCS on a Precision Approach with a glide slope Equal to or Less than 3.5 degrees

A

Approved for both 4000 ft and below and above 4000 ft airport field elevation

98
Q

CRJ 700 Use of AFCS on a Precision Approach with a glide slope greater than 3.5 degrees, but less than 4 degrees

A

Approved where Airport Elevation is 4000 ft and below.

Prohibited where Airport Elevation is greater than 4000 ft.

99
Q

CRJ 700 Use of AFCS on a Precision Approach with a glide slope greater than 4.0 degrees

A

Prohibited

100
Q

CRJ 700 Can you use the AFCS to fly an ILS with a glide slope of 3.7 degrees to an airport with an elevation of 4100 MSL

A

NO

Anything greater than 3.5 degrees is prohibited above an airport elevation of 4000 ft.

101
Q

CRJ 700 Can you use the AFCS to fly an ILS with a glide slope of 4.1 degrees to an airport with elevation of Sea Level?

A

NO

Anything greater than 4 degrees is prohibited for all airport elevations

102
Q

CRJ 700 Can you use the AFCS to fly an ILS of 4.0 degrees to an airport with an elevation of 4000 ft. ?

A

YES
Equal to and less than 4.0 degree glide slope
Equal to and less than 4000 ft airport elevation

103
Q

CRJ 700 With a glide slope greater than 3.5 to 4.0 degrees, what is the minimum altitude the AFCS can be used

A

120 ft AGL

Not withstanding the limitation for all 3 aircraft of 50 ft above terrain or this limitation, whichever is higher.

104
Q

CRJ 900 Use of the AFCS on a precision approach is limited to a glide slope of:
and a max airport elevation of:

A

3.5 degrees and less

all airports, unless single engine, then limitation is up to an airport elevation of 4000 ft and below

105
Q

CRJ 900 The minimum altitude for use of the AFCS on a precision approach

A

80 ft AGL

Single Engine 110 ft AGL

106
Q

CRJ 700/900 APU Start Limitation

A

Do not perform more than 3 starts in 1 hour

107
Q

Minimum Engine Fuel Temp for Takeoff

A

Takeoff with engine fuel temperature indications of +5 degrees C is prohibited

108
Q

Bulk Fuel Takeoff Limit

A

-30 Degrees C

109
Q

Number of Emergency Memory Items

A

11

110
Q

What are the Emergency Memory Items

A 
1. Hot Start, Interrupted Start, N2 Stagnation 
(CRJ 200)
2. No Light Off (CRJ 200)
3. L / R Start Abort Message, Hot Start (CRJ 700/900)
4. Configuration Warnings
5. Rejected Take-Off
6. Excessive Asymmetry or Loss of Braking
7. Stab Trim Runaway (CRJ 200)
8. Stab Trim Runaway (CRJ 700/900)
9. Stall Recovery
10. Emergency Descent
11. Evacuation
111
Q

How Many Radio Altimeter Antennae are there?

A

4

112
Q

How many Static Wicks on the Tail Section of the CRJ 700

A 
13 Total Static Wicks
3 on each side of the elevator
2 on the Aft Nav Lights
3 on the Rudder
2 on the APU Exhaust
113
Q

How many Static Wicks are on the Wings on the CRJ 700

A

7 on each side

114
Q

How many Static Wicks are on the Wings of the CRJ 200

A

6 on each side

115
Q

How many Static Wicks are on the Tail Section of the CRJ 200

A 
12 or 14 Total
4 on each side of the elevator
1 top center above the top nav light
2 or 4 down the middle of the Rudder
1 bottom center below the aft nav light

2013 AQP Study Guide (5 decks)

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