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XJT CRJ 200 > CRJ200 Limitations > Flashcards

CRJ200 Limitations Flashcards

0
Q

Max. Ramp Weight (MRW)

A

53,250 lbs.

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1
Q

Cargo Load Limit

A

3,500 lbs.

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2
Q

Max. Takeoff Weight (MTOW)

A

53,000 lbs.

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3
Q

Max. Landing Weight (MLW)

A

47,000 lbs.

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4
Q

Max. Zero Fuel Weight (MZFW)

A

44,000 lbs.

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5
Q

Max. Airport Pressure Altitude (T/O & LDG)

A

10,000 ft.

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6
Q

Max. Operating Altitude

A

41,000 ft.

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7
Q

Max. Ambient Air Temp. (T/O & LDG)

A

ISA + 35 C

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8
Q

Min. Ambient Temp. for Takeoff

A

-40 C

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9
Q

How to Avoid Excessive Rotation Rate / Pitch Attitude

A

3 degrees
Rotate Smoothly to Target Pitch Attitude
Transition to Speed Control

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10
Q

Max. Tailwind T/O & LDG

A

10 kts.

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11
Q

Pitch Trim

A

Set according to A/C computed CG

Failure may result in excessive rotation

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12
Q

Runway Slope Limitations

A

+/- 2% (up/down) (T/O & LDG)

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13
Q

Min. Flight Crew

A

2 (Pilot and CoPilot)

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14
Q

Engine Stabilization

A

TakeOff: 2 min
Shutdown: 2 min < 80% N2

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15
Q

Conditions to Monitor when Aircraft Cold Soaked

A

Mon for Engines 60 sec.
FFoD w/ Temps < -30 C [-22 F] ( > 8 hours)
Thrust Reversers (Min. 5 sec cycle)

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16
Q

Continuous Engine Ignition Required

A

T/O or LDG - Contaminated Runways
T/O > 10 kts. XW
Flight w/ Mod-Heavy Rain and/or Heavy Turb
Flight Vicinity T-Storms

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17
Q

Starter Cranking Limits

A

First Attempt - 1 minute = 10 sec off

N2 not to exceed 55% prior to engage

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18
Q

Ground Starts ITT Limitation

A

ITT < 120 C

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19
Q

Reduced Thrust Takeoff N1 Fan Speed Limits

A

Cannot be used if takeoff fan speed < 85% N1

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20
Q

Reduced Thrust Not Allowed

A

Wing/Cowl Anti-Ice Bleeds On
Contaminated Runway
Windshear/Downdrafts Forecasted

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21
Q

Reduced Thrust Actual Temperature

A

Don’t use SAT. Only current surface Wx

Wet Runways Ok if applicable Perf Data used.

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22
Q

Max. Fuel Imbalance

A

800 lbs.

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23
Q

Center Fuel Tank Takeoff

A

< 500 lbs. prohibited unless each wing > 4,400 lbs.

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24
Q

Min. Go-Around Fuel

A

450 lbs. per wing (10 degree nose up MAX)

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25
Q

Single Engine Taxi Fuel Boost Pumps

A

L R Boost Pumps Off (prevents imbalance)

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26
Q

APU Start Limits (Batt or Normal In-Flight)

A

First Attempt - 30 sec = 2 minutes

Second Attempt - 30 sec = 20 min OFF

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27
Q

APU Starting (Ext. Ground Power)

A

First Attempt - 15 seconds = 2 min OFF

Second Attempt - 15 seconds = 20 min OFF

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28
Q

APU Start Delay

A

2 min between cranking attempts

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29
Q

APU Bleed Air Limits (A/C)

A

No extraction above 15,000 ft

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30
Q

APU Bleed Air Limitations (Ground Ops Engine Start)

A

No Limitation - Operating Engine Thrust < 70% N2

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31
Q

APU Bleed Air (In-Flight Start) -

Single Engine vs Dual Engine Failure

A

Single Engine Start (APU Bleed not permitted)

Dual Engine Failure (APU Bleed <13,000 ft only)

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32
Q

What could occur with Rapid/Large Alternating Control Inputs

A

AVOID: Structural Failure may occur at any speed below VA

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33
Q

Flap Operating Speed (0 - 8 degrees)

A

200 KIAS

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34
Q

Flap Operating Speed (8 - 20 degrees)

A

200 KIAS

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35
Q

Flap Operating Speed (20 - 30 degrees)

A

185 KIAS

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36
Q

Flap Operating Speed (30 - 45 degrees)

A

170 KIAS

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37
Q

Flap Operating Speeds

A 
200 KIAS (0-20), 
185 KIAS (20-30), 
170 KIAS (30-40)
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38
Q

Max. Flap Extended Speed - 8 degrees

A

215 KIAS

39
Q

Max. Flap Extended Speed - 20 degrees

A

215 KIAS

40
Q

Max. Flap Extended Speed - 30 degrees

A

185 KIAS

41
Q

Max. Flap Extended Speed - 45 degrees

A

170 KIAS

42
Q

Max. LDG Gear Extend Speed

A

250 KIAS

43
Q

Max. LDG Gear Retract Speed

A

200 KIAS

44
Q

Max. Gear Down Speed (in flight)

A

250 KIAS

45
Q

Tire Limit Speed (not required)

A

182 kts. Ground Speed

46
Q

Max. Turbulence Penetration speed

A

280 KIAS or .75 Mach

47
Q

Minimum Operating Speed

A

Not below that which activates stick shaker

48
Q

Windshield Wiper Operation

A

220 KIAS

49
Q

Max. Wind Limitation

A

60 kts. (55 kts. Headwind)

50
Q

Crosswind Limits (Dry, Wet, PIC < 100 hrs)

A

27 kts.

51
Q

Crosswind Limits (Braking Action < Good)

A

15 kts.

52
Q

What is Required when using a Low Pressure Air Source (not required)

A

Cabin or Avionics Bay Door Open

53
Q

Autopilot Altitude Limit (AFCS)

A

Prohibited below 600 AGL except:
VIS/NP APP: 400 AGL or 50 below MDA
Precision APP: 80 ft. AGL or 50 below DA
DES sub mode (Flight Director/AP Coupled) Prohibited

54
Q

ADC and ATC transponder

A

Same source while in RVSM airspace

55
Q

When is Bleed Air 10th Stage Valves (T/O and LDG) not allowed?

A

Closed if Wing/Cowl ON

56
Q

Max. DC Power (Ground Ops)

A

5 min.

57
Q

Circuit Breaker Reset

A

Only by QRH/OM or PIC for safety of flight

58
Q

Flaps In-Flight (Max. Extended)

A

Enroute Prohibited and/or above 15,000 ft.

59
Q

Spoilers In-Flight

A

VREF + 17 kts.
Below 800 ft. AGL
Flaps Max. 30 degrees

60
Q

Stall Protection System

A

Test before FFoD

ON for all phases of flight

61
Q

Taxi Light

A

OFF if stationary > 10 min.

62
Q

Thrust Reverse Limitations

A 
Not Permitted below 60 kts. 
T/O Prohibited w/ :
THRUST REVERSER UNLK light
REV icon on N1 gauge
L/R REV UNLOCKED Caution MSG
Preflight Limited to Reverse Idle
Taxi Ops and Backing Up Prohibited
(Emergency Ops only)
63
Q

Brake Temp Monitor System (BTMS)

A

15 min. Cool Down Max. 6 (above 5 use QRH PERF 12)

64
Q

Respond to a TCAS RA

A

Must comply unless performance limited
Engine Failure
Obvious Error

65
Q

Conditions a EGPWS will Fail to Alert

A

When no GPS input and
Surface Temp < ISA,
Non-Standard Lapse Rate,
Incorrect Barometric Settings on Altimeter

66
Q

Max. Speed for ADG deployment for test flights/training?

A

215 KIAS

67
Q

Max Cruise Speed for RVSM airspace

A

.85 Mach

68
Q

Max. M (MO) Speed

A

.85 Mach

69
Q

What ALT to be set in MDA window on ILS app with DA of 212?

A

220 feet (increments of 10 … go to next highest)

70
Q

Can a pilot deviate from ATC Clearance to comply with a TCAS RA?

A

Yes

71
Q

Minimum Stable Approach Altitude (Cat. II)

A

1000 feet AGL

72
Q

Accept Cat. II APP w/ Braking Action Fair or Poor

A

No Cat II should be accepted with Braking Action Report LESS than FAIR

73
Q

Cat. II Operations Wind Limitations

A

15 kts. Crosswind
17 kts. Headwind
10 kts. Tailwind

74
Q

Min. Bulk Fuel Temp for Takeoff

A

-30 degrees C (Jet A)

75
Q

Max. Engine ITT allowed during Takeoff

A

900 degrees C

76
Q

Cold Weather Ops (-20 C) – Min. N2 to accelerate above idle?

A

57%

77
Q

After Abnormal Start (unless another start successful)

A

Call Maintenance

78
Q

Max. ITT for fuel introduction during ground starts

A

120 C

79
Q

Max. ITT for fuel introduction during in-flight starts (not memory item)

A

90 C

80
Q

Max. N2 for starter engagement

A

55%

81
Q

Max Starter Time for 1st Dry Motor (not memory item)

A

90 seconds

82
Q

Cooling Period after Dry Motor (not memory item)

A

5 minutes

83
Q

Difference between Dry Motor & Starter Attempt? (not memory item)

A

Thrust Levers OFF during Dry Motor

84
Q

Max Time On for APU start (on BATT start)?

A

30 seconds

85
Q

Max. Time On for APU start (or Ground start)?

A

15 seconds

86
Q

First Failed Start on APU

A

2 minute delay (cool of starter, start contactor, APU drainage)

87
Q

What Restriction is placed on Bleed Loading after APU start

A

Delay 2 minutes to reduce EGT spiking

88
Q

Min. ALT for Single Pack Operations

A

FL250

MEL limitation on Dispatch Release, TLR or QRH (in-flight)

89
Q

Prior to Opening Doors (not memory item)

A

Complete Depressurization

90
Q

Limitation on FMS as related to Calculated Thrust Settings (not memory item)

A

Must not be used if Pressure ALT > 36,000 feet

91
Q

When should GRND PROX TERRAIN switch be selected to OFF?

A

Within 15NM of Landing or Taking off From an airport NOT in the EGPWS airport database.

92
Q

Definition of icing conditions (in-flight)

A

TAT

93
Q

When to use Cowl Anti-Ice?

A

ICE Light ON by Ice Detection System or ICE Conditions

94
Q

When to use Wing Anti-Ice?

A

ICE Light ON by Ice Detection System or ICE Conditions and

95
Q

Limitation of of Type II or IV fluids and Wing Anti-Ice

A

Do not turn on until just before Takeoff Power applied

96
Q

Flight into SLD icing conditions

A

Prohibited - Wing and Cowl Anti Ice Required ON

Indicated by Ice Accretion on Flight Compartment Side Windows

XJT CRJ 200 (3 decks)

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