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XJT CRJ 200 > CRJ200 Limitations > Flashcards

CRJ200 Limitations Flashcards

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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
Min. Go-Around Fuel
450 lbs. per wing (10 degree nose up MAX)
25
Single Engine Taxi Fuel Boost Pumps
L R Boost Pumps Off (prevents imbalance)
26
APU Start Limits (Batt or Normal In-Flight)
First Attempt - 30 sec = 2 minutes | Second Attempt - 30 sec = 20 min OFF
27
APU Starting (Ext. Ground Power)
First Attempt - 15 seconds = 2 min OFF | Second Attempt - 15 seconds = 20 min OFF
28
APU Start Delay
2 min between cranking attempts
29
APU Bleed Air Limits (A/C)
No extraction above 15,000 ft
30
APU Bleed Air Limitations (Ground Ops Engine Start)
No Limitation - Operating Engine Thrust < 70% N2
31
APU Bleed Air (In-Flight Start) - | Single Engine vs Dual Engine Failure
Single Engine Start (APU Bleed not permitted) | Dual Engine Failure (APU Bleed <13,000 ft only)
32
What could occur with Rapid/Large Alternating Control Inputs
AVOID: Structural Failure may occur at any speed below VA
33
Flap Operating Speed (0 - 8 degrees)
200 KIAS
34
Flap Operating Speed (8 - 20 degrees)
200 KIAS
35
Flap Operating Speed (20 - 30 degrees)
185 KIAS
36
Flap Operating Speed (30 - 45 degrees)
170 KIAS
37
Flap Operating Speeds
``` 200 KIAS (0-20), 185 KIAS (20-30), 170 KIAS (30-40) ```
38
Max. Flap Extended Speed - 8 degrees
215 KIAS
39
Max. Flap Extended Speed - 20 degrees
215 KIAS
40
Max. Flap Extended Speed - 30 degrees
185 KIAS
41
Max. Flap Extended Speed - 45 degrees
170 KIAS
42
Max. LDG Gear Extend Speed
250 KIAS
43
Max. LDG Gear Retract Speed
200 KIAS
44
Max. Gear Down Speed (in flight)
250 KIAS
45
Tire Limit Speed (not required)
182 kts. Ground Speed
46
Max. Turbulence Penetration speed
280 KIAS or .75 Mach
47
Minimum Operating Speed
Not below that which activates stick shaker
48
Windshield Wiper Operation
220 KIAS
49
Max. Wind Limitation
60 kts. (55 kts. Headwind)
50
Crosswind Limits (Dry, Wet, PIC < 100 hrs)
27 kts.
51
Crosswind Limits (Braking Action < Good)
15 kts.
52
What is Required when using a Low Pressure Air Source (not required)
Cabin or Avionics Bay Door Open
53
Autopilot Altitude Limit (AFCS)
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
ADC and ATC transponder
Same source while in RVSM airspace
55
When is Bleed Air 10th Stage Valves (T/O and LDG) not allowed?
Closed if Wing/Cowl ON
56
Max. DC Power (Ground Ops)
5 min.
57
Circuit Breaker Reset
Only by QRH/OM or PIC for safety of flight
58
Flaps In-Flight (Max. Extended)
Enroute Prohibited and/or above 15,000 ft.
59
Spoilers In-Flight
VREF + 17 kts. Below 800 ft. AGL Flaps Max. 30 degrees
60
Stall Protection System
Test before FFoD | ON for all phases of flight
61
Taxi Light
OFF if stationary > 10 min.
62
Thrust Reverse Limitations
``` 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
Brake Temp Monitor System (BTMS)
15 min. Cool Down Max. 6 (above 5 use QRH PERF 12)
64
Respond to a TCAS RA
Must comply unless performance limited Engine Failure Obvious Error
65
Conditions a EGPWS will Fail to Alert
When no GPS input and Surface Temp < ISA, Non-Standard Lapse Rate, Incorrect Barometric Settings on Altimeter
66
Max. Speed for ADG deployment for test flights/training?
215 KIAS
67
Max Cruise Speed for RVSM airspace
.85 Mach
68
Max. M (MO) Speed
.85 Mach
69
What ALT to be set in MDA window on ILS app with DA of 212?
220 feet (increments of 10 ... go to next highest)
70
Can a pilot deviate from ATC Clearance to comply with a TCAS RA?
Yes
71
Minimum Stable Approach Altitude (Cat. II)
1000 feet AGL
72
Accept Cat. II APP w/ Braking Action Fair or Poor
No Cat II should be accepted with Braking Action Report LESS than FAIR
73
Cat. II Operations Wind Limitations
15 kts. Crosswind 17 kts. Headwind 10 kts. Tailwind
74
Min. Bulk Fuel Temp for Takeoff
-30 degrees C (Jet A)
75
Max. Engine ITT allowed during Takeoff
900 degrees C
76
Cold Weather Ops (-20 C) -- Min. N2 to accelerate above idle?
57%
77
After Abnormal Start (unless another start successful)
Call Maintenance
78
Max. ITT for fuel introduction during ground starts
120 C
79
Max. ITT for fuel introduction during in-flight starts (not memory item)
90 C
80
Max. N2 for starter engagement
55%
81
Max Starter Time for 1st Dry Motor (not memory item)
90 seconds
82
Cooling Period after Dry Motor (not memory item)
5 minutes
83
Difference between Dry Motor & Starter Attempt? (not memory item)
Thrust Levers OFF during Dry Motor
84
Max Time On for APU start (on BATT start)?
30 seconds
85
Max. Time On for APU start (or Ground start)?
15 seconds
86
First Failed Start on APU
2 minute delay (cool of starter, start contactor, APU drainage)
87
What Restriction is placed on Bleed Loading after APU start
Delay 2 minutes to reduce EGT spiking
88
Min. ALT for Single Pack Operations
FL250 MEL limitation on Dispatch Release, TLR or QRH (in-flight)
89
Prior to Opening Doors (not memory item)
Complete Depressurization
90
Limitation on FMS as related to Calculated Thrust Settings (not memory item)
Must not be used if Pressure ALT > 36,000 feet
91
When should GRND PROX TERRAIN switch be selected to OFF?
Within 15NM of Landing or Taking off From an airport NOT in the EGPWS airport database.
92
Definition of icing conditions (in-flight)
TAT
93
When to use Cowl Anti-Ice?
ICE Light ON by Ice Detection System or ICE Conditions
94
When to use Wing Anti-Ice?
ICE Light ON by Ice Detection System or ICE Conditions and
95
Limitation of of Type II or IV fluids and Wing Anti-Ice
Do not turn on until just before Takeoff Power applied
96
Flight into SLD icing conditions
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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