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CRJ 200 > Limitations > Flashcards

Limitations Flashcards

0
Q

Maximum Takeoff Weight

A

53,000 lbs

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1
Q

Maximum Ramp Weight

A

53,250 lbs

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2
Q

Maximum Landing Weight

A

47,000 lbs

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3
Q

Maximum Zero Fuel Weight

A

44,000 lbs

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4
Q

Max AFT Cargo

A

3,500 lbs

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5
Q

Flight Time to Suitable airport

A

45 minute

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6
Q

Minimum Runway Width

A

100 ft

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7
Q

Maximum Operating Altitude (Skywest)

A

37,000 ft

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8
Q

Minimum airspeed at cruise

A

250 KIAS or M.70

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9
Q

Maximum Takeoff and Landing Altitude

A

10,000 ft

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10
Q

Maximum Takeoff and Landing Temperature

A

ISA + 35°C

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11
Q

Minimum Temperature for Takeoff

A

-40°C

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12
Q

Maximum Tailwind

A

10 knots

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13
Q

Vmo

A

335 KIAS

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14
Q

Mmo

A

.85 M

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15
Q

Vfo 8

A

200 KIAS

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16
Q

Vfo 20

A

200 KIAS

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17
Q

Vfe 8

A

215 KIAS

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18
Q

Vfe 20

A

215 KIAS

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19
Q

Vfe 30

A

185 KIAS

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20
Q

Vfe 45

A

170 KIAS

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21
Q

Vlo ext

A

200 KIAS

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22
Q

Vlo ret

A

200 KIAS

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23
Q

Vle

A

220 KIAS

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24
Q

Vtire

A

182 knots ground speed

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25
Q

Vadg deploy max (wet)

A

250 KIAS

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26
Q

Vadg deploy max (dry)

A

Vmo/Mmo

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27
Q

Vb

A

280 KIAS

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28
Q

Mb

A

.75 M

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29
Q

Vwiper ops max

A 
200 = 220 KIAS
(700/900 = 250 KIAS)
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30
Q

When does anti-skid become available?

A

> 35 knots or WOW +5 sec

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31
Q

When is anti-skid inop?

A

Below 10 knots

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32
Q

Maximum altitude for slats/flaps

A

15,000 ft

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33
Q

Minimum airspeed with deployed spoilers

A

Approach speed +20 knots

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34
Q

Minimum altitude with deployed spoilers

A

1,000 ft AGL

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35
Q

Maximum ITT for engine start (nice to know)

A

900°C (red)

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36
Q

Minimum N1 reduced thrust setting

A

3A1 engine: 85%

3B1 engine: 83.5%

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37
Q

N2 idle (nice to know)

A

56.5 - 68.0% (green)

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38
Q

Engine Start (Ground) attempts: starter time limits 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

Verify ITT is 120°C or less for all ground starts before moving thrust lever from SHUTOFF to IDLE.

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39
Q

Dry Motoring (Ground) time limits

A

90 sec ON - 5 minutes OFF

30 sec ON - 5 minutes OFF

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40
Q

Pressure Refueling: Total USABLE FUEL (6.75 lbs/gal)

A 
200 = 14,518 lbs
700/900 = 19,594 lbs
41
Q

Total usable fuel - gravity refueling

A 
200 = 13,906
700 = 14,580
900 = 14,810
42
Q

Maximum Fuel Imbalance

A

800 lbs

43
Q

Maximum Fuel Imbalance FOR TAKEOFF

A 
200 = 800 lbs
700/900 = 300 lbs
44
Q

Minimum Fuel per wing for a Go-around

A 
200 = 450 lbs (amber)
700/900 = 600 lbs
45
Q

Maximum KVA for each Main Generator up to 35,000 ft (nice to know)

A

30 KVA

46
Q

Maximum KVA for each Main Generator above 35,000 ft (nice to know)

A

25 KVA

47
Q

Maximum KVA for APU up to 37,000 ft (MUST KNOW)

A

30 KVA

48
Q

Maximum time limit to use only DC Power on the ground

A

5 minutes

49
Q

Automatic Flight Control System AFCS: IAS mode limitation

A

IAS Mode is prohibited during approach

50
Q

Automatic Flight Control System AFCS: APPR Mode limitation

A

APPR Mode prohibited during VOR approaches

51
Q

Automatic Flight Control System AFCS: Minimum Altitude use for Takeoff

A

600 ft AGL

52
Q

Automatic Flight Control System AFCS: Minimum Altitude Use during Non-precision or Visual approach

A

400 ft AGL

  • The autopilot may not be used less than 50 feet below the approved MDA for the approach procedure or 400 feet AGL, whichever is higher.
53
Q

Automatic Flight Control System AFCS: Precision Approach limitations

A

Glide path must be less than or equal to 3.5°

Minimum Altitude Use : 80 ft AGL

54
Q

APU Maximum Operating Altitude

A

37,000 ft

55
Q

APU Maximum Start Altitude

A

30,000 ft

56
Q

APU Maximum Altitude for bleed air use

A

15,000 ft

57
Q

APU Maximum Altitude for engine start assist

A

13,000 ft

58
Q

APU Start Limitation using Aircraft Battery

A 
30 sec ON - 2 min OFF
30 sec ON - 20 min OFF
30 sec ON - 2 min OFF
30 sec ON - 40 min OFF
(Do not perform more than 3 starts/start attempts in one hour.)
59
Q

Maximum Differential Pressurization (nice to know)

A

8.7 psi

60
Q

Maximum Negative Pressure Differential (nice to know)

A

-0.5 psi

61
Q

Maximum Single Pack Operation altitude:

A

FL 250

62
Q

What altitude does the CPAM bring the cabin altitude in an Emergency Depressurization?

A

14,250 +/- 750 ft Cabin Pressure Altitude (CPA)

63
Q

Maximum N2 ground idle split

A

No greater than 2% split

64
Q

Engine Warm-Up: If N2 is 57% or less when OAT is -20°C or warmer, then

A

Do not accelerate above idle.

65
Q

Engine Warm-Up: After all STARTS,

A

Do not exceed 75% N1 for TWO MINUTES after start, or until all operating indications are in normal range, which ever is longer.

66
Q

Engine Warm-Up: Before the FFOD, when airplane is COLD-SOAKED at a temperature of

A

-30°C OR BELOW for more than 8 hours, engines must be motored for 60 seconds and fan rotation verified before engine start is initiated.

67
Q

Engine Warm-Up: CRJ 200 preflight- If aircraft has been cold soaked for more than 8 hours, the thrust reversers

A

Must be actuated during preflight checks until the deploy and stow cycles are less than 5 seconds.

68
Q

Continuous ignition must be used during the following: (5)

A
  • Takeoffs and Landings on contaminated runways
  • Crosswind components > 10 knots (CRJ 200 only)
  • Flight in moderate or heavier intensity rain
  • Flight in moderate or heavier intensity turbulence
  • Flight in vicinity if thunderstorms
69
Q

Thrust Reversers: go-around restriction

A

Do not attempt a go-around maneuver after deployment of the thrust reversers.

70
Q

Thrust Reversers: Landing limitations

A

Do not use maximum reverse thrust below 75 KIAS. Reverse thrust must be at idle (not above 30% N1) below 60 KIAS.

71
Q

When must engine oil level be checked?

A

Within 3 minutes to 2 hours if every engine shutdown.

72
Q

APU bleed limitation: taxiing single engine, N2 on operating engine must be below ______ before/during second engine start

A

The operating engine’s thrust must not exceed 70% N2

73
Q

APU CRJ 200: Starter limitation - max time below 50% rpm

A

60 seconds maximum

74
Q

During taxi, LANDING AND TAXI LIGHTS must be turned OFF if stationary longer than

A

10 minutes

75
Q

Takeoff with a fuel load in excess of

A

500 LB in the center tank is not permitted unless each main tank is above 4,400 LB.

76
Q

Takeoff with engine fuel temperature indications (nice to know)

A

BELOW 5°C is PROHIBITED

L/R FUEL LO TEMP caution message

77
Q

Bulk fuel minimum takeoff temperature limit

A

-30°C

78
Q

Bulk fuel freezing point

A

-40°C

79
Q

TCAS: Pilots are authorized to deviate from Air Traffic Control clearances in order to comply with

A

a TCAS resolution advisory (RA) command.

80
Q

Reduced thrust takeoffs are prohibited when: (7)

A
  • Cowl and/or wing anti-ice is selected on.
  • The takeoff runway is contaminated with standing water, slush, ice, or snow
  • Taliwind components in excess of 5 knots
  • Warnings of windshear or downdrafts have been forecasted or reported
  • Anti-skid is inoperative
  • Takeoff behind a heavy aircraft
  • CRJ 200 : Flaps 8 takeoff
81
Q

Are reduced thrust takeoffs permitted on wet runways?

A

Yes. Reduced thrust takeoffs on wet runways are permitted.

82
Q

If ACARS performance is not available, then

A

The appropriate additions to V1 and VR using the laminated flight deck flip cards must be made

83
Q

Icing Conditions on the ground/takeoff

A

When OAT is 10°C or below: visible moisture, or when operating on contaminated ramps, taxiways, or runways

84
Q

Icing Conditions in flight

A

When the TAT is 10°C or below and visible moisture in any form is encountered, except when the SAT is -40°C or below.

85
Q

A Cold Weather Preflight Inspection must be performed by a flight deck crewmember during the external walkaround inspection to determine the wing is free from frozen contaminants when: (6)

A
  • The OAT is 5°C or less, or
  • The wing fuel temperature is 0°C or less, or
  • Atmospheric conditions conducive to icing exist, or
  • The aircraft has remained overnight and may have frozen contaminants due to exposure to frost or precipitation, which could involve the entire airframe, or
  • On any through flight where residual ice from the inbound flight may have accumulated on airframe surfaces or components, or
  • Cold soak ice is suspected in the fuel tank area
86
Q

Frost or ice on the ____ _____ of the wing must be removed.

A

upper surface

87
Q

The cowl anti-ice system must be ON for takeoff when

A

OAT is 10°C or below and visible moisture is present ( includes fog w/visibility of 1 mi or less) OR if runway is contaminated

88
Q

The cowl anti-ice system must be ON for taxi when

A

the OAT is 10°C or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush is present, visible moisture is present, or visibility 1 mile or less

89
Q

CRJ 200 Wing Anti-ice: during taxi

A

Wing Anti-ice must be ON when OAT is 5°C and colder (with or without visible moisture) and have NOT used type II or IV to anti-ice. 200 only!

90
Q

CRJ 200 Wing Anti-ice: if Type II or IV anti-ice fluids have been applied, then

A

Do not turn on wing anti-ice for final taxi

91
Q

When must the “WING A/I ON” advisory message be displayed

A

Prior to takeoff

92
Q

If wing anti-ice is on and APU is OFF, then

A

a “BLEED MISCONFIG” caution message will be displayed.

93
Q

Bombardier definition of final taxi:

A

The period following SECOND ENGINE START or about 2 MINUTES prior to takeoff.

94
Q

Takeoff - Wing Anti-ice: if OAT 5°C or colder and Non-Icing conditions, then

A

Turn the WING anti-ice OFF just prior to takeoff.

95
Q

When must the wing anti-ice be on for take off?

A

OAT 5°C or colder and:

  • Visible moisture in any form (clouds, fog, or mist) BELOW 400 ft AGL is REPORTED, or
  • The runway is WET or CONTAMINATED or,
  • ANY precipitation exists or,
  • visibility is 1 SM or less.
96
Q

In flight, when must the engine cowl anti-ice system be ON?

A

When in ICING CONDITIONS, or when “ICE” IS ANNUNCIATED by the ice detection system.

97
Q

In flight, when must the wing anti-ice system be ON?

A

When “ICE” IS ANNUNCIATED by ice detection system, or in ICING CONDITIONS and airspeed is less than 230 KIAS.

98
Q

Definition of “wet runway”:

A

REFLECTIVE with a WATER DEPTH LESS THAN 1/8” covering 100% of runway surface

99
Q

Definition of contaminated runway:

A

More than 25% of runway within the REQUIRED LENGTH and WIDTH being used, is COVERED by MORE THAN 1/8” of STANDING WATER or ITS EQUIVALENT in slush, or wet or dry snow.

CRJ 200 (3 decks)

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