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CRJ200 Limitations > CRJ 200 Limitations > Flashcards

CRJ 200 Limitations Flashcards

1
Q

MAX RAMP

A

53,250LB

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2
Q

MAX T/O

A

53,000LB

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3
Q

MAX LND

A

47,000LB

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4
Q

MAX ZFW

A

44,000LB

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5
Q

MIN FLT WT.

A

30,000LB

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6
Q

WING SPAN

A

69’8”

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7
Q

AIRCRAFT LENGTH

A

87’10”

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8
Q

TAIL HEIGHT

A

20’8”

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9
Q

MAX OPS ALT

A

37,000’

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10
Q

MAX T/O & LND ALT

A

10,000’

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11
Q

MAX TEMP T/O & LND

A

ISA +35C

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12
Q

MIN TEMP T/0

A

-40C

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13
Q

MAX TAILWIND T/O & LND

A

10KTS

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14
Q

VMO

A

335KTS

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15
Q

MMO

A

MACH .85

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16
Q

VLO EXT

A

220KTS

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17
Q

VLO RET

A

200KTS

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18
Q

VLE

A

220KTS

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19
Q

VTIRE

A

182KTS (GS)

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20
Q

VADG DEPLOY MAX

A

250KTS(WET) VMO/MMO(DRY)

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21
Q

VB

A

280KTS

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22
Q

MB

A

MACH .75

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23
Q

VWIPER OPS MAX

A

22OKTS

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24
Q

VFO 8

A

200KTS

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25
Q

VFO 20

A

200KTS

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26
Q

VFE 8

A

215KTS

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27
Q

VFE 20

A

215KTS

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28
Q

VFE 30

A

185KTS

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29
Q

VFE 45

A

170KTS

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30
Q

MAX ALT SLATS/FLAPS

A

15,000’

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31
Q

FLAPS/SLATS ENROUTE

A

PROHIBITED

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32
Q

MIN SPOILER SPEED

A

APR + 20

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33
Q

MIN ALT SPOILER

A

1,000’ HAT

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34
Q

SPOILERS WITH FLAPS 45

A

PROHIBITED

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35
Q

MIN RUNWAY WIDTH

A

100’

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36
Q

STANDING WATER T/0

A

.5 INCH

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37
Q

STANDING WATER LND

A

.75 INCH

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38
Q

SLUSH T/O

A

.5 INCH

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39
Q

SLUSH LND

A

.88 INCH

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40
Q

WET SNOW T/O

A

1 INCH

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41
Q

WET SNOW LND

A

1.5 INCH

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42
Q

DRY SNOW T/O

A

3 INCH

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43
Q

DRY SNOW LND

A

3.75 INCH

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44
Q

APU MIN TEMP START

A

-40C

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45
Q

MAX APU OPS ALT

A

37,000’

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46
Q

MAX APU START ALT

A

30,000’

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47
Q

MAX APU ALT BLEED USE

A

15,000’

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48
Q

MAX ALT APU ENG START

A

13,000’

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49
Q

MAX DOOR OPEN APU NOT IN USE

A

300KIAS

50
Q

APU BAT START 1

A

30 SECONDS ON 2 MINUTES OFF

51
Q

APU BAT START 2

A

30 SECONDS ON 20 MINUTES OFF

52
Q

APU BAT START 3

A

30 SECONDS ON 2 MINUTES OFF

53
Q

APU BAT START 4

A

30 SECONDS ON 40 MINUTES OFF

54
Q

AUTO PILOT MUST BE ENGAGED ABOVE

A

FL200 UNLESS MEL

55
Q

AUTO PILOT IAS MODE

A

PROHIBITED DURING APP

56
Q

AUTO PILOT DES MODE

A

PROHIBITED DURING APP

57
Q

AUTO PILOT APPR MODE

A

PROHIBITED DURING VOR APPROACH

58
Q

MAX TIME DC ONLY

A

5 MINUTES

59
Q

MAX CONTINUOUS DC TRU

A

100A

60
Q

CARGO FIREX PROVIDES

A

45 MIN FLT TIME TO SUITABLE AIRPORT

61
Q

TOTAL FUEL (PRESSURE REFUELING)

A

14,518LB

62
Q

TOTAL FUEL(GRAVITY REFUELING)

A

13,906LB

63
Q

MAX FUEL IMBALANCE FOR T/O

A

800LB

64
Q

MIN FUEL FOR GA PER WING

A

500 LB

65
Q

MIN BULK FUEL TEMP FOR T/O

A

-30C

66
Q

MIN BULK FUEL TEMP IN FLIGHT

A

-40C

67
Q

MIN REDUCED THRUST 3A1

A

85%

68
Q

MIN REDUCED THRUST 3B1

A

83.5%

69
Q

ENG START ON GND 1

A

60 SECONDS ON 10 SECONDS OFF

70
Q

ENG START ON GND 2

A

60 SECONDS ON 10 SECONDS OFF

71
Q

ENG START ON GND 3

A

60 SECONDS ON 5 MINUTES OFF

72
Q

ENG START ON GND 4

A

60 SECONDS ON 5 MINUTES OFF

73
Q

WHEN BOTH ENGINES ARE TO BE STARTED USING THE APU THE OPERATING ENGINE MUST NOT EXCEED

A

70% N2

74
Q

DRY MOTORING 1

A

90 SECONDS ON 5 MINUTES OFF

75
Q

DRY MOTORING 2

A

30 SECONDS ON 5 MINUTES OFF

76
Q

MAX WINDMILLING/STARTER ASSISTED CROSS BLEED RELIGHT ALT

A

FL210

77
Q

DO NOT EXCEED 75% N1 UNTIL:

A

2 MINUTES OR ALL OPERATING INDICATIONS ARE IN THE GREEN BAND, WHICHEVER IS LONGER.

78
Q

MAX GROUND IDLE SPLIT N2

A

LESS THAN OR EQUAL TO 2%

79
Q

WITH OAT -20C THRST LEVERS AT IDLE N2

A

GREATER THAN 57%

80
Q

IF N2 IS NOT GREATER THAN 57% AT IDLE WITH -20C

A

DO NOT ADVANCE THRUST LEVER, CONTACT MX

81
Q

ENGINE COOL DOWN

A

2 MINUTES AT IDLE/NEAR IDLE THRUST

82
Q

THRUST REVERSER USE DURING TAXI

A

PROHIBITED

83
Q

OIL PRESSURE LIMITS

A

ENGINE MUST REMAIN AT IDEL UNTIL OIL PSI RETURNS TO NORMAL INDICATIONS. MUST BE IN NORMAL RANGE WITHIN 10 MINUTES

84
Q

SINGLE PACK OPS

A

FL250

85
Q

CPAM PAX O2

A

14,000’ +/- 500’

86
Q

BEFORE THE FIRST FLIGHT OF THE DAY WHEN THE AIRPLANE IS COLD SOAKED THE ENGINES MUST BE

A

MOTORED FOR 60 SECONDS AND FAN ROTATION VERIFIED BEFORE ENGINE START IS INITIATED

87
Q

AFTER BEING COLD SOAKED THE THRUST REVERSERS MUST BE ACTUATED UNTIL:

A

THE DEPLOY AND STOW CYCLES ARE LESS THAN 5 SECONDS

88
Q

HOT START, INTERRUPTED START N2 STAGNATION “QRC MEMORY ITEM”

A

AFFECTED THRUST LEVER……SHUTOFF
IGNITION….OFF
DRY MOTOR…..UNTIL ITT REDUCED BELOW 12O DEGREES, RESPECTING THE STARTER TIME LIMIT
AFFECTED ENGINE…STOP

89
Q

NO LIGHT OFF “QRC MEMORY ITEM”

A

AFFECTED THRUST LEVER…SHUTOFF
IGNITION…OFF
DRY MOTOR…UNTIL STARTER LIMIT
AFFECTED ENGINE…STOP

90
Q

At what crosswind component is continuous ignition required for takeoff

A

Greater than 10 kts

91
Q

When is reduced thrust prohibited?

A
  • Wings/Cowls on
  • Contaminated RWY
  • T/O Behind a Heavy
  • Tailwind Greater than 5kts
  • Windshear reported
  • Anti Skid Inop
  • Flaps 8
92
Q

For an unpressurized takeoff, the pressurization is set to what altitude before takeoff?

A

3000’ above field elevation

93
Q

What conditions/indications would direct a decision to abort the takeoff?

A
  • Engine Failures
  • EICAS Warnings
  • REV UNLOCKED
  • SMOKE TOILET
94
Q

The autopilot must be engaged above

A

FL200

95
Q

The autopilot can be engaged at

A

600’

96
Q

What is the climb speed schedule below 10,000

A

250

97
Q

What is the climb speed schedule above 10,000

A

250/.70

98
Q

What bank deviation requires a PM call out

A

In excess of 30 Degrees

99
Q

What Speed deviation requires a PM call out

A

+/- 10 KIAS or .02M

100
Q

What heading from bugged or course deflection require PM call out

A

+/- 10 degrees

Course from established 1/4 deflection

101
Q

What are the PM callouts

A 
SPEED
BANK
HEADING
COURSE
PITCH
VERTICAL SPEED
102
Q

On the Speed Cards VMD speed line, what do the dashed lines indicate?

A

Does not provide adequate bank protection for turns in excess of 15 degrees. Bank angles in excess of 15 degrees and holding are prohibited at these altitudes and weights

103
Q

Double Engine Failure Memory Item

A

IGNITION CONTINOUS

NO LESS THAN 240KIAS

104
Q

When should you arrive at traffic pattern altitude and flap 0 maneuving speed?

A

12 miles out straight-in approach, or

8 miles out abeam approach

105
Q

For VMC circle-to-land the aircraft must be aligned with the runway by?

A

500ft HAT

106
Q

Arming the APPR too early may result in a?

A

False localizer capture

107
Q

Maximum X-Wind for CAT2

A

15kts

108
Q

What are the STABILIZER TRIM RUNAWAY memory items?

A
  • Control Wheel…….Assume Manual Control and Override runaway
  • Both Stab Trim Disc…..Press,Hold,and Release
  • Airplane Control…….Transfer to Pilot (LH) side
  • Circuit Breakers (2F5 and 4A1)…..OPEN
109
Q

Maximum rate of descent for an overweight landing

A

360fpm

110
Q

What are the EXCESSIVE ASYMMETRY OR LOSS OF BRAKING memory items?

A
  • Wheel Brakes……..Release Momentarily
  • Anti-Skid……….OFF
  • Wheel Brakes……Re-Apply, as required
111
Q

What is the allowance for delamination along the edge of the windshield or window

A

2 inches from the edge of the window around the entire periphery

112
Q

What is the allowance for delamination along the corner of the windshield or window

A

4 inches of penetration is allowable in the corners

113
Q

When is a cold weather preflight required

A
  • OAT Less than 5
  • Wing Fuel Temp is 0 or less
  • Atmospheric Icing Conditions Exists
  • RON may have frozen contaminates
114
Q

What is a Holdover Time (HOT)

A

Is an estimate of the time the deicing/anti-icing fluid is effective in preventing the formation of frost, ice, or the accumulation of snow on a treated surface.

115
Q

What is the clean wing concept

A

Aircraft must not take off when frost, ice, or snow is adhering to the wings, control surfaces, engine inlets, and other critical surfaces of the aircraft.

116
Q

What Altitude does RVSM start?

A

FL290

117
Q

MIN FUEL

A

1,550 lb

118
Q

EMER FUEL

A

1,050 lb

119
Q

Max X-Wind TO/LND CRJ 200

A

27 Kts

120
Q

Max X-Wind TO/LND RCC 1 or 2
> 1/8” Standing Water
> 1/8” Slush
Ice

A

10 Kts

121
Q 
TO/LND Wet Ice
Slush Over Ice
Water over Compact snow
Dry Snow over ice
Wet snow over ice
A

Prohibited

CRJ200 Limitations (4 decks)

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