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Tri-State Training > 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

250KTS

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17
Q

VLO RET

A

200KTS

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18
Q

VLE

A

250KTS

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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 + 17

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33
Q

MIN ALT SPOILER

A

800’ AGL

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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

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50
Q

APU BAT START 1

A

30 SECONDS ON 2 MINUTES OFF

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51
Q

APU BAT START 2

A

30 SECONDS ON 20 MINUTES OFF

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52
Q

APU BAT START 3

A

30 SECONDS ON 2 MINUTES OFF

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53
Q

APU BAT START 4

A

30 SECONDS ON 40 MINUTES OFF

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54
Q

AUTO PILOT MUST BE ENGAGED IN

A

RVSM Airspace

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55
Q

AUTO PILOT IAS MODE

A

PROHIBITED DURING APP

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56
Q

AUTO PILOT DES MODE

A

PROHIBITED DURING APP

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57
Q

AUTO PILOT APPR MODE

A

PROHIBITED DURING VOR APPROACH

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58
Q

MAX TIME DC ONLY

A

5 MINUTES

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59
Q

MAX CONTINUOUS DC TRU

A

100A

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60
Q

TOTAL FUEL (PRESSURE REFUELING)

A

14,518LB

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61
Q

TOTAL FUEL(GRAVITY REFUELING)

A

13,906LB

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62
Q

MAX FUEL IMBALANCE FOR T/O

A

800 LB

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63
Q

MIN FUEL FOR GO-AROUND PER WING

A

459 LB

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64
Q

MIN BULK FUEL TEMP FOR T/O

A

-30C

65
Q

MIN BULK FUEL TEMP IN FLIGHT

A

-40C

66
Q

MIN REDUCED THRUST 3A1

A

85%

67
Q

MIN REDUCED THRUST 3B1

A

83.5%

68
Q

ENG START ON GND 1

A

60 SECONDS ON 10 SECONDS OFF

69
Q

ENG START ON GND 2

A

60 SECONDS ON 10 SECONDS OFF

70
Q

ENG START ON GND 3

A

60 SECONDS ON 5 MINUTES OFF

71
Q

ENG START ON GND 4

A

60 SECONDS ON 5 MINUTES OFF

72
Q

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

A

70% N2

73
Q

DRY MOTORING 1

A

90 SECONDS ON 5 MINUTES OFF

74
Q

DRY MOTORING 2

A

30 SECONDS ON 5 MINUTES OFF

75
Q

MAX WINDMILLING/STARTER ASSISTED CROSS BLEED RELIGHT ALT

A

FL210

76
Q

DO NOT EXCEED 75% N1 UNTIL:

A

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

77
Q

MAX GROUND IDLE SPLIT N2

A

LESS THAN OR EQUAL TO 2%

78
Q

WITH OAT -20C THRST LEVERS AT IDLE N2

A

GREATER THAN 57%

79
Q

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

A

DO NOT ADVANCE THRUST LEVER, CONTACT MX

80
Q

ENGINE COOL DOWN

A

2 MINUTES AT IDLE/NEAR IDLE THRUST

81
Q

THRUST REVERSER USE DURING TAXI

A

PROHIBITED

82
Q

OIL PRESSURE: STEADY STATE IDLE

A

25 psi minimum

83
Q

SINGLE PACK OPS

A

FL250

84
Q

CPAM PAX O2

A

14,000’ +/- 500’

85
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

86
Q

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

A

THE DEPLOY AND STOW CYCLES ARE LESS THAN 5 SECONDS

87
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

88
Q

NO LIGHT OFF “QRC MEMORY ITEM”

A

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

89
Q

At what crosswind component is continuous ignition required for takeoff

A

Greater than 10 kts

90
Q

When is reduced thrust prohibited?

A
  • Wings/Cowls anti-icing bleeds are in use
  • Contaminated RWY
  • Warnings of windshear or downdrafts are forecast
91
Q

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

A

3000’ above field elevation

92
Q

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

A
  • Engine Failures
  • Fire
  • Loss of Directional Control
  • Windshear
  • Unable to Fly
93
Q

The autopilot must be engaged above

A

RVSM Airspace - FL290

94
Q

The autopilot can be engaged at

A

600’

95
Q

What is the climb speed schedule below 10,000

A

250

96
Q

What is the climb speed schedule above 10,000

A

290/.74

97
Q

What bank deviation requires a PM call out

A

In excess of 30 Degrees

98
Q

What Speed deviation requires a PM call out

A

+10/-5 KIAS or .02M

99
Q

What heading from bugged or course deflection require PM call out

A

+/- 10 degrees

Course from established 1/4 deflection

100
Q

What are the PM callouts

A 
SPEED
BANK
HEADING
COURSE
PITCH
VERTICAL SPEED
101
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

102
Q

Double Engine Failure Memory Item

A

IGNITION CONTINOUS
NO LESS THAN 240KIAS

103
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

104
Q

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

A

500ft HAT

105
Q

Arming the APPR too early may result in a?

A

False localizer capture

106
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
107
Q

Maximum rate of descent for an overweight landing

A

360fpm

108
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
109
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

110
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

111
Q

When is a cold weather preflight required

A
  • OAT Less than 5
  • Wing Fuel Temp is 0 or less
  • Atmospheric conditions have been conducive to frost formation
112
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.

113
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.

114
Q

What Altitude does RVSM start?

A

FL290

115
Q

MIN FUEL

A

1,550 lb

116
Q

EMER FUEL

A

1,050 lb

117
Q

Max X-Wind TO/LND CRJ 200

A

27 Kts

118
Q

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

A

10 Kts

119
Q 
TO/LND Wet Ice
Slush Over Ice
Water over Compact snow
Dry Snow over ice
Wet snow over ice
A

Prohibited

120
Q

Max Number of PAX on Door

A

4 PAX or 1,000 pounds

121
Q

Flaps AD for Landing

A

Flaps should not be extended out of 0° unless:
* Prec. app vis. is above the vis. associated with the landing min and expected to remain so.
* Non. prec. same as prec. app but ceilings must also remain above requirments
* An emergency requires landing at nearest airport
* Fuel remaining is sufficient to conduct app, go missed, divert with flaps extended in landing config., conduct app, and land with 1,000lbs of fuel remianing.

122
Q

Min. Oil Pressure Idle

A

Min. 25psi

123
Q

Min. Oil Pressure for Takeoff

A

Min. 45psi

124
Q

Max Oil Continious Temp.

A

+155° C

125
Q

Max. Oil Permissable Temp.

A

+163° C

126
Q

APU Max EGT

A

743° C

127
Q

Never Go Below What Mach Speed in a Climb

A

.70M

128
Q

Holding Speeds

A

200 KIAS - Below 14,000
225 KIAS - 14,001 to FL250
250 KIAS - Above FL250

129
Q

RVSM Required Equipment

A
  • Two independent altitude measuring systems
  • An altitude alerting system
  • An automatic altitude control system
  • A seconday survellance radar transponder with altitude reporting system that can be connected to the altitude measuring system in use for altitude keeping
130
Q

Max Rotation Rate

A

3° per second

131
Q

Kinds of Operations

A

IFR, VFR, Known Icing

132
Q

OIL PRESSURE: TAKEOFF THRUST

A

45 psi minimum

133
Q

OIL PRESSURE: MAXIMUM CONTINUOUS

A

115 psi maximum

134
Q

OIL PRESSURE: MAXIMUM TRANSIENT AFTER COLD START

A

156 psi maximum
(130 psi at idle. 10 min max)

135
Q

COWL A/I MUST BE ON? (GROUND)

A

OAT 10° C or below AND =
* Visible moisture is present
* When operating on any contaminated runway
* Anytime the wing A/I system is on

136
Q

WITH COWL A/I ON, CAUTION MESSAGE SHOULD DISAPPEAR BY

A

78% N2 or must call maintenance

137
Q

COWL A/I MUST BE ON? (FLIGHT)

A
  • In icing conditions
  • When “ICE” is annunciated by the ice detection system
138
Q

WING A/I ON WHEN (GROUND)

A
  • During final taxi prior to takeoff if the OAT is 5° C or less (Unless type II, III, or IV have been applied)
  • On for Takeoff when OAT is 5° C or less and
  • Visible moisture in any form below 400’ AGL
  • contaminated runway
  • Presence of any precipitation
139
Q

WING A/I ON WHEN (FLIGHT)

A
  • “ICE” is annuciated by the ice detection system
  • In icing conditions and airspeed less than 230 KIAS
140
Q

WHEN DO YOU TURN ON WING A/I IF TYPE II, III, OR IV HAVE BEEN APPLIED

A

JUST BEFORE TAKEOFF THRUST IS APPLIED

141
Q

CRITICAL AIRCRAFT SURFACES

A
  • Wings
  • Upper fuselage
  • Horizontal stabilizers
  • Vertical stabilizers
  • Control surfaces
  • Engine inlets
142
Q

MAX RUNWAY SLOPE FOR T/O

A
  • 2% uphill
  • -2% downhill
143
Q

MINIMUM FLIGHT CREW

A

One pilot and one copilot

144
Q

MAXIMUM CABIN DIFFERENTIAL PRESSURE

A

8.7 psi

145
Q

MAX NEGATIVE PRESSURE DIFFERNTIAL

A

-0.5 psi

146
Q

MAX DIFFERENTIAL PRESSURE DURING GROUND MANEUVERING

A

0.1 psi

147
Q

MAX DIFFERENTIAL PRESSURE AT TOUCHDOWN

A

1.0 psi

148
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT ON NON-PREC APP

A

400’ AGL but no lower than 50’ below the DDA, whichever is higher

149
Q

MIN ALT FOR AUTOPILOT ENGAGEMENT ON PREC APP

A

50’ below the DA or 80’, whichever is higher

150
Q

CIRCUT BREAKER RESET LIMITATION

A

Unless in the AFM, no reset unless safety of flight

151
Q

TAXI LIGHT USE LIMIT

A

Must be off if aircraft is stationary for more than 10 min

152
Q

COLD SOAKED AIRCRAFT DEFINITION

A

Ambient temperature of -30° C or less for more than 8 hours

153
Q

MIN FUEL TEMP FOR TAKEOFF

A

5° C

154
Q

MAX OIL CONSUPTION PER HOUR

A

6.4 ounces per hour (0.05 gallons)

155
Q

MAX HOURS WITHOUT FUEL SURVICING

A

16 Hours

156
Q

MAX OIL REFILL ALLOWED

A

2 qts without dry motoring

157
Q

MAX TURBULENT PENETRATION SPEED

A

280 kias / 0.75M

158
Q

MAX LOAD FACTOR

A
  • Flaps up: -1.0G to 2.5G
  • Flaps down: 0.0G to 2.0G

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