CRJ 200 Limitations. Flashcards

0
Q

Maximum ramp weight

A

53,250 lbs

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1
Q

Kinds of operations

A

Transport category
Day and Night
VFR and IFR
Flight into icing conditions

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2
Q

Maximum take off weight

A

53,000 lbs

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3
Q

Maximum landing weight

A

47,000 lbs

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4
Q

Maximum zero fuel weight

A

44,000 lbs

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5
Q

Maximum take off and landing pressure altitude

A

10,000’

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6
Q

Maximum operating altitude

A

41,000’

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7
Q

Max take off and landing air temp

A

iSA +35

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8
Q

Minimum take off and landing air temp

A

-40c / -40f

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9
Q

cowl anti ice -Ground

A

On: OAT <= +10 & Visible moisture. Visibility <=1sm

On: Contaminated surfaces

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10
Q

Cowl anti-ice in flight

A

On: TAT <= 10c and visible moisture except SAT <=-40c

On: when ICE annunciation illuminates by the ice detection system

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11
Q

Wing anti-ice ground

A

On: OAT <=5c and visible moisture. Visibility < 1sm

Contaminated runway

When type II or IV fluid has been applied-just prior to applying take off thrust

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12
Q

Wing anti-ice. Flight

A

On: ice annunciation illuminates by the ice detection system

When in icing conditions and airspeed is <=230 KIAS

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13
Q

Super cooled large droplets (SLD) icing

A

Continued flight operations prohibited, identified by side window icing.

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14
Q

It asks off permitted with frost

A

Upper surface of fuselage (see surface features)

Underside of cold soaked wing (1/8 in max)

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15
Q

Runway slope

A

+- 2%

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16
Q

Max tailwind component

A

10 Kts

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17
Q

Minimum flight crew

A

1 pilot, 1 co-pilot

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18
Q

Cargo limits

A

Flight within 60 minutes if cargo is in cargo compartment

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19
Q

Ozone limits.

A

25 ppm, sea level equivalent at any time above FL320

.01 ppm equivalent time weighed average during any 3 hour interval above FL270

Sea level equivalent = 25c / 760 mm Mercury

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20
Q

Engines

A

General Electric CF34-3B1

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21
Q

N1 % RPM

A

98.6, O-98.5

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22
Q

N2 % RPM.

A

99.3, 0-99.2

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23
Q

Oil Temp. C

A

163 max
150-162 caution
-40 - 149 Normal

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24
Q

Oil Pressure

A

0-25 Red
115-156 Caution
26-115 normal

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25
Q

Airplane Cold Soak

A

> 8 hours at <(-30c, -22f)

Before start, motor engines for 60 sec and verify fan rotation

Actuate Thrust Reversers until deploy and stow cycles are less than 5 seconds

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26
Q

Use of continuous ignition

A

Take off and landing on contaminated runway

Rain > moderate

Turbulence > moderate

In the vicinity of thunderstorms

Take off with high crosswinds

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27
Q

Starter limitations

A

Starts 1&2, 60 seconds on, followed by 10 seconds off

Starts 3 +, 60 seconds on, followed by 5 minutes off

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28
Q

ITT Starting limits

A

At initiation of thrust lever movement from shut off to idle:

ITT must be 120c or less for ground starts

ITT must be less than 90 c for air starts

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29
Q

N2 RPM limits for starts

A

N2 must be less than 55%

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30
Q

Starter limits for motoring engine

A

Start 1: 90 seconds on, 5 minutes off

Starts 2+: 30 seconds on, 5 minutes off

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31
Q

Fuel capacity

A
Total = 14,518
Wings = 9520
Center = 4998
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32
Q

Minimum go-around fuel

A

450 lbs per wing, 10 nose up pitch max

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33
Q

Max fuel imbalance in-flight

A

800 lbs

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34
Q

APU type

A

Garrett GTPC-36-150RJ

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35
Q

APU max RPM

A

107%

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36
Q

APU maximum Temp

A

743c-974c

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37
Q

APU Minimum Start Temp

A

-40c / -40 f

38
Q

APU maximum generator load

A

30 kVA

39
Q

APU altitude limits

A

Max Alt= FL370
Starting=FL300
Pneumatics=15,000’

40
Q

Vmo/Mmo

A

335kias / 0.85m

41
Q

Vt (turbulence)

A

280kias / 0.75m

42
Q

Max ADG operating speed

A

Dry ADG type, no limit

43
Q

Max windshield wiper

A

220 KIAS

44
Q

Maximum RVSM airspeed

A

O.83m

45
Q

Minimum airspeed

A

Vss (stick shaker)

46
Q

Vfe flaps 8

A

200 KIAS

47
Q

Vfe flaps 20

A

200 KIAS

48
Q

Vfe flaps 30

A

185 KIAS

49
Q

Vfe flaps 45

A

170 KIAS

50
Q

Flaps use prohibited

A

Enroute

.flights with flaps extended at altitudes above 15,000’

51
Q

Vlo / Vle

A

250 KIAS

52
Q

Vlo ret

A

200 KIAS

53
Q

Max tire speed

A

182 Kts ground speed

54
Q

Max relief differential

A

+8.7 psi

55
Q

Min relief differential

A

-.5 psi

56
Q

Max taxi / takeoff / landing differential

A

+.1 psi

57
Q

Autopilot minimum use height

A

Take off = 600’
NPA= 400’
PA=80’

58
Q

Max generator load 0-FL350

A

Engine / APU generator = 30kVA

59
Q

Max generator load 35,001’-37,000’

A

Engine=25kVA

APU=30kVA

60
Q

Max generator load 37,001’ and above

A

Engine only = 25kVA

61
Q

Max load, each TRU in flight

A

100 amps

62
Q

Max ground time, DC power only

A

5 minutes

63
Q

Use of spoilers prohibited

A

< 300’ agl

Less than approach speed +17 Kts

64
Q

Stall protection system switches

A

On for all phases of flight

65
Q

Fuel Balance for take off

A

Center tank > 500 lbs and wing tanks < 4400 lbs
Or
Minimum wing tank cannot be less than 2200 lbs and
ZFW reduced by the amount of center fuel tank fuel over 500 lb limit
And
CG compliance

66
Q

Max fuel imbalance

A

Less than 800 lbs

67
Q

Min engine fuel temp

A

5c

68
Q

Min bulk fuel temp for takeoff

A

Jet a <=-30c

Jet A1 <=-37c

69
Q

Powered Xfeed and gravity Xfeed for takeoff

A

Off

70
Q

Starter assist re-light. Bleed >60 psi

SFC to 15,000’

A

Sfc to 15,000’:
speed: Vref to Vmo
N2: 0-55%

71
Q

Starter assist relight Bleed >60psi

15,000’ to 21,000’

A

Speed: 180 KIAS to Vmo
N2: 0-55%

72
Q

Windmilling relight SFC to 15,000’

A

Speed: 300 KIAS to Vmo / Mmo
N2: 9-55%

73
Q

Windmilling relight 15,000’ to 21,000’

A

Speed: 300 KIAS to Vmo / Mmo
N2: 12 to 55%

74
Q

Minimum flight weight

A

30,000 lbs

75
Q

Minimum BOW

A

25,480 lbs

76
Q

Minimum pavement for 180 turn

A

75’

77
Q

Dimensions

A

H=21’
L= 88’
W= 69’8”

78
Q

What doors are not on EICAS

A

Crew Hatch and Aft Equipment Hatch

79
Q

Max weight on door

A

1000 lbs (4 pax)

80
Q

Door EICAS colors

A

Cabin. Red, open. Amber, handle not latched, Green, closed

All other Green closed, Amber open

81
Q

Engines and thrust

A

GE CF34 3B1

8729 normal
9220 APR

82
Q

APU functions

A

Primary is electric

Secondary is pneumatic

83
Q

Green line on Airspeed Tape

A

1.26 Vs

84
Q

Alignment times for AHRS

A

70 seconds Mag mode

10 minutes DG mode

85
Q

Deck utter criteria

A

Pitch 30 / -20

Roll more than 65

86
Q

CRT and AVIONICS Cooling

A

Fan 1 flight
Fan 2 ground

Vented overboard with door open
Underfloor door closed

87
Q

Function of Data Concentrator Unit

A

To collect data from A/C systems, processes and information and relays it to proper component display

88
Q

What audio warnings are not disabled with DCU Disable switch

A

EGPWS AND TCAS

89
Q

What happens if ED 1 fails

A

Automatically switches to ED2

90
Q

What items can be boxed on EICAS

A

White and Amber can be boxed

Red and green cannot

91
Q

What does step button on EICAS Control do

A

Allows a sequential step thru all synoptic pages

92
Q

How does info get to FDR

A

EICAS sends alt, as, position, hug, acceleration and radio communication to the FDR

93
Q

Turning on the beacon or strobes or WOW senses airborne

A

What activates the FDR