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CRJ200 Limitations > CRJ200 Limitations > Flashcards

CRJ200 Limitations Flashcards

1
Q

max ramp weight

A

53,250

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2
Q

max t/o weight

A

53,000

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3
Q

max landing weight

A

47,000

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4
Q

max zero fuel weight

A

44,000

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5
Q

min flight weight

A

30,000

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6
Q

wingspan

A

69 feet 8 inches

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7
Q

aircraft length

A

87 feet 10 inches

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8
Q

tail height

A

20 feet 8 inches

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9
Q

ALT&TEMP: max ops alt

A

37,000’

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10
Q

ALT&TEMP: max t/o and land

A

10,000’

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11
Q

ALT&TEMP: max tamp and land

A

ISA +35 degrees C

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12
Q

ALT&TEMP: min temp t/o:

min temp in flight:

A
  • 30 degrees C

- 40 degrees C

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13
Q

max tailwind t/o and land

A

10 kts

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14
Q

Vmo

A

335

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15
Q

Mmo

A

0.85

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16
Q

Vlo EXT

A

220

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17
Q

Vlo RET

A

200

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18
Q

Vle

A

220

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19
Q

Vtire

A

182 (GS)

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20
Q

V ADG deploy max

A

250 (wet)

Vmo/Mmo (dry)

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21
Q

Vb

A

280

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22
Q

Mb

A

0.75

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23
Q

V wiper ops max

A

220

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24
Q

Vfo 8

A

200 KTS

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25
Q

Vfo 20

A

200 KTS

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26
Q

Vfe 8

A

215 KTS

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27
Q

Vfe 20

A

215 KTS

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28
Q

Vfe 30

A

185 KTS

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29
Q

Vfe 45

A

170 KTS

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30
Q

SLATS/FLAPS:

max alt:

A

15,000’

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31
Q

SLATS/FLAPS:

enroute alt:

A

prohibited

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32
Q

min spoiler speed *

A

appr speed +20

* approach speed is current maneuvering or straight-in speed

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33
Q

min alt spoilers

A

1,000’ HAT

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34
Q

Spoiler usage

A

spoilers use with flaps 45 prohibited

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35
Q

Min RWY width

A

100’

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36
Q

standing water

A

t/o: 0.50 in (12.7 mm)

landing: 0.75 in (19.1 mm)

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37
Q

slush

A

t/o: 0.50 in (12.7 mm)

landing: 0.88 in (22.4 mm)

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38
Q

wet snow

A

t/o: 1.00 in (25.4 mm)

landing: 1.50 in (38.1 mm)

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39
Q

dry snow

A

t/o: 3.00 in (76.2 mm)

landing: 3.75 in (95.3mm)

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40
Q

APU: min temp start

A

-40 degrees C

41
Q

APU: max ops alt

A

37,000’

42
Q

APU: max start alt

A

30,000’

43
Q

APU: max alt bleed use

A

15,000’

44
Q

APU: max alt engine start

A

13,000’

45
Q

max door open w/ APU not operating

A

300 KIAS

46
Q

ground ops DC only

A

5 mins

47
Q

max continuous DC TRU

A

100 AMPS

48
Q

APU generator

A

to FL370 -30 kVA

49
Q

fire protection: flight time to suitable airport

A

45 mins

50
Q

total pressure refueling

A

14,518 lbs

51
Q

total gravity refueling

A

13,906 lbs

52
Q

max imbalance for t/o

A

800 lbs

53
Q

min for GA per wing *

A

450 lbs

*assumes a max airplane climb attitude pf 10 degrees nose up

54
Q

min bulk fuel temp for t/o

A

-30 degrees C

55
Q

min bulk fuel temp in flight

A

-40 degrees C

56
Q

taxi light

A

must be turned off in excess of 10 mins

57
Q

APU starter duty cycle (1)

A

Max time: 30 secs

Followed by: no more than 3 starts/ start attempts in 1 hour

58
Q

APU starter duty cycle (2)

A

Max time: 30 secs

Followed by: 20 mins off

59
Q

APU starter duty cycle (3)

A

Max time: 30 secs

Followed by: a 2 min delay between cranking attempts

60
Q

APU starter duty cycle (4)

A

Max time: 30 secs

Followed by: 40 mins off

61
Q

Why must be on to start APU?

A

GEN

62
Q

APU start (DC ground power) (1)

A

15 secs

63
Q

APU start (DC ground power) (2)

A

15 secs and 20 mins off

64
Q

APU start (DC ground power) (3)

A

15 secs

65
Q

APU start (DC ground power) (4)

A

15 secs and 40 mins off

66
Q

Cold soak

A

= or less -30 degrees C more than 8 hours

67
Q

Single PACK ops

A

FL250

68
Q

Cabin pressure acquisition module (CPAM)

A

PAX 02 - 14,000 +/- 500

69
Q

T/O w/ a fuel load in excess of 500Ibs in the center tank is not permitted unless:

A
  1. Each main tank is above 4,400Lbs or;
  2. Each wing tank is above 2,000Lbs and;
  3. The allowable zero fuel weight is reduced by the weight of the fuel in the center tank is excess of 500 Lbs and;
  4. The allowable center of gravity (CG) in this configuration is verified to be w/ in the allowable scarf envelope
70
Q

Min reduced thrust

A

3A1- 85%

3B1- 83.5%

71
Q

Engine start ground

A

60sec on- 10 sec off
60 sec on- 10 sec off
60 sec on- 5 mins off
60 sec on- 5mins off

ITT less than 120 to restart

72
Q

Dry motoring (ground)

A

90 sec on- 5 mins off

30 sec on- 5 mins off

73
Q

Max windmilling/ starter-assisted crossovers relight alt

A

FL210

74
Q

Max breakaway n1 for single engine taxi limited to

A

50%

75
Q

Thirst reveres prohibition

A

Oh ground

76
Q

Engine warm up:

Until oil pressure reaches green band

A

Do no exceed idle

77
Q

Engine warm up:

Do no exceed 75% N1 until…

A

2 mins; or all operating indications in green band, which ever is longer

78
Q

Ground ops:

Ground idle N2 spilt

A

Greater than 2%

79
Q

ground ops:

during 2nd engine, APU bleed start

A

operating engine <70%

80
Q

ground ops:

W/ OAT -20 degrees C, thrust levers at idle N2

A

> 57%*

*if N2 is = 57% W/ OAT of -20 degrees C or greater, do not advance thrust levers above idle. contact Mx.

81
Q

Engine Cooldown

engine must not be shut down until:

A

2 mins @ idle/ near idle thrust

Note: taxi time counts towards this limitation

82
Q

Oil Limits:

Mac after cold start

A

engine must remain at idle until oil PSI returns to normal range. must be in normal range W/ in 10 mins

83
Q

Continous Ignition:

A 
Xwinds > 10 kts
thunderstorms
mod turb
mob precip
windshear
contaminated rwy
84
Q

max tailwind

A

10 kts

85
Q

reduced thrust

A

tailwind = or less than 5 kts
not contaminated
airplane allows it
not FOOD

86
Q

Fo max Xwind

A

15 kts

87
Q

speeds above 10,000

A

normal: 290 kts to .70m
long range: 250 kts .70m
high speed: 320 kts to .77m
min: 250 kts to .70m

88
Q

Ice conditions in flight:

A
  • TAT indicates = 10 degrees C & vis moisture

- icing conditions no longer exit in flight if SAT = -40 degrees C

89
Q

cowls on:

A
  • ice conditions or ice ammunicated by ice detection system

- 5 degrees C/ vis moisture and 400’

90
Q

wings on:

A
  • airspeed is less than 230 kts & icing conditions or ice is annunciated by
  • 10 degrees C/ vis moisture/ and vis less than 1 mile
91
Q

autopilot min alts

A

t/o: 600’
precision: 80’
non precision: 400’

92
Q

Autopilot:

must be used above

A

FL200

93
Q

Autopilot:

IAS & DES

A

prohibited on approach

94
Q

autopilot:

approach mode

A

prohibited on VOR

95
Q

Autopilot:

ADC source

A

coupled to active autopilot & coupled to ATC transponder in RVSM

96
Q

(APR):

Automatic Performance Reserve

A
  1. must be used when t/o performance is predicated upon the use of APR
  2. must be selected OFF when an APR INOP caution message is displayed on EICAS
  3. APR OFF performance must be used when an APR INOP caution message is displayed
  4. must be selected OFF for t/o & APR OFF performance must be used when the ambient temp is -18 degrees C & below, & pressure alt is less than 1,000’
97
Q

Pressurization & air conditioning:

single pack ops to…

A

FL250

98
Q

CANNOT use reduced thrust

A 
windshear
tail wind 5kts
behind a heavy
anti skid
anti ice
flaps 8
contaminated rwy

CRJ200 Limitations (1 decks)

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