All Flashcards

1
Q

Max ramp weight

A

53,250 lbs

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2
Q

Max TO weigh

A

53,000 lbs

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3
Q

Max landing weight

Max fuel weight

A

47,000 lbs

44,000 lbs

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4
Q

Min flight weight

Max cargo weight

A

30,000lbs

3500 lbs

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5
Q

Max operating Alt

A

41,000ft

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6
Q

Max Turbulent speed

Max Operating speed

A

280 kias .75 M

335 kias. 85 M

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7
Q
Flap Speed
8
20
30
45
A

VFO VFE

8 200 230

20 200 230

30 185 185

45 170 170

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8
Q

vLE max gear extension speed

Max gear retraction speed

Max windshield wipers speed

A

250

200

220

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9
Q

Max dif pressure

Max negative pressure

Max dif for taxi TO and landings

Min cabin ALT in manual mode

A

8.7
-.5
.1

-1500ft

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10
Q

Max ATL for single pack

AP for Visual and NPA (disconnect before__agl)

AP for precision approach

A

25,000ft

400ft

80ft

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11
Q

Fuel quant

Left main

Right main

Center tank

Total

A

Pressure Gravity

Left main 4760 4488

Right main 4760 4488

Center tank 4998 4930

Total. 14,518 13906

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12
Q

Min Eng fuel temp for TO

Max fuel imbalance

Min wing tank fuel for G/A

Break cooling time

Started cranking time

A

Min Eng fuel temp for TO 5degrees🌡

Max fuel imbalance
800lbs

Min wing tank fuel for G/A
450lbs

Break cooling time
15 mins

Started cranking time
1min on, 10 sec off (x2)
1min on, 5 mins off

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13
Q

APU

max operating ALT

max starting ALT

max bleed ALT

Max engine start ALT

A

APU

max operating ALT 37,000

max starting ALT. 30,000

max bleed ALT. 15,000

Max engine start ALT. 13,000

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14
Q

Continuous ignition must be used during…

A

TO and landing on contamined runways

With high cross wind components (15kts 90 degrees

Through moderate and severe icing

Vicinity of TS

Through moderate or heavy Turb

TO after deice/antiICE

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15
Q

Flex power CRJ 200

If reduced thrust used, must not be lower the 85.0%

Reduce thrust must not be used if…..

A

If N1 fan is less then 85.0%

When anti ice system is INOP

When WING AND COWL ANTI ICE system is on for TO

When the RW is contaminated with standing water, slush, snow or ice

Areas of windsher and downdrafts

On wet RWs, Unless “wet performance data” is used

When AeroDate requires you to use max thrust

  • wet RW flex data is only availability when it’s warmer then +10 degrees outside
  • FMS “flex N1” must be greater or equal to AeroDate calculated flex N1 data
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