CRJ 200 Flashcards

1
Q

Max Taxi Ramp Weight

MTRW

A

53,250 lbs

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2
Q

Max Takeoff Weight

MTW

A

53,000 lbs

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3
Q

Max Landing Weight

MLW

A

47,000 lbs

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4
Q

Max Zero Fuel Weight

MZFW

A

44,000 lbs

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5
Q

Minimum Flight Weight

MFW

A

30,000 lbs

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6
Q

Max X-Wind- Takeoff on dry

A

27 kts

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7
Q

Max X-Wind - Landing on dry

A

27 kts

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8
Q

Max X-Wind - Takeoff and landing on wet

A

27 kts

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9
Q

Max X-Wind - Takeoff and landing (RCC3)

A

15 kts

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10
Q

Max X-Wind - Takeoff and landing (RCC2 or 1)

A

15 kts

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11
Q

Max headwind for CAT II approach

A

17 kts

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12
Q

Max X-Wind for CAT II approach

A

15 kts

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13
Q

Max Tail Wind - Takeoff and landing

A

10 kts

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14
Q

Max Tail Wind - SWOA

A

3 kts

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15
Q

Alternate Airport Required if X-Wind exceeds

A

25 kts

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16
Q

Max Operating Altitude (Bombardier)

A

FL410

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17
Q

Max Dispatch Altitude (Company)

A

FL370

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18
Q

Max Altitude Single Pack in Operation

A

FL250

19
Q

Max Altitude dual Pack inop (Ferry only)

A

10,000 ft

20
Q

Vle- Max gear extended and locked

A

250 KIAS

21
Q

Vlo- Max gear operation Extension

A

250 KIAS

22
Q

Vlo- Max gear operation retraction

A

200 KIAS

23
Q

Max Flaps Extended Speed - Flaps 8

A

230 KIAS

24
Q

Max Flaps Extended Speed - Flaps 20

A

230 KIAS

25
Q

Max Flaps Extended Speed - Flaps 30

A

185 KIAS

26
Q

Max Flaps Extended Speed - Flaps 45

A

170 KIAS

27
Q

Approach Minimums Category

A

Category D

28
Q

Max pressure refueling

A

14,518 lbs

29
Q

Left Main Tank Fuel

A

4,760 lbs

30
Q

Right Main Tank Fuel

A

4,760 lbs

31
Q

Center Tank Fuel

A

4,998 lbs

32
Q
Max imbalance (left/right) Main Tanks
For Takeoff
A

800 lbs

33
Q
Max imbalance (left/right) Main Tanks
For Taxi, enroute and landing
A

800 lbs

34
Q

APU Fuel Burn Rate

A

160 lbs/hr

35
Q

Takeoff with a fuel load in excess of 500 lbs in the center tank is not permitted, unless…

A
  1. Each main wing is above 4,400 lbs
  2. Each main wing is above 2,000 lbs and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lbs. and the CG in this configuration is verified to be within the allowable CG envelope.
36
Q

Max Altitude for bleed air extraction

A

FL250

37
Q

Max altitude for APU starting

A

FL250

38
Q

Max APU operating altitude

A

FL250

39
Q

Max runway slope

A

+/- 2%

40
Q

Main Cargo bay (company)

A

3,500 lbs (no forward cargo compartment)

41
Q

Max OAT for Takeoff and Landing

A

ISA + 35C or above

42
Q

Min OAT for Takeoff and Landing

A

-40C or below

43
Q

Cowl Anti-ice on for takeoff (icing conditions)

A

10C or below

44
Q

Wing Anti-ice on for takeoff (icing conditions)

A

5C or below