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CRJ200 (480) > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp WT (LR)

A

53,250 lbs

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2
Q

Max TO WT (LR)

A

53,000 lbs

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3
Q

Max Landing WT (LR)

A

47,000 lbs

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4
Q

Max zero fuel weight (ZFW)

A

44,000 lbs

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5
Q

Max Temp for TO/LD

A

ISA +35 deg C

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6
Q

Min Temp for TO/Dispatch

A

-40 deg C

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7
Q

Max TO/LD Altitude

A

10,000’

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8
Q

Max RWY Slope

A

+2 percent

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9
Q

Max Tailwind

A

10 knots

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10
Q

Max Operating Alt

A

FL410

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11
Q

Max Load in Cargo Compartment

A

3,500 lbs

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12
Q

Must be within __ min of suitable airport, with cargo hold:

A

45 min

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13
Q

Min time between a RTO or LD, and subsequent TO:

A

15 min

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14
Q

Max BTMS temp for TO

A

06

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15
Q

Load Factor Limits (flaps UP)

A

-1.0 to +2.5 G’s

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16
Q

Load Factor Limits (flaps DOWN)

A

0.0 to +2.0 G’s

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17
Q

Min O2 psi for dispatch

A

1410 psi

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18
Q

Vle

A

250

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19
Q

Vlo

A

250

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20
Q

Vlo (ret)

A

200

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21
Q

Vfe (8)

A

215

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22
Q

Vfe (20)

A

215

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23
Q

Vfe (30)

A

185

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24
Q

Vfe (45)

A

170

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25
Q

Max wiper speed

A

220

26
Q

Max tire speed

A

182

27
Q

Turbulence Air Penetration speed

A

280 or .75 Mach (whichever is lower)

28
Q

Max ADG deployment speed

A

Vmo, Mmo

29
Q

Stab/mach trim inop speed

A

250 or .70 Mach

30
Q

Max number of pax on stairs

A

4 (or 1,000lbs)

31
Q

Max time taxi lights on when stationary

A

10 min

32
Q

Min altitude for A/P engagement

A

600’ AGL

33
Q

Min altitude for A/P (precision aprch)

A

80’ AGL or no less than 50’ below the DA

34
Q

Min altitude for A/P (non-precision aprch)

A

400’ AGL or 50’ below MDA (whichever is higher)

35
Q

Max L/R fuel tank qty

A

4,760 lbs

36
Q

Max CENTER fuel tank qty

A

4,998 lbs

37
Q

TO with greater than 500lbs in center of tank is prohibited unless each wing tank is greater than ___lbs

A

4,400 lbs

38
Q

Approved fuel:

A

Jet A

39
Q

Minimum fuel qty for Go-Around

A

450 lbs/side

40
Q

Min FUEL FEED TO temp:

A

+5 deg C

41
Q

Min BULK fuel temp:

A

-40 deg C

42
Q

Max fuel imbalance:

A

800 lbs

43
Q

Cross flows (powered and gravity) must be ___ for TO:

A

OFF

44
Q

Max ITT (APR NOT Op.) ___ (first 2 min), ___ (next 3 min):

A

900 deg C, 884 deg C

45
Q

Max ITT (APR Op.) ___ (first 2 min), ___ (next 3 min):

A

928 deg C, 900 deg C

46
Q

MCT (max continuous thrust) max ITT

A

900 deg C

47
Q

Max N1 percent

A

98.6 percent

48
Q

Min N2 percent to introduce fuel during start

A

20 percent

49
Q

Max ITT during start

A

900 deg C

50
Q

Max N1 percent and N2 percent for normal TO

A

96.2 percent, 98.3 percent

51
Q

Max N1 percent and N2 percent for APR TO

A

98.6 percent, 99.4 percent

52
Q

Engines must be running for a Minimum of ___min prior to TO

A

2 mins

53
Q

Engines must be idle for a Minimum of ___min prior to shutdown

A

2 mins

54
Q

Engine start cycle limits:

A

1 min ON, 10 sec OFF
1 min ON, 10 sec OFF
1 min ON, 5 mins OFF

55
Q

Max ITT for engine start on the ground

A

Less than or equal to 120 deg C

56
Q

Max ITT for in-flight engine start

A

Less than or equal to 90 deg C

57
Q

Max N2 percent to engage Starter

A

Starter not to be used if greater than 55 percent N2

58
Q

Dry motoring limits

A

90 sec ON, 5 min OFF

30 sec ON, 5 min OFF

59
Q

Thrust reverser limitations on TO (3):

A
  1. Ground use only
  2. No Go-Arounds after deployment of TRs
  3. TO with any abnormal TR annunciator is prohibited
60
Q

Reject TO (3 items)

A

Thrust Lever - IDLE
Wheel Brakes - Apply MAX breaking until safe stop
Thrust reversers - Apply MAXIMUM

61
Q

What does APR stand for?

A

Automatic Performance Reserve…hotter/higher numbers when you have APR use

CRJ200 (480) (8 decks)

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