CRJ Systems Flashcards

0
Q

Max landing weight

A

47,000 lbs

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1
Q

Max takeoff weight

A

53,000lbs

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2
Q

Max zero fuel weight

A

44,000 lbs

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3
Q

Max temp for takeoff/landing

A

ISA+35c

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4
Q

Max N1% and N2% for APR TO

A
  1. 6 N1

99. 4 N2

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5
Q

Min temp for takeoff/ dispatch

A

-40c

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6
Q

Max takeoff/landing altitude

A

10,000’

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7
Q

Maximum runway slope

A

+2%

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8
Q

Max tailwind

A

10kts

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9
Q

Dry motoring limits

A

90sec on, 5min off

30sec on, 5 min off

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10
Q

Turbulent air penetration speed

A

280 or .75M (whichever is lower)

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11
Q

Engine start limits

A

1min on, 10sec off
1min on, 10sec off
1min on, 5 min off

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12
Q

Maximum N1%

A

98.6%

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13
Q
Maximum ITT (APR op)
\_\_\_\_\_\_(first 2 min), \_\_\_\_\_\_\_(next 3 min)
A

928c

900c

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14
Q
Maximum ITT (APR not op)
\_\_\_\_\_\_(first 2 min), \_\_\_\_\_\_\_(next 3 min)
A

900c

884c

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15
Q

Takeoff with >500lbs is prohibited unless each wing tank >_____lbs

A

4, 400lbs

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16
Q

Minimum altitude for Autopilot (non precision)

A

400’agl or 50’below MDA, whichever is higher

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17
Q

Maximum time for taxi lights on when stationary

A

10min

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18
Q

Stab/Mach trim inop speed

A

250 or .70M

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19
Q

Load factor limits (flaps up)

A

-1.0 to +2.5 G

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20
Q

Thrust reverser limitations on takeoff (3)

A

Ground use only
No go around after deployment of thrust reverser
Takeoff with any abnormal thrust reverse annunciator is prohibited

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21
Q

Continuous ignition must be used (5 items)

A
Takeoff/LDG on contaminated runway
Takeoff with Xwind >10kts
Moderate or greater rain
Moderate or greater turbulence
Flight in vicinity of thunderstorms
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22
Q

Maximum N2% to engage starter

A

Starter must not be used if >55%N2

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23
Q

Maximum ITT for in flight engine start

A

> /= 90c

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24
Q

Maximum ITT for engine start on the ground

A

</= 120c

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25
Q

Maximum ramp weight

A

53,250lbs

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26
Q

Maximum operating altitude

A

FL410

27
Q

Maximum load in cargo compartment

A

3,500lbs

28
Q

Must be within _________ min of suitable airport with cargo hold

A

45 minutes

29
Q

Minimum time between an RTO or landing subsequent takeoff

A

15 minutes

30
Q

Maximum BTMS temp for takeoff

A

06

31
Q

Load factor limits flaps down

A

0.0 to 2.0 G

32
Q

Minimum oxygen for dispatch

A

1410 psi

33
Q

Vle

A

250kts

34
Q

Vlo

A

250kts

35
Q

Vlo(retract)

A

200kts

36
Q

Vfe(45)

A

170kts

37
Q

Vfe(30)

A

185kts

38
Q

Vfe(20)

A

215kts

39
Q

Vfe(8)

A

215kts

40
Q

Max wiper speed

A

220kts

41
Q

Max tire speed

A

182kts

42
Q

Maximum ADG deployment speed

A

Vmo, Mmo

43
Q

Maximum number of passengers on stairs

A

4

44
Q

Minimum altitude for autopilot engagement

A

600’ agl

45
Q

Minimum altitude for autopilot (precision approach)

A

80’ or not less than 50’ below DA

46
Q

Maximum L/R fuel tank quantity

A

4760lbs

47
Q

Maximum center tank quantity

A

4,998 lbs

48
Q

Approved fuel

A

Jet A

49
Q

Minimum fuel for go around

A

450 lbs per side

50
Q

Minimum fuel feed takeoff temp

A

+5c

51
Q

Minimum bulk fuel temp

A

-40c

52
Q

Maximum fuel imbalance

A

800lbs

53
Q

Cross flows (powered and gravity) must be ________ for takeoff

A

Off

54
Q

MCT max ITT

A

900c

55
Q

Minimum N2% to introduce fuel during start

A

20%

56
Q

Maximum ITT during start

A

900c

57
Q

Engines must be running for a minimum of _______ prior to shutdown

A

2 minutes

58
Q

Engines must be running for a minimum of ________ prior to takeoff

A

2 minutes

59
Q

Maximum N1% and N2% for normal takeoff

A
  1. 2% N1

98. 3% N2

60
Q

Max altitude for single pack operations

A

25,000

61
Q

Max altitude to start engine with apu

A

13,000’

62
Q

Max altitude for APU bleed air extraction to supply air conditioning packs

A

15,000 ft

63
Q

Max altitude for APU to be running

A

37000

64
Q

Max altitude to start APU

A

30000