CRJ 700 Limitations Flashcards

1
Q

Max Ramp Weight

A

75,250lbs

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2
Q

Max Takeoff Weight

A

75,000lbs

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3
Q

Max Takeoff Weight Delta & Alaska

A

74,999lbs

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4
Q

Max Landing Weight

A

67,000lbs

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5
Q

Max Zero Fuel Weight

A

62,300lbs

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6
Q

Min Flight Weight

A

42,000lbs

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7
Q

Max Aft Cargo

A

3,740lbs

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8
Q

Max Aft Cargo for WiFi equipped plane

A

3,650lbs

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9
Q

Max Aft Cargo Alaska

A

4,375lbs

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10
Q

Max Forward Cargo

A

1,000lbs

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11
Q

Flight time to suitable airport

A

60 min

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12
Q

Minimum runway length

A

100ft

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13
Q

Max operation altitude

A

41,000ft

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14
Q

Max operating altitude SkyWest

A

39,000ft

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15
Q

Max altitude takeoff and landing

A

9,600ft

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16
Q

Max temp takeoff and landing

A

ISA +35c

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17
Q

Min temp for takeoff

A

-40c

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18
Q

Runway slope

A

+/- 2%

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19
Q

Max Tailwind

A

10kts

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20
Q

Vmo

A

335 KIAS

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21
Q

Mmo

A

.85 (.83 RVSM)

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22
Q

Flaps 1

A

230 KIAS

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23
Q

Vfe 8

A

230 KIAS

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24
Q

Vfe 20

A

230 KIAS

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25
Q

Vfe 30

A

185 KIAS

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26
Q

Vfe 45

A

170 KIAS

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27
Q

Vlo Ext

A

220 KIAS

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28
Q

Vlo Ret

A

200 KIAS

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29
Q

Vle

A

220 KIAS

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30
Q

Vtire

A

182 K GS

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31
Q

Vadg Deploy Max (wet)

A

Vmo/ Mmo

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32
Q

Vadg Deploy Max (dry)

A

Vmo/ Mmo

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33
Q

Vb

A

280 KIAS

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34
Q

Mb

A

.75 M

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35
Q

Vwiper ops

A

250 KIAS

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36
Q

Brakes normal psi

A

1800-3200 psi

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37
Q

Anti skid operation

A

> 35 kts or WOW +5 Sec

38
Q

Anti skid inop below

A

10 KTS

39
Q

Flaps/ Slats max altitude

A

15,000ft

40
Q

Flaps/ Slats enroute altitude operation

A

Prohibited

41
Q

Min Spoiler Speed

A

Appr speed +10

42
Q

Min Spolier operation altitude

A

300ft AGL

43
Q

ITT max APR not operating/ normal takeoff

A

For 5 min 920c

44
Q

ITT max APR operating

A

For 5 min 960c

45
Q

ITT max continuous thrust

A

927c

46
Q

ITT max start

A

815c

47
Q

N1 Idle

A

20-25%

48
Q

N1 max continuous

A

99.5%

49
Q

N1 normal takeoff

A

97.9%

50
Q

N1 APR max power

A

99.5%

51
Q

N2 start

A

20%

52
Q

N2 idle

A

55-65%

53
Q

N2 max takeoff (APR op) APR max power

A

99.4%

54
Q

N2 Max Continuous

A

97.9%

55
Q

N2 normal takeoff

A

98.3%

56
Q

Engine Start ground

A
90 sec On……………10 sec Off
90 sec On……………10 sec Off
90 sec On…………….5 min Off
90 sec On…………….5 min Off
90 sec On…………….5 min Off
57
Q

Dry Motoring ground

A
90 sec On………….5 min Off
30 sec On………….5 min Off
30 sec On………….5 min Off
30 sec On………….5 min Off
30 sec On………….5 min Off
58
Q

Fuel L main pressure fueling

A

7,492lbs

59
Q

Fuel R main pressure fueling

A

7,492lbs

60
Q

Fuel center pressure fueling

A

4,610lbs

61
Q

Pressure fueling total

A

19,594lbs

62
Q

Fuel L main gravity fueling

A

7,290lbs

63
Q

Fuel R main gravity fueling

A

7,290lbs

64
Q

Center gravity fueling

A

N/A

65
Q

Gravity fueling total

A

14,580lbs

66
Q

Fuel max imbalance

A

800lbs

67
Q

Fuel max imbalance for takeoff

A

300lbs

68
Q

Fuel min for go around per wing

A

600lbs

69
Q

Fuel min temp takeoff

A

+5c

70
Q

Main gen

A

to 41,000ft - 40KVA

71
Q

APU gen

A

to 41,000ft - 40KVA

72
Q

Max contiuous DC TRU

A

120 A

73
Q

Ground ops DC only

A

5 min

74
Q

AP use on Takeoff

A

600ft AGL

75
Q

AP non precision visual approach

A

400ft AGL

76
Q

AP Precision approach <4 degrees

A

120ft AGL

77
Q

AP precision approach <3.5 degrees

A

80ft AGL

78
Q

APU max RPM

A

107%

79
Q

APU max EGT ground

A

789c

80
Q

APU max EGT flight

A

807c

81
Q

APU max EGT

A

1038c

82
Q

APU min start temp

A

-40c

83
Q

APU max operation altitude

A

41,000ft

84
Q

APU max start altitude

A

37,000ft

85
Q

APU max bleed use altitude

A

25,000ft

86
Q

APU max engine start altitude

A

21,000ft

87
Q

APU max gen load

A

40 KVA

88
Q

APU max door open with apu not operating

A

220 KIAS

89
Q

Max altitude single pack

A

FL310

90
Q

CPAM PAX O2 (CPA)

A

less than or equal to 14,000ft

91
Q

Emergency depress (CPA)

A

14,500 +/- 500ft