Limitations Flashcards

1
Q

APU Minimum Start Temperature

A

-40 C

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2
Q

APU Max Ops Altitude

A

37,000’

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3
Q

Max APU start altitude

A

30,000’

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4
Q

Max APU bleed use altitude

A

15,000’

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5
Q

Max APU assisted engine start altitude

A

13,000’

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6
Q

Max APU Door Open Speed

A

300 KIAS

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7
Q

APU start duty cycle

A

30 seconds on - recommended 2 minutes off
30 seconds on - 20 minutes off
30 seconds on - recommended 2 minutes off
30 seconds on - 40 minutes off

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8
Q

Max DC only ground ops Time

A

5 minutes

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9
Q

Max continuous DC TRU

A

100A

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10
Q

APU Generator output

A

To FL370 - 30kVA

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11
Q

Cargo FIREX time to suitable airport

A

45 minutes

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12
Q

Total Fuel (pressure refueling)

A

14,518lbs

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13
Q

Total Fuel (gravity refueling)

A

13,906 lbs

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14
Q

Max Fuel Imbalance for Takeoff

A

800 lbs

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15
Q

Minimum fuel for Go Around per wing

A

450 lbs

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16
Q

Minimum bulk fuel temperature (for Takeoff)

A

-30 C

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17
Q

Minimum Bulk Fuel Temperature (Flight)

A

-40 C

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18
Q

Takeoff with fuel in excess of 500 lbs in center tank is prohibited unless…

A
  • each main tank is above 4400 lbs, or
  • each wing tank is above 2000 lbs, and
  • the allowable ZFW is reduced by the weight of the center fuel in excess of 500 lbs, and
  • CG is within limits
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19
Q

Powered cross flow must be _____ for takeoff

A

Off

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20
Q

Max Ramp Weight

A

53,250 lbs

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21
Q

Max T/O Weight

A

53,000 lbs

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22
Q

Max Land Weight

A

47,000 lbs

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23
Q

Max Zero Fuel Weight

A

44,000 lbs

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24
Q

Minimum Flight Weight

A

30,000 lbs

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25
Q

Wing span

A

69’8”

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26
Q

Aircraft Length

A

87’10”

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27
Q

Tail Height

A

20’8”

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28
Q

When must APR be OFF for takeoff

A

When ambient temperature is less than -18 C, and pressure altitude less than 1000 FT (3A1 engines only)

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29
Q

Minimum Reduced Thrust

A

3A1 - 85%

3B1 - 83.5%

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30
Q

Engine Start (ground) starter duty cycle

A

60 seconds on - 10 seconds off
60 seconds on - 10 seconds off
60 seconds on - 5 minutes off
60 seconds on - 5 minutes off

ITT MUST be 120 C or less for all ground starts before introducing fuel

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31
Q

When both engines are started using APU, operating engines thrust must not exceed _____% N2.

A

70

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32
Q

Dry Motoring (ground)

A

90 seconds on - 5 minutes off

30 seconds on - 5 minutes off

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33
Q

Max windmilling/starter assisted cross bleed relight altitude

A

FL210

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34
Q

Do not exceed ________ until oil pressure reaches the _______ band.

A

Idle, green

35
Q

Do not exceed _______% N1 until…

A

75%

2 minutes, or

All operating indications in green band

Whichever is longer

36
Q

Ground idle N2 split

A

Less than or equal to 2%

37
Q

With OAT greater than or equal to -20 C, thrust levers at idle, N2 must be_______

A

Greater than 57%

38
Q

Engines must not be shut down until

A

2 minutes at idle/near idle thrust

39
Q

Max Single Pack operation altitude

A

FL250

40
Q

CPAM activates pax O2 at

A

14,000 +/- 500 ft

41
Q

Use of EMER DEPRESS is prohibited above

A

15,000 ft

42
Q

Limit climb to less than _______ FPM above ________

A

1,500 FPM, FL300

43
Q

Minimum Runway Width

A

100 FT

44
Q

Maximum Standing Water Depth

A

Takeoff: 0.50 in.
Landing: 0.75 in.

45
Q

Maximum Slush Depths

A

Takeoff: 0.50 in.
Landing: 0.88 in.

46
Q

Maximum Wet Snow Depth

A

Takeoff: 1.00”
Landing: 1.50”

47
Q

Maximum dry snow Depth

A

Takeoff: 3.00”
Landing: 3.75”

48
Q

Can you dispatch with only one reverser if the runway has ice on it?

A

No!

49
Q

Taxi lights must be switched off whenever the airplane is stationary in excess of ________ minutes

A

10

50
Q

Minimum Runway Width

A

100 FT

51
Q

Maximum Standing Water Depth

A

Takeoff: 0.50 in.
Landing: 0.75 in.

52
Q

Maximum Slush Depths

A

Takeoff: 0.50 in.
Landing: 0.88 in.

53
Q

Maximum Wet Snow Depth

A

Takeoff: 1.00”
Landing: 1.50”

54
Q

Maximum dry snow Depth

A

Takeoff: 3.00”
Landing: 3.75”

55
Q

Can you dispatch with only one reverser if the runway has ice on it?

A

No!

56
Q

Taxi lights must be switched off whenever the airplane is stationary in excess of ________ minutes

A

10

57
Q

When must continuous ignition be on?

A

• Takeoffs and landings on contaminated runways
• takeoffs with crosswinds greater than 10 knots
• flight through moderate or heavy intensity rain
Flight through moderate or heavy turbulence
• flight in the vicinity of thunderstorms

58
Q

Maximum Operating Altitude

A

37,000 FT

59
Q

Max takeoff and landing altitude

A

10,000 FT

60
Q

Max Temp for Takeoff and Landing

A

ISA +35 C

61
Q

Minimum Takeoff Temp

A

-40 C

62
Q

Max Tailwind For Landing

A

10 KTS

63
Q

Vmo

A

335 KTS

64
Q

Mmo

A

0.85

65
Q

Vlo EXT

A

220 KIAS

66
Q

Vlo RET

A

200 KIAS

67
Q

Vle

A

220 KIAS

68
Q

Vtire

A

182 KGS

69
Q

Vadg Deploy

A

250 Wet

Vmo/Mmo Dry

70
Q

Vb

A

280 KIAS

71
Q

Mb

A

0.75

72
Q

Vwiper ops max

A

220 KIAS

73
Q

Vfo 8

A

200 KIAS

74
Q

Vfo 20

A

200 KIAS

75
Q

Vfe 8

A

215 KIAS

76
Q

Vfe 20

A

215 KIAS

77
Q

Vfe 30

A

185 KIAS

78
Q

Vfe 45

A

170 KIAS

79
Q

Max flaps altitude

A

15,000 FT

80
Q

Enroute flap operation

A

Prohibited

81
Q

Minimum spoiler speed

A

Appr Speed + 20 (SW)

82
Q

Minimum Spoiler Altitude

A

1,000 FT HAT

83
Q

Spoiler usage with flaps 45 is _______________

A

Prohibited