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Global 5000/5500/6000 > Black Limitations > Flashcards

Black Limitations Flashcards

1
Q

Minimum Inside Main Gear Turning Radius.

A

8 ft

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2
Q

Minimum Outside Main Gear Turning Radius.

A

21 ft

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3
Q

Minimum Nose Gear Turning Radius.

A

46 ft

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4
Q

Minimum Outside Wingtip Turning Radius.

A

129 ft

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5
Q

45-Minute IFR Reserve Fuel Quantity

A

2500 lbs

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6
Q

Hot Spare Fuel Quantity

A

8500 lbs

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7
Q

Emergency Fuel Quantity

A

1500 lbs

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8
Q

Parking in Inclement Weather Fuel

A

15,000 lbs

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9
Q

Minimum Runway Length

A

4500 ft

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10
Q

Minimum Runway Width

A

75 ft

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11
Q

Max Runway Slope (+/-)

A

2%

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12
Q

Ops Review Runway Requirements

A

Contaminated: Less than 5800 ft

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13
Q

RVSM Operation Equipment

A
  • (1) Autopilot
  • (1) Altitude Alerting Device
  • (1) ATC Altitude Reporting Transponder
  • (2) Air Data Computers (ADC)
  • (2) Pitot probe heaters on the probes linked to the ADC in use
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14
Q

GL5000/5500 Max Ramp & Taxi Weight

A

92,750 lbs

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15
Q

GL6000 Max Ramp & Taxi Weight

A

99,750 lbs

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16
Q

GL5000/5500 Max ZFW

A

58,000 lbs

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17
Q

GL6000 Max ZFW

A

58,000 lbs

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18
Q

Max Baggage Compartment Weight With Net

A

1500 lbs

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19
Q

Max Baggage Compartment Weight Without Net

A

1000 lbs

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20
Q

Max Altitude for Takeoff

A

13,700 ft

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21
Q

Max Altitude for SLAT/FLAP Extended

A

18,000 ft

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22
Q

Max Altitude Landing Gear Extended

A

20,000 ft

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23
Q

Minimum Takeoff Temperature

A

-40C

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24
Q

Max Takeoff/Landing Temperature

A

50C

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25
Q

Max Speed Below 8000ft

A

300 kts

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26
Q

Max Speed 8,000 - 30,267ft

A

340 kts

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27
Q

Max Speed 30,267 - 35,000 ft

A

.89M

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28
Q

GL5500 Max Tire Speed

A

196 kts

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29
Q

GL5000/6000 Max Tire Speed

A

183 kts

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30
Q

Max Landing Gear Extended Speed

A

250 kts/.70M

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31
Q

Max Airspeed Slats OUT/Flaps 0

A

225 kts

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32
Q

Max Airspeed Slats OUT/Flaps 6

A

210 kts

33
Q

Max Airspeed Slats OUT/Flaps 16

A

210 kts

34
Q

Max Airspeed Slats OUT/Flaps 30

A

185 kts

35
Q

Max Differential Pressurization

A

10.73 psi

36
Q

Pressurization Safety Valve Setting

A

10.63 psi

37
Q

Max Negative Pressurization Relief

A

-0.5 psi

38
Q

Max Differential Pressurization Taxi/Takeoff

A

0.1 psi

39
Q

Max Differential Pressurization for Landing

A

1.0 psi

40
Q

QFE Air Conditioning and Pressurization Operations

A
  1. LDG ELEV - MAN
  2. LDG ELEV - 0
41
Q

Minimum Temperature for APU Start on the Ground

A

-40C

42
Q

Max APU Temperature During Start

A

Red Max Limit

43
Q

Max APU Air Extraction Altitude

A

30,000 ft

44
Q

Max APU Air Extraction Temperature

A

+45C

45
Q

Max Altitude with Yaw Damper Disengaged

A

41,000 ft

46
Q

APU Generator Load Limit

A

40 kVA

47
Q

GL5000/5500/6000 Wing Pressure Fueling Quantity

A

30,100 lbs

48
Q

GL5000/5500 Center Tank Pressure Fueling Quantity

A

9,150 lbs

49
Q

GL6000 Center Tank Pressure Fueling Quantity

A

12,700 lbs

50
Q

GL6000 Aft Tank Pressure Fueling Quantity

A

2,300 lbs

51
Q

GL5000/5500 Total Pressure Fueling Quantity

A

39,250 lbs

52
Q

GL6000 Total Pressure Fueling Quantity

A

45,100 lbs

53
Q

Max Fuel Imbalance Ground

A

600 lbs

54
Q

Max Fuel Imbalance in Flight

A

1,100 lbs

55
Q

Minimum Go-Around Fuel per Tank

A

600 lbs

56
Q

Do not use starter if N2 exceeds…

A

42% (windmill)

57
Q

GL5000/6000 Max Oil Consumption

A

0.21 qt/hr

58
Q

GL5500 Max Oil Consumption

A

0.20 qt/hr

59
Q

Minimum Oil Temp for Start

A

-40C

60
Q

Maximum Oil Temperature

A

160C

61
Q

Normal Oil Pressure

A

35 - 45 psi

62
Q

Minimum Oil Pressure

A

25 psi

63
Q

Minimum OAT Oil Replenishment System

A

-12C

64
Q

Engine Oil Replenishment

A

Engine Shutdown for minimum of 5 min, but no more than 30 min.

65
Q

APU Oil Replenishment

A

Shutdown more than 15 min.

66
Q

Minimum N2 when operating in icing conditions

A

76%

67
Q

Wide cut fuel is limited to ____ ft until bulk fuel temperature is below ____ C.

A

13,000 ft, 5C

68
Q

Do not takeoff if engine fuel temperature is below ____.

A

5C

69
Q

Minimum bulk fuel temperature for takeoff.

A

-30C

70
Q

Bulk fuel freezing point of Jet A

A

-40C

71
Q

Oxygen Bottles/Normal Pressure

A

4x 50.1ft3 bottles, 1850PSI at 21C

72
Q

DC Auxiliary Pumps are used…

A
  • For Engine & APU Starting.
  • Wing-to-Wing Transferring.
  • In the Event of AC PUMP Failure they come on automatically.

Automatically During Takeoff/Landing with engines on & at least one of the following:

  • Flaps > 0
  • Landing gear down in flight.
  • Low wing fuel condition (600lbs each wing)
73
Q

Cabin Altitude Caution

A

8200 ft

74
Q

Cabin Altitude Warning

A

9000 ft

75
Q

EICAS Inhibited

A
  • Takeoff: 80kts to 400ft
  • Landing: 200ft to 50kts
76
Q

OUT/6 Takeoff Crosswind Exceeds 20kts adds…

A

1700ft Field Length

77
Q

Packs in MAN TEMP controls temperature limits.

A

5 - 60C

78
Q

Rotor Bow Start times

A

20 min - 5 hours.

79
Q

Yaw Damper

A
  • Prevents Dutch Roll.
  • Coordinates Turns.

Global 5000/5500/6000 (12 decks)

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