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Global 6000 > Limitations > Flashcards

Limitations Flashcards

1
Q

45-minute IFR fuel reserve

A

2500 lbs.

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2
Q

hot spare fuel

A

8500 lbs.

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3
Q

emergency fuel

A

1500 lbs.

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4
Q

inclement weather fuel

A

15,000 lbs.

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5
Q

minimum runway length

A

4500

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6
Q

minimum runway width

A

75

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7
Q

max slope

A

+/- 2%

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8
Q

runway ops review required if…

A

contaminated: less than 5800 feet

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9
Q

For runway less than 95 feet wide, four requirements:

A

1) contact FPD or CP for approval
2) LP must accomplish landing
3) comply with crosswind limits
4) gust factor is 10kts max for all operations

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10
Q

Crosswind limit, dry or wet runway

A

29 kts

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11
Q

Crosswind limit, contaminated runway condition “fair/medium”

A

20 kts

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12
Q

Crosswind limit, contaminated runway condition “poor”

A

10 kts

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13
Q

Max tailwind takeoff and landing

A

10 kts

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14
Q

RVSM requirements

A

Autopilot (1)
Altitude alerting device (1)
ATC altitude reporting transponder (1)
Air data computers (2)
Pitot probe heaters (2) on probes linked to the ADC in use

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15
Q

Buoyancy limitations if above max landing weight for takeoff or landing over bodies of water

A

Outflow valve 2 - close
R Pack - off
Manually enter ARR or DEP PERF V-speeds

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16
Q

Max ramp and taxi weights

A

GL5000/5500: 92,750
GL6000: 99,750

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17
Q

Max takeoff weights

A

GL5000/5500: 92,500
GL6000: 99,500

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18
Q

Max landing weight

A

GL5000/5500/6000: 78,600

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19
Q

Max zero fuel weight

A

GL5000/5500/6000: 58,000

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20
Q

Baggage compartment weights

A

1500 with net
1000 without net

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21
Q

Max operating altitude

A

51,000

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22
Q

Maximum takeoff and landing altitude

A

13,700

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23
Q

Max altitude SLAT/FLAP extended

A

18,000

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24
Q

Max altitude landing gear extended

A

20,000

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25
Q

Minimum altitude FLIGHT SPOILERS

A

300 (unless steep approach)

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26
Q

Minimum temperature takeoff

A

-40 C
Alternate airports must be warmer than -40 F

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27
Q

Max temperature takeoff/landing

A

+50 C

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28
Q

Max airspeed Slats OUT/Flaps 0

A

225

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29
Q

Max airspeed Slats OUT/Flaps 6

A

210

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30
Q

Max airspeed Slats OUT/Flaps 16

A

210

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31
Q

Max airspeed Slats OUT/Flaps 30

A

185

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32
Q

Max landing gear operating speed

A

200

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33
Q

Max landing gear extended speed

A

250/.7

34
Q

Turbulent air penetration speed

A

lesser of 300 or .80

35
Q

Air Cond and Pressurization
Aux Press - ON

A

GL5000/6000: max altitude 41,000 ft
GL5500: max altitude 37,000 ft

36
Q

Air Cond and Pressurization
Emer Depress - On

A

Max altitude 15,000 ft

37
Q

Air cond and pressurization
QFE Operations

A
  1. LDG ELEV - MAN
  2. LDG ELEV - 0
38
Q

APU Starter operation

A

Three attempts in 1 hour

39
Q

APU Max altitude for start

A

37,000

40
Q

Minimum temp for APU start on ground

A

-40 C

41
Q

Max temp during APU start

A

Red max limit

42
Q

APU max operating altitude

A

45,000 ft

43
Q

APU max air extraction altitude

A

30,000 ft

44
Q

Max APU air extraction temperature

A

+45 C

45
Q

Autopilot max approach glide path angle

A

4.49 degrees

46
Q

Max altitude with yaw damper disengaged

A

41,000

47
Q

Minimum autopilot engagement altitude after takeoff

A

400 AGL

48
Q

Minimum autopilot altitude Cat 1 ILS or LPV (GS less than or equal to 3.5)

A

80 AGL

49
Q

Minimum autopilot altitude Cat 1 ILS or LPV (GS 3.51 to 4.49), approach to DA using VGP

A

160 AGL

50
Q

Minimum autopilot altitude approach to DDA using VGP, DDA using VPATH or FPA, approach to MDA

A

400 AGL

51
Q

APU generator load limit

A

40 kVA

52
Q

Flight controls (spoilers)

A

Do not use MAX spoilers unless directed by AFM or emergency

53
Q

GL5000/5500 pressure refueling total quantity

A

39,250

54
Q

GL6000 pressure refueling total quantity

A

45,100

55
Q

Fuel imbalance

A

Ground 600
Flight 1100

56
Q

Minimum go around fuel

A

600 per tank
Wings level, pitch max 10 degrees nose up

57
Q

Anti-ice operation in visible moisture or on contaminated surfaces, on ground, OAT 10 C or below

A

Cowls on, wing off

58
Q

Anti-ice operation in visible moisture or on contaminated surfaces, on ground, OAT 5 C or below, just prior to takeoff

A

Cowls on, wing on

59
Q

Anti-ice operation in visible moisture, in flight, TAT 10 C or below

A

Cowls on, wings on

60
Q

Engine anti-ice auto takeoff

A

Do not use cowl anti-ice in AUTO mode during takeoff

61
Q

Wing anti-ice auto takeoff

A

Do not use wing anti-ice in AUTO mode during takeoff

62
Q

Anti-ice fluid limitation

A

If type II, III, or IV fluids have been applied, select wing anti-ice ON just prior to takeoff thrust.

63
Q

Anti-ice holding limitation

A

Do not hold in icing conditions with slats OUT

64
Q

Minimum turn time (brakes)

A

15 minutes

65
Q

Minimum fuel for towing

A

5000 lbs

66
Q

Approach FLC limitation

A

When descending on any segment of an instrument or visual approach, use of FLC mode is prohibited.

67
Q

Approach category

A

C, unless approach speed greater than 140 kts, then D

68
Q

Takeoff thrust limitation

A

5 minutes all engines operating, 10 minutes if engine failure

69
Q

Max tailwind for engine start

A

20 kts

70
Q

Max crosswind for engine start

A

GL5000/6000: 35 kts
GL5500: 25 kts

71
Q

Do not exceed 66% N1 below 30kts when crosswind component exceeds

A

GL5000/6000: 20 kts
GL5500:
20 kts for pressure altitude less than 5000 ft
15 kts for pressure altitude 5000 ft and above

72
Q

Tailwind N1 rotation

A

When N1 is rotating due to tailwind, crank engine for 30 seconds, followed immediately by AUTO start

73
Q

Auto throttle EPR

A

Ensure takeoff EPR is achieved prior to 60 kts

74
Q

Minimum oil temperature (taxi)

A

20 C

75
Q

Engine starter limitations

A

Three attempts:
1) 3 min on - 15 seconds off
2) 3 min on - 15 seconds off
3) 3 min on - 15 minutes off

Do not use starter if N2 exceeds 42% (windmilling)

76
Q

GL6000 wing fuel

A

30,100

77
Q

GL6000 center tank fuel

A

12,700

78
Q

GL6000 aft tank fuel

A

2300

79
Q

Center tank fuel usage

A

Center tank is usable only when each wing tank is full at departure and planned cruise altitude is above 30,000

80
Q

Aft fuel tank usage limitation

A

Aft tank fuel usable only when each wing tank quantity is more than 5500 lbs at departure and planned cruise altitude is above 30,000

81
Q

Center or aft tank quantity minimum for flight

A

Must be more than 500 lbs if center or aft tank is to be used in flight

82
Q

Fuel cross feed limitation

A

Fuel cross feed must be closed for takeoff or landing

Global 6000 (3 decks)

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