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Global 6000 > Limitations > Flashcards

Limitations Flashcards

(82 cards)

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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
Minimum altitude FLIGHT SPOILERS
300 (unless steep approach)
26
Minimum temperature takeoff
-40 C Alternate airports must be warmer than -40 F
27
Max temperature takeoff/landing
+50 C
28
Max airspeed Slats OUT/Flaps 0
225
29
Max airspeed Slats OUT/Flaps 6
210
30
Max airspeed Slats OUT/Flaps 16
210
31
Max airspeed Slats OUT/Flaps 30
185
32
Max landing gear operating speed
200
33
Max landing gear extended speed
250/.7
34
Turbulent air penetration speed
lesser of 300 or .80
35
Air Cond and Pressurization Aux Press - ON
GL5000/6000: max altitude 41,000 ft GL5500: max altitude 37,000 ft
36
Air Cond and Pressurization Emer Depress - On
Max altitude 15,000 ft
37
Air cond and pressurization QFE Operations
1. LDG ELEV - MAN 2. LDG ELEV - 0
38
APU Starter operation
Three attempts in 1 hour
39
APU Max altitude for start
37,000
40
Minimum temp for APU start on ground
-40 C
41
Max temp during APU start
Red max limit
42
APU max operating altitude
45,000 ft
43
APU max air extraction altitude
30,000 ft
44
Max APU air extraction temperature
+45 C
45
Autopilot max approach glide path angle
4.49 degrees
46
Max altitude with yaw damper disengaged
41,000
47
Minimum autopilot engagement altitude after takeoff
400 AGL
48
Minimum autopilot altitude Cat 1 ILS or LPV (GS less than or equal to 3.5)
80 AGL
49
Minimum autopilot altitude Cat 1 ILS or LPV (GS 3.51 to 4.49), approach to DA using VGP
160 AGL
50
Minimum autopilot altitude approach to DDA using VGP, DDA using VPATH or FPA, approach to MDA
400 AGL
51
APU generator load limit
40 kVA
52
Flight controls (spoilers)
Do not use MAX spoilers unless directed by AFM or emergency
53
GL5000/5500 pressure refueling total quantity
39,250
54
GL6000 pressure refueling total quantity
45,100
55
Fuel imbalance
Ground 600 Flight 1100
56
Minimum go around fuel
600 per tank Wings level, pitch max 10 degrees nose up
57
Anti-ice operation in visible moisture or on contaminated surfaces, on ground, OAT 10 C or below
Cowls on, wing off
58
Anti-ice operation in visible moisture or on contaminated surfaces, on ground, OAT 5 C or below, just prior to takeoff
Cowls on, wing on
59
Anti-ice operation in visible moisture, in flight, TAT 10 C or below
Cowls on, wings on
60
Engine anti-ice auto takeoff
Do not use cowl anti-ice in AUTO mode during takeoff
61
Wing anti-ice auto takeoff
Do not use wing anti-ice in AUTO mode during takeoff
62
Anti-ice fluid limitation
If type II, III, or IV fluids have been applied, select wing anti-ice ON just prior to takeoff thrust.
63
Anti-ice holding limitation
Do not hold in icing conditions with slats OUT
64
Minimum turn time (brakes)
15 minutes
65
Minimum fuel for towing
5000 lbs
66
Approach FLC limitation
When descending on any segment of an instrument or visual approach, use of FLC mode is prohibited.
67
Approach category
C, unless approach speed greater than 140 kts, then D
68
Takeoff thrust limitation
5 minutes all engines operating, 10 minutes if engine failure
69
Max tailwind for engine start
20 kts
70
Max crosswind for engine start
GL5000/6000: 35 kts GL5500: 25 kts
71
Do not exceed 66% N1 below 30kts when crosswind component exceeds
GL5000/6000: 20 kts GL5500: 20 kts for pressure altitude less than 5000 ft 15 kts for pressure altitude 5000 ft and above
72
Tailwind N1 rotation
When N1 is rotating due to tailwind, crank engine for 30 seconds, followed immediately by AUTO start
73
Auto throttle EPR
Ensure takeoff EPR is achieved prior to 60 kts
74
Minimum oil temperature (taxi)
20 C
75
Engine starter limitations
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
GL6000 wing fuel
30,100
77
GL6000 center tank fuel
12,700
78
GL6000 aft tank fuel
2300
79
Center tank fuel usage
Center tank is usable only when each wing tank is full at departure and planned cruise altitude is above 30,000
80
Aft fuel tank usage limitation
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
Center or aft tank quantity minimum for flight
Must be more than 500 lbs if center or aft tank is to be used in flight
82
Fuel cross feed limitation
Fuel cross feed must be closed for takeoff or landing

Global 6000 (3 decks)

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