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Global 7500 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight

A

115,100

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2
Q

Max Takeoff Weight ***

A

114,850

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3
Q

Max Landing Weight ***

A

87,600

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4
Q

Max Zero Fuel Weight

A

67,500

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5
Q

Minimum Flight Weight

A

60,000

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6
Q

45 minute IFR Reserve Fuel

A

2500 lb

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7
Q

Hot Spare fuel

A

8500 lb

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8
Q

Emergency fuel

A

1500 lb Wings
or 750 lb per wing

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9
Q

Parking Inclement weather fuel

A

20000 lb

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10
Q

Runway Requirements

A

4500 ft long
98 ft or 30 m wide
Max slope 2%
Opp review required
Dry less than 5000 ft
Wet/Contaminated less than 5800 ft

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11
Q

Max Crosswind ***

A

27
Contaminated/Runway
Fair/Medium 20
Poor. 10

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12
Q

Max Tailwind ***

A

10

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13
Q

Buoyancy Limitations when above max landing weight ***

A

Taking off or landing over water you must have
Outflow valve 2 closed
R Pack off

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14
Q

Baggage compartment weight limit

A

2500 lb

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15
Q

Maximum operating altitude***

A

51,000 ft

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16
Q

Maximum take off and landing altitude

A

10,000 ft. Pres. Alt

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17
Q

Maximum slat/flap extended altitude

A

18,000 ft

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18
Q

Maximum landing gear extended altitude

A

20,000 ft

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19
Q

Minimum flight spoiler altitude ***

A

300 ft

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20
Q

Minimum take off temperature

A

-40 c

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21
Q

Maximum take off and landing temperature

A

ISA +40 c

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22
Q

Vmo below 8000 ft

A

300

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23
Q

Vmo 8000 -10,000 ft

A

300 increasing linear to 335

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24
Q

Vmo 10,000-16,000 ft

A

335

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25
Q

Vmo 16,000-20,000 ft

A

335 decreasing linear to 320

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26
Q

Vmo 20,000-35,000 ft

A

320

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27
Q

Vmo 35,000-51,000

A

.925

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28
Q

Vfe Flaps 1 ***

A

225

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29
Q

Vfe Flaps 2 ***

A

210

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30
Q

Vfe Flaps 3 ***

A

210

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31
Q

Vfe Flaps 4 ***

A

185

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32
Q

Minimum speed with flight spoilers extended

A

Vref+10

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33
Q

Vlo ***

A

200

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34
Q

Vle

A

250

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35
Q

Maximum tire speed

A

195

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36
Q

Turbulent air penetration speed MSL to 8,000ft

A

265 linear to 285

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37
Q

Turbulent air penetration speed 10,000 ft and above ***

A

Lesser of 285 or .85

38
Q

Max differential preservation

A

10.73

39
Q

Max negative relief pressurization

A

-0.5

40
Q

Max differential taxi and take off pressurization

A

0.1

41
Q

Max differential landing

A

1.0

42
Q

Air conditioning and pressurization Aux Press On Max altitude ***

A

41,000 ft

43
Q

Max passengers

A

14 pax + 1 FA + 2 pilots =17

44
Q

Lap children are approved for seat

A

4 and Crew rest seat. May not occupy the divan during Taxi Takeoff and Landing

45
Q

APU start attempts limit ***

A

3 attempts in 1 hour

46
Q

APU max altitude for start ***

A

45,000 ft

47
Q

APU min temp for starting on ground

A

-40 c

48
Q

APU max temp during start EGT

A

Red max limit AOM
1032° C. CAE sheet

49
Q

APU max operating altitude ***

A

51,000 ft

50
Q

APU max air extraction altitude

A

25,000 ft

51
Q

APU max air extraction temp on the ground

A

+48 c or 118.4 f

52
Q

Autopilot after Takeoff ***

A

400 ft AGL

53
Q

Autopilot non steep Approach ***

A

80 ft AGL

54
Q

Autopilot steep Approach ***

A

200 AGL

55
Q

Engine Generator Load Limit

A

60 kVA continuous
67.5 kVA for 5 min
75 kVA for 2 min

56
Q

APU generator load limits

A

40 kVA at 51,000 ft
60 kVA at 45,000 ft

57
Q

Fuel capacity pressure fueling

A

Wings. 35,100 Both 17,550 Each
Center 14,200
Aft. 2550
Total. 51850

58
Q

Fuel imbalance

A

Ground. 600
In-flight. 1100

59
Q

Fuel crossfeed/xfer usage limits

A

•Do not select AFT XFER ON if either wing tank exceeds 15,000 lb
•Fuel crossfeed must be closed for Takeoff and landing
•Do not use fuel crossfeed below 10,000 ft for dual engine operations
•Minimum fuel quantity is 2500 lb per wing tank for wing to wing fuel transfer

60
Q

Fuel Temp. Limitations

A

• Do not takeoff if engine fuel temp below 5°c
• Min. bulk fuel temp. for Takeoff -30°c
• In flight bulk fuel temp must remain above the applicable bulk fuel freezing point Jet A is -40°c

60
Q

Engine anti ice ***

A

•Must be on for Takeoff when OAT is 10°c or below in visible moisture or when operating on contaminated runway use in accordance with anti-ice System operations

60
Q

Wing Anti-ice ***

A

• Must be on for Takeoff when OAT is 5°c or below in visible moisture or when operating on contaminated runway.
Use in accordance with Anti-Ice system operation
• Do not hold in icing conditions with slats out
• When TAT is above 10°c do not use wing Anti-Ice in flight

61
Q

Brakes min turn time ***

A

15 min if Temp is white 35 min & decreasing through 15 indication

62
Q

EFIS ***

A

Do not use MAP PLAN display for navigation while operating north of 70°N or south or 70°S

63
Q

FLC mode ***

A

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

64
Q

Approach Category ***

A

C with speeds faster than 140 kt use category D

65
Q

Max tailwind for engine start ***

A

20 kt

66
Q

When crosswind component exceeds 18 kt ***

A

Do not exceed 60% N1 below 30 kt

67
Q

Min oil temp for taxi ***

A

20°c

68
Q

Min oil temp for takeoff ***

A

43°c

69
Q

Min oil for the oil replenishment system ***

A

2.5 qt minimum

70
Q

Starter limitations ***

A

Start 1 & 2 max time 5 min followed by a cool down of 5 min and starts 3 through 10 max time 5 min followed by a cool down of 15 min

71
Q

Thrust Reversers Limitations

A

• Use TRs in flight
• Touch & Go after deployment or TRs
• Use TRs to back the aircraft

72
Q

Display Units

A

No operations with cabin temp in excess of 40°C for more than 30 min

73
Q

Usable Fuel with Gravity Refueling

A

L/R wing tank 14,850 lb each
29,700 lb total

74
Q

Wide cut fuels and mixing of fuels

A

JP4, Jet B wide cut fuels prohibited

Fuel mixing is permitted

75
Q

T.O thrust time 2 & 1 engines

A

5 min. Both
10 min. Single

76
Q

Minimum Oil start temp.

A

-40° c

77
Q

Max oil consumption rate

A

.31 qt/hr

78
Q

Oil replenishment min. temp.

A

-12°c

79
Q

APU max temp for operations

A

ISA + 40°c

80
Q

OMS Onboard Maintenance System

A

Prohibited for use in flight

81
Q

Super Cooled Large Droplet Icing

A

WAI & CAI required ON
Leave ice if ice builds on side window

82
Q

Max Starter Engagement

A

56% N2

83
Q

Towing With torque link connected

A

Is prohibited except for straight push back

84
Q

QFE ops landing

A

Manually set landing elevation to 0.

85
Q

Engine inoperative: What’s your limitation, when it come to type of speed

A

Man speed only

86
Q

Max Spoiler

A

Prohibited unless directed by procedure.

87
Q

Speakers muted

A

Crew must wear headsets.

88
Q

Wing Span

A

104 ft

89
Q

Height

A

27 ft

90
Q

Wheelbase distance

A

14 ft 5 in

Global 7500 (5 decks)

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