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Global Express > Limitations > Flashcards

Limitations Flashcards

1
Q

Dimensions

A

Wingspan 94ft
Length 99ft 5in
Tail approx 25ft

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2
Q

Maximum Taxi/Ramp weight

A

98,250 lbs

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3
Q

Maximum Takeoff Weight

A

98,000 lbs

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4
Q

Maximum Landing Weight

A

78,600 lbs

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5
Q

Maximum Zero Fuel Weight (ZFW)

A

56,000 lbs

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6
Q

Minimum Flight Weight

A

48,200 lbs

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7
Q

Minimum Operating Weight Empty

A

45,000 lbs

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8
Q

Flaps 0 Load Limits

A

-1 to +2.5G

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9
Q

Slats/Flaps Extended Load Limit

A

0 to +2G

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10
Q

Minimum/Maximum runway slope

A

+/-2%

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11
Q

May operations from unprepared runways be conducted?

A

No

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12
Q

Turbulence Penetration Speed

A

300 KIAS / .80M

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13
Q

Max operating altitude

A

51,000ft

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14
Q

Max pressure altitude for takeoff and landing

A

10,000ft pressure altitude

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15
Q

Max/Min ambient temperature for takeoff

A

+50C / -40C

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16
Q

Max tailwind component for engine start

A

20kts

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17
Q

When winds exceed 20kts, what is the required thrust for taxi?

A

Minimum Thrust

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18
Q

Max slats extended speed

A

225 KIAS

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19
Q

At what altitude must flight spoilers be retracted on approach?

A

300ft AGL

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20
Q

Max tailwind component for takeoff and landing

A

10kts

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21
Q

Max Flaps 6 Speed

A

210 KIAS

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22
Q

Max Flaps 16 Speed

A

210 KIAS

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23
Q

Max Flaps 30 Speed

A

185 KIAS

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24
Q

Vlo

A

200 KIAS

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25
Q

Vle

A

250 KIAS

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26
Q

Tire limiting speed

A

183 KIAS

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27
Q

Vmcg

A

80 KIAS

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28
Q

Vmca

A

86 KIAS

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29
Q

Minimum autopilot engagement height

A

400ft AGL

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30
Q

Minimum autopilot use height for precision approach? Non-precision approach?

A

CAT I or II ILS - 50ft AGL
Non-precision - 400ft AGL

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31
Q

Max ITT for ground/air start

A

700C (ground)
850C (air)

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32
Q

Start duty cycles

A

3 min on, 15 secs off
3 min on, 15 secs off
3 min on, 15 min off

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33
Q

Auto-throttle must be engaged and verified by what Airspeed?

A

60 KIAS

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34
Q

Max engine relight altitude

A

30,000ft

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35
Q

Min temperate for starting a cold soaked APU

A

-40C

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36
Q

Max OAT for bleed air extraction from the APU for air conditioning ops?

A

> 45C

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37
Q

Max Load rating for APU

A

40 KVA

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38
Q

What is the associated limit of the APU is powering an AC Bus above 37,000ft?

A

The associated hydraulic pump must be selected off (3412)
1B - AC Bus 3
3A - AC Bus 4
3B - AC Bus 1
2B - AC Bus 2

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39
Q

When must the fuel crossfeed be selected off?

A

Takeoff and Landing

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40
Q

When does the fuel transfer from the center tank to the wing tank start?

A

Wing tank quantity drops below 93%, continues till wing reaches full

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41
Q

What is the operating limitations while holding in icing conditions?

A

Do not hold with slats extended

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42
Q

Max operating speed for extending/retracting the landing gear?

A

200KIAS

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43
Q

Max Airspeed with landing gear extended

A

250 KIAS / .7 M

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44
Q

Max operating altitude with landing gear extended

A

20,000 ft

45
Q

How many AC Buses does the AC electrical system have?

A

8 total
Four primary - 1,2,3,4
Four secondary - 1A, 2A, 3A, ESS

46
Q

When do the passenger masks deploy?

A

14,500ft cabin altitude

47
Q

How much thrust do the engines on the Global express supply at sea level?

A

14,750lbs @ SL ISA to +20C

48
Q

Bleed air extraction is used for:

A

Air conditioning
Pressurization
Cowl and wing anti-ice
Engine starts

49
Q

When should ‘rotorbow’ dry cranking be expected during automatic starts?

A

Between 20 mins and 5 hours of previous engine start

50
Q

How are the primary flight controls controlled and actuated?

A

Mechanically controlled
Hydraulically actuated

51
Q

Which hydraulic systems power the rudder PCUs?

A

Hydraulic systems 1,2 and 3

52
Q

How may the pilot stop the stick pusher?

A

Pressing and holding the autopilot/stick pusher (AP/SP DISC) disconnect button

53
Q

What is the normal circling approach configuration and category?

A

Flaps 30 and Vref + 10kts
CAT C minimums
At it above 141kts - CAT D

54
Q

Max demonstrated crosswind for takeoff and landing

A

29 kts

55
Q

For airplane operations in excess of 3 hours, the oil system must be verified?

A

Full before flight, greater than 10.62qts

56
Q

Mmo - FL350, FL414, FL470, FL510

A

FL350 - .89M
FL414 - .88M
FL470 - .858M
FL510 - .842M

57
Q

Vmo - above and below 8,000ft

A

Above - 340 KIAS
Below - 300 KIAS

58
Q

What must be done if a tailwind causes observed N1 rotation before start?

A

Extended dry crank (EDC) for 30 secs followed by an immediate auto start

59
Q

Max altitude for slats/flaps

A

18,000ft

60
Q

Min autopilot use height for a non-precision approach with vertical path guidance?

A

160 AGL

61
Q

Max starting altitude for APU

A

37,000ft

62
Q

Fuel in the aft tank must be considered unusable unless?

A

Each wing contains at least 5,000lbs fuel at departure -and- the plane cruise altitude is greater than 30,000ft

63
Q

Minimum Go-Around fuel

A

600lbs/wing
Note - level flight and max 10 degrees nose up

64
Q

When does fuel transfer from the aft tank start?

A

Wing tank falls to 5,500lbs

65
Q

Min pavement width for 180 turn?

A

68ft

66
Q

How are active/armed flight director and auto-throttle modes indicated on the AFCS display?

A

Active - green
Armed - white

67
Q

During normal operation, symbol generator (SG) 1 generates symbols for which display units (DUs)?

A

DU 1 and DU 2

68
Q

In the event of a single generator operation, which AC Buses are automatically shed?

A

AC Buses 2 and 3
This results in AC buses 2A and 3A also being shed

69
Q

Which hydraulic systems power the aileron PCUs?

A

Left aileron - systems 1 and 3
Right aileron - systems 2 and 3

70
Q

Which hydraulic systems power the elevator PCUs?

A

Left elevator - systems 1 and 3
Right elevator - systems 2 and 3

71
Q

How many spoiler panels are located on each wing?

A

4 multifunction spoilers -and- 2 ground spoilers

72
Q

What is the ground operation limit of the display units with the cockpit temperature in excess of 40C?

A

Operation for greater than 30 mins is prohibited

73
Q

What are the buoyancy limitations for takeoff or landing near water above maximum landing weight?

A

Outflow valve 2 closed, one air pack shut down

74
Q

What must be done if crosswind component exceeds 20kts on takeoff?

A

Do not exceed 66% N1 until 30 KIAS
Increase takeoff distance by:
1700ft - flaps 6
1500ft - flaps 16

75
Q

What is the maximum altitude for flight with the yaw damper disengaged?

A

41,000ft

76
Q

What is the static ground operation limit?

A

Steady operation between 66% to 80% prohibited

77
Q

Name 3 thrust reverse limitations:

A

Must not be selected in flight
Must not be used for touch and goes
May not back up the airplane

78
Q

Do not test the operation of the pressure relief valves when?

A

Wing tank above 11,800lbs
Center tank above 8,000lbs

79
Q

Normal and Maximum cabin differential pressure

A

Normal - 10.33 psid
Max - 10.73 psid
‘Delta P’ message - 10.85 psid

80
Q

When is cowl anti-ice required? Prohibited?

A

OAT +10C and visible moisture or contaminated taxiways/runways
AUTO prohibited for takeoff

81
Q

When is wing anti-ice required? Prohibited?

A

OAT +5C and visible moisture or contaminated taxiways/runways
AUTO prohibited for takeoff
Type II and IV - anti-ice prohibited ON until just prior to thrust increase for takeoff

82
Q

What are the conditions for inflight icing conditions?

A

Visible moisture and temp between TAT +10 and SAT -40C

83
Q

What is the result of pushing the event button on the landing gear Control panel?

A

Flags a particular event in time within the flight data recorder memory
Encodes the central aircraft information maintenance system

84
Q

What are the sources of airplane generated AC power?

A

4 40kVA engine driven generators
1 40kVA APU generator
Ram air turbine

85
Q

What are the 6 primary DC power sources?

A

TRU 1, 2, ESS TRU 1, 2
Avionics battery
APU battery

86
Q

Which DC Buses are automatically shed during single TRU operation?

A

DC Bus 1 and 2

87
Q

What five events occur when the ENG FIRE DISCH handle is pulled?

A

1) fuel SOV closes
2) hydraulic SOV closes
3) bleed air SOV closes
4) AC VFGs taken offline
5) fire bottle arms

88
Q

How is operation of the slats and flaps controlled?

A

By two independent slat/flap control units (SFCUs)

89
Q

The MFS are used for what purpose?

A

Roll assist
Proportional lift dumping
Ground lift dumping
Combination roll assist and proportional lift dumping

90
Q

What is the prioritization of checklists?

A

Memory items
Emergency checklists (Red)
Normal checklists (normals)
Caution and advisory information (ambers)

91
Q

What is the max altitude for APU operations?

A

45,000ft

92
Q

What is the maximum altitude for bleed air extraction from the APU?

A

30,000ft

93
Q

Max permissible fuel imbalance for on ground and during takeoff and landing?

A

1100lbs < 19,450 fuel tank load
600lbs > 20,250 fuel tank load

94
Q

Max permissible fuel imbalance during flight?

A

1100lbs

95
Q

What does a GEN ‘FAIL’ light on the electrical panel indicate?

A

Failed generating channel
-or-
Fire discharge handle is pulled

96
Q

What are the 4 main DC buses?

A

DC Bus 1 and 2
DC ESS Bus
BATT Bus

97
Q

Ground spoilers when armed will deploy on landing with?

A

Engine throttle at idle or below and two of the following three conditions:
-RA below 7ft
-one main landing gear WOW
-one wheel speed greater than 16kts

98
Q

What are the warning messages and associated cabin altitudes for loss of pressurization?

A

CAB ALT - 8200ft
CAB ALT Warning - 9000ft
Or 1000 / 1800 ft above landing if landing above 7230 MSL

99
Q

Selecting the ENG RUN switch to OFF closes which fuel shutoff valve?

A

High pressure shutoff valve within the fuel metering unit

100
Q

How is emergency shutdown of the APU accomplished?

A

BATT MASTER switch selected OFF with no AC power on
APU fire DISCH handle pulled
APU SHUTOFF button (services panel)
APU compartment SHUTDOWN button

101
Q

What happens when the APU DISCH is pulled?

A

1) fuel SOV closes
2) ignition shut off
3) pneumatics shut off
4) APU electrics isolated
5) fire bottle arms

102
Q

What engines are installed on the Global Express?

A

BR700-710A2-20

103
Q

Describe the two main engine rotating assemblies

A

Single stage LP fan driven by a two stage turbine
Ten stage HP compressor driven by a two stage turbine

104
Q

What are the engine idle limits?

A

Max ITT - 860C
Min N2 - 58.0%

105
Q

Engine takeoff thrust limits

A

MAX ITT - 900C
N2 - 99.6%
N1 - 102.0%
5 mins two engines, 10 mins SE

106
Q

Engine max continuous operating limits

A

MAX ITT - 860C
N2 - 98.9%
N1 - 102.0%

107
Q

What is the purpose of the DC POWER EMERGENCY OVERRIDE switch?

A

During loss of all DC power
Allows ESS TRU 1 and 2 to bypass the DCPC and power the SPDAs directly

108
Q

When do the AC wing boost pumps operate?

A

ENG RUN switches ‘ON’
Crossfeed shutoff valve selected ‘open’ during single engine operation

109
Q

When do the wing DC aux fuel pumps operate automatically?

A

One or both AC pumps low pressure
Flaps position > 0
In flight with landing gear down and locked
Low fuel condition < 600lbs/wing
Wing transfer - 400lb or greater wing imbalance

Global Express (4 decks)

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