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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
Vle
250 KIAS
26
Tire limiting speed
183 KIAS
27
Vmcg
80 KIAS
28
Vmca
86 KIAS
29
Minimum autopilot engagement height
400ft AGL
30
Minimum autopilot use height for precision approach? Non-precision approach?
CAT I or II ILS - 50ft AGL Non-precision - 400ft AGL
31
Max ITT for ground/air start
700C (ground) 850C (air)
32
Start duty cycles
3 min on, 15 secs off 3 min on, 15 secs off 3 min on, 15 min off
33
Auto-throttle must be engaged and verified by what Airspeed?
60 KIAS
34
Max engine relight altitude
30,000ft
35
Min temperate for starting a cold soaked APU
-40C
36
Max OAT for bleed air extraction from the APU for air conditioning ops?
> 45C
37
Max Load rating for APU
40 KVA
38
What is the associated limit of the APU is powering an AC Bus above 37,000ft?
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
39
When must the fuel crossfeed be selected off?
Takeoff and Landing
40
When does the fuel transfer from the center tank to the wing tank start?
Wing tank quantity drops below 93%, continues till wing reaches full
41
What is the operating limitations while holding in icing conditions?
Do not hold with slats extended
42
Max operating speed for extending/retracting the landing gear?
200KIAS
43
Max Airspeed with landing gear extended
250 KIAS / .7 M
44
Max operating altitude with landing gear extended
20,000 ft
45
How many AC Buses does the AC electrical system have?
8 total Four primary - 1,2,3,4 Four secondary - 1A, 2A, 3A, ESS
46
When do the passenger masks deploy?
14,500ft cabin altitude
47
How much thrust do the engines on the Global express supply at sea level?
14,750lbs @ SL ISA to +20C
48
Bleed air extraction is used for:
Air conditioning Pressurization Cowl and wing anti-ice Engine starts
49
When should ‘rotorbow’ dry cranking be expected during automatic starts?
Between 20 mins and 5 hours of previous engine start
50
How are the primary flight controls controlled and actuated?
Mechanically controlled Hydraulically actuated
51
Which hydraulic systems power the rudder PCUs?
Hydraulic systems 1,2 and 3
52
How may the pilot stop the stick pusher?
Pressing and holding the autopilot/stick pusher (AP/SP DISC) disconnect button
53
What is the normal circling approach configuration and category?
Flaps 30 and Vref + 10kts CAT C minimums At it above 141kts - CAT D
54
Max demonstrated crosswind for takeoff and landing
29 kts
55
For airplane operations in excess of 3 hours, the oil system must be verified?
Full before flight, greater than 10.62qts
56
Mmo - FL350, FL414, FL470, FL510
FL350 - .89M FL414 - .88M FL470 - .858M FL510 - .842M
57
Vmo - above and below 8,000ft
Above - 340 KIAS Below - 300 KIAS
58
What must be done if a tailwind causes observed N1 rotation before start?
Extended dry crank (EDC) for 30 secs followed by an immediate auto start
59
Max altitude for slats/flaps
18,000ft
60
Min autopilot use height for a non-precision approach with vertical path guidance?
160 AGL
61
Max starting altitude for APU
37,000ft
62
Fuel in the aft tank must be considered unusable unless?
Each wing contains at least 5,000lbs fuel at departure -and- the plane cruise altitude is greater than 30,000ft
63
Minimum Go-Around fuel
600lbs/wing Note - level flight and max 10 degrees nose up
64
When does fuel transfer from the aft tank start?
Wing tank falls to 5,500lbs
65
Min pavement width for 180 turn?
68ft
66
How are active/armed flight director and auto-throttle modes indicated on the AFCS display?
Active - green Armed - white
67
During normal operation, symbol generator (SG) 1 generates symbols for which display units (DUs)?
DU 1 and DU 2
68
In the event of a single generator operation, which AC Buses are automatically shed?
AC Buses 2 and 3 This results in AC buses 2A and 3A also being shed
69
Which hydraulic systems power the aileron PCUs?
Left aileron - systems 1 and 3 Right aileron - systems 2 and 3
70
Which hydraulic systems power the elevator PCUs?
Left elevator - systems 1 and 3 Right elevator - systems 2 and 3
71
How many spoiler panels are located on each wing?
4 multifunction spoilers -and- 2 ground spoilers
72
What is the ground operation limit of the display units with the cockpit temperature in excess of 40C?
Operation for greater than 30 mins is prohibited
73
What are the buoyancy limitations for takeoff or landing near water above maximum landing weight?
Outflow valve 2 closed, one air pack shut down
74
What must be done if crosswind component exceeds 20kts on takeoff?
Do not exceed 66% N1 until 30 KIAS Increase takeoff distance by: 1700ft - flaps 6 1500ft - flaps 16
75
What is the maximum altitude for flight with the yaw damper disengaged?
41,000ft
76
What is the static ground operation limit?
Steady operation between 66% to 80% prohibited
77
Name 3 thrust reverse limitations:
Must not be selected in flight Must not be used for touch and goes May not back up the airplane
78
Do not test the operation of the pressure relief valves when?
Wing tank above 11,800lbs Center tank above 8,000lbs
79
Normal and Maximum cabin differential pressure
Normal - 10.33 psid Max - 10.73 psid ‘Delta P’ message - 10.85 psid
80
When is cowl anti-ice required? Prohibited?
OAT +10C and visible moisture or contaminated taxiways/runways AUTO prohibited for takeoff
81
When is wing anti-ice required? Prohibited?
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
What are the conditions for inflight icing conditions?
Visible moisture and temp between TAT +10 and SAT -40C
83
What is the result of pushing the event button on the landing gear Control panel?
Flags a particular event in time within the flight data recorder memory Encodes the central aircraft information maintenance system
84
What are the sources of airplane generated AC power?
4 40kVA engine driven generators 1 40kVA APU generator Ram air turbine
85
What are the 6 primary DC power sources?
TRU 1, 2, ESS TRU 1, 2 Avionics battery APU battery
86
Which DC Buses are automatically shed during single TRU operation?
DC Bus 1 and 2
87
What five events occur when the ENG FIRE DISCH handle is pulled?
1) fuel SOV closes 2) hydraulic SOV closes 3) bleed air SOV closes 4) AC VFGs taken offline 5) fire bottle arms
88
How is operation of the slats and flaps controlled?
By two independent slat/flap control units (SFCUs)
89
The MFS are used for what purpose?
Roll assist Proportional lift dumping Ground lift dumping Combination roll assist and proportional lift dumping
90
What is the prioritization of checklists?
Memory items Emergency checklists (Red) Normal checklists (normals) Caution and advisory information (ambers)
91
What is the max altitude for APU operations?
45,000ft
92
What is the maximum altitude for bleed air extraction from the APU?
30,000ft
93
Max permissible fuel imbalance for on ground and during takeoff and landing?
1100lbs < 19,450 fuel tank load 600lbs > 20,250 fuel tank load
94
Max permissible fuel imbalance during flight?
1100lbs
95
What does a GEN ‘FAIL’ light on the electrical panel indicate?
Failed generating channel -or- Fire discharge handle is pulled
96
What are the 4 main DC buses?
DC Bus 1 and 2 DC ESS Bus BATT Bus
97
Ground spoilers when armed will deploy on landing with?
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
What are the warning messages and associated cabin altitudes for loss of pressurization?
CAB ALT - 8200ft CAB ALT Warning - 9000ft Or 1000 / 1800 ft above landing if landing above 7230 MSL
99
Selecting the ENG RUN switch to OFF closes which fuel shutoff valve?
High pressure shutoff valve within the fuel metering unit
100
How is emergency shutdown of the APU accomplished?
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
What happens when the APU DISCH is pulled?
1) fuel SOV closes 2) ignition shut off 3) pneumatics shut off 4) APU electrics isolated 5) fire bottle arms
102
What engines are installed on the Global Express?
BR700-710A2-20
103
Describe the two main engine rotating assemblies
Single stage LP fan driven by a two stage turbine Ten stage HP compressor driven by a two stage turbine
104
What are the engine idle limits?
Max ITT - 860C Min N2 - 58.0%
105
Engine takeoff thrust limits
MAX ITT - 900C N2 - 99.6% N1 - 102.0% 5 mins two engines, 10 mins SE
106
Engine max continuous operating limits
MAX ITT - 860C N2 - 98.9% N1 - 102.0%
107
What is the purpose of the DC POWER EMERGENCY OVERRIDE switch?
During loss of all DC power Allows ESS TRU 1 and 2 to bypass the DCPC and power the SPDAs directly
108
When do the AC wing boost pumps operate?
ENG RUN switches ‘ON’ Crossfeed shutoff valve selected ‘open’ during single engine operation
109
When do the wing DC aux fuel pumps operate automatically?
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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