G7500 FCS Flashcards

(56 cards)

1
Q

What type of system provides pitch roll and yaw control on the Global 7500?

A

Fly by wire

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2
Q

Which flight control surfaces control the pitch axis?

A

Elevators and horizontal stabilizer

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3
Q

How many ailerons are there on the Global 7500?

A

Four

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4
Q

What surfaces augment roll control besides the ailerons?

A

Multifunction spoilers

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5
Q

What surfaces provide speed brake control?

A

Multifunction spoilers

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6
Q

What is the primary function of the ground spoilers?

A

Ground lift dumping

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7
Q

How is yaw controlled on the Global 7500?

A

Rudder

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8
Q

Is aileron trim automatic or manual in FBW normal mode?

A

Automatic

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9
Q

In which FBW modes is manual aileron trim available?

A

All direct modes

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10
Q

What happens if the aileron trim switch is held for more than 3 seconds in PFCC direct mode?

A

Trim is disabled and a double beep sounds

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11
Q

How is elevator position indicated on the FLT CTRL synoptic?

A

Green triangle against a white scale

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12
Q

What happens to elevator deflection as airspeed increases in FBW normal mode?

A

Deflection decreases

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13
Q

How is available elevator deflection indicated?

A

Upper and lower tick marks on the white scale

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14
Q

What color indicates normal elevator status on the FLT CTRL synoptic?

A

Green

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15
Q

What CAS message appears if both elevator PCUs fail?

A

L ELEVATOR FAIL or R ELEVATOR FAIL

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16
Q

What does the PITCH AUTHORITY CAS message indicate?

A

Elevator command is near maximum authority

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17
Q

How is the rudder actuated?

A

Three hydraulically actuated PCUs

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18
Q

How many hydraulic systems power the rudder PCUs?

A

Three

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19
Q

What happens if two rudder PCUs fail?

A

RUDDER DEGRADED CAS message

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20
Q

What color indicates a failed rudder on the synoptic?

A

Red

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21
Q

Where is the rudder trim switch located?

A

Center pedestal

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22
Q

Is rudder trim active in both normal and direct modes?

A

Yes

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23
Q

What happens if rudder trim is outside takeoff range during takeoff?

A

CONFIG RUDDER TRIM CAS message and NO TAKEOFF alert

24
Q

What keeps primary flight controls in position when hydraulics are de energized?

A

Residual hydraulic pressure

25
What is the purpose of the gust lock system?
Prevents abrupt movement of control surfaces
26
What are the two types of stops in the sidestick pitch axis?
Soft stops and hard stops
27
What provides a tactile cue for stall awareness on the sidestick?
Sidestick shaker
28
What happens if both sidesticks are operated at once?
Inputs are summed and DUAL INPUT warning sounds
29
What must be done to enable sidestick pitch trim commands?
Both halves of the trim switch must be pressed
30
What does the trim speed bug indicate in normal mode?
HSTAB trim speed setting
31
What happens to the trim speed bug when the autopilot is engaged?
It is removed from the airspeed tape
32
How is the HSTAB trimmed in FBW direct mode?
Manually with the pitch trim switch
33
Where is the backup STAB trim switch located?
TRIMS panel on center pedestal
34
What does the STAB TRIM FAIL CAS message indicate?
Horizontal stabilizer trim has failed
35
How is momentary sidestick priority activated?
AP PTY pushbutton on sidestick
36
What does latched sidestick priority do?
Disables opposite sidestick until reset
37
What surfaces make up the secondary flight controls?
MFSs GSs HSTAB
38
What lever provides manual control of the MFSs?
FLIGHT SPOILER lever
39
How many multifunction spoilers are on each wing?
Three
40
What are the three functions of the MFSs?
Roll assist speed braking ground lift dumping
41
How are MFSs actuated?
Single PCU on separate hydraulic systems
42
What happens to MFSs when thrust levers are advanced above 20 degrees in normal mode?
They automatically retract
43
What command input devices are used by pilots for flight controls?
Sidesticks rudder pedals FLIGHT SPOILER lever trim switches
44
What is the primary function of the SLAT FLAP lever?
Controls high lift surfaces
45
What is the backup method for extending slats and flaps?
ALTN FLAP guarded PBA
46
How many slats and flaps are on each wing?
Four slats two flaps
47
What powers the high lift system?
Electric motors
48
What does the FLT CTRL synoptic display?
Position and status of all major flight control surfaces
49
What does a green symbol on the synoptic indicate?
Surface is operational
50
What is the function of the airplane response monitor ARM?
Compares airplane attitude with FBW envelope limits
51
What happens if an ARM trigger point is exceeded for more than one second?
FBW degrades to REU direct mode
52
What triggers the transition to PFCC direct mode?
Loss of air data or inertial inputs to all three PFCCs
53
Which direct mode allows manual deployment of MFS after landing?
REU direct mode
54
What protection is lost in all FBW direct modes?
Full flight envelope protection
55
Which CAS message appears in REU direct mode?
FLT CTRL DIRECT
56
How many hydraulic PCUs operate per surface in AFCU direct mode?
One PCU per surface