The priority logic of the elevators control is: 27-001
a. ELAC2, ELAC1, SEC2, SEC1
b. ELAC1, ELAC2
c. ELAC1, SEC1, ELAC2,SEC2
Aircraft in flight, first the Pilot’s side stick is moved forward, second F/O side stick is moved in the same direction, what will happen with deflection angle electrical signals from the both side sticks. 27-003
a. The flight control system ignores the signals from F/O side stick.
b. The resulting surface movement is the difference between electrical signals.
c. Flight control system summarizes that electrical signals.
In flight when Normal Low is present, Rudder is electrically controlled by? 27-036
a. Flight Augmentation Computer (FAC) #1. 56p.
b. FAC#2
c. FAC#3
22.We can reset the Wing Tip Brakes (WTB)… 27-071
a. in flight by the switch “WTB RESET” on the overhead panel.
b. manually by the FLAPS lever on the ground only.
c. on the ground through the CFDS only. 168p.
Will the ailerons be controlled if the Elevator Aileron Computers (ELAC#1 and ELAC#2) are failed? 27-008
a. No, it will not. All ailerons are in the damping mode in this case.
b. The Flight Augmentation Computers (FAC's) control the ailerons in this case.
c. The Spoiler Elevator Computers (SEC's) generate the ailerons deflection depending on side stick controller signals in this case .
When you press RESET P/B SWITCH on the RUDER TRIM CONTROL PANEL: 27-019
a. Rudder automatically is positioned to the zero position
b. RUDER TRIM is not available any more, but the RUDDER PEDALS is available to control the rudder
c. RUDDER PEDALS is not available but RUDER TRIM is available to control the rudder
The available modes of the aileron servo actuator are: 27-065
a. Active and centering modes.
b. Active and damping modes.
c. Active, damping and centering modes.
Which spoilers are used as the Speed Brakes? 27-074
a. Spoilers 2 to 4 are used as the Speed Brakes.
b. Spoilers 1 to 5 are used as the Speed Brakes.
c. Spoilers 1 to 2 are used as the Speed Brakes.
Under what condition the A/C starts to operate on FLARE Mode? 27-011
a. When the A/C passes 30 ft RA
b. 8 second after A/C passes 30 ft RA
c. When the A/C passes 50 ft RA
In the event of a loss of the electrical control of the one servo controls of a elevator surface: 27-012
a. The elevator surface is brought in the centering position
b. The elevator surface stays and is held in the last position
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c. The elevator surface is still controlled by adjacent servo control.
Which mode has the spoiler actuator if the hydraulic pressure is lost? 27-009
a. There is damping mode. The spoiler panel can be moved to retract and to extend positions by the aerodynamic forces.
b. There is locked mode. The spoiler panel can only be moved towards the retracted position, pushed by the aerodynamic forces.
c. There is biased mode. The spoiler panel retracts electrically.
What will happen with the Trimmable Horizontal Stabilizer (THS) control in case of total loss of the green and yellow hydraulic pressure? 27-062
a. The THS will have an ability to be controlled by the Pitch Trim Actuator electric motors.
b. The THS will have an ability to be controlled by the manual control.
c. The THS will be kept in the last specified position without any ability to be controlled.
31. The available modes of the aileron servo actuator are:
a. Active and centering modes.
b. Active and damping modes.
c. Active, damping and centering modes.
What flight control law is introduced if the aircraft is on the ground? 27-067
a. Direct Law.
b. Alternate Law.
c. Normal Law.
The Rudder can be manually operated in case of loss of all the three hydraulic systems. Is it truth?
a. Yes.
b. No.
c. Yes, it is possible by the Rudder electrical trimmer.
ATA 27A. FLIGHT CONTROLS System Operation:
Electrical/Fly-by-Wire (LVL 3)
If both ELACs fail, what controls the elevator and stabilizer? 27A-012
a. SEC 1 or 2 depending of the status
b. Elevator and stabilizer revert to mechanical backup
c. Backup mode of ELAC's
In the event of electrical control loss of one servo controls of elevator surface: 27A-007
a. The elevator surface stays and is held in the last position
b. The elevator surface is brought back in the 0 zero position
c. The elevator surface is still controlled by adjacent servo control.
ATA 25. Equipment and Furnishing (LVL 3)
What components have each floor heated panel on emergency exit door? 25-001
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a. the temperature sensor and two safety switches, the insulation material, the heating foil, the aluminum outer cover plate, two drain holes
b. the control unit, two LED’s, the temperature sensor and two safety switches
c. the temperature sensor and two safety switches, the heating foil, the control unit, two LED’s, two fuses, C/B panel, relay panel.
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