Under what condition the A/C starts to operate on FLARE Mode? 27-011
Nbsp; Content checked IAW course syllabus by responsible examiner: _________________ _____________________ Name Signature/ Stamp Course reference: A320F(CFM56) B1.1 + B2 Training session: 4 ATA Chapters: VAR.2 51-57/29/29A/27/27A/25/25A Exam: X Re-Exam: Candidate`s name: Signature:
ATA 25. Equipment and Furnishing (LVL 3)
What do we have to do to inflate the off-wing emergency exit escape slide on the A-320? 25-015
a. We have to remove one of the emergency hatches.
b. We have to remove one of the emergency exit handle cover.
c. We have to remove all right-hand or all left-hand emergency exit hatches respectively.
How can you check the life vests presence in the Capitan and First Officer seats?25-002
a. By means of the life vest check indicator on the seat armrest.
b. By means of opening life vest compartment in the seats only.
c. By means of life vest check window on the aft sets back.
What components have each floor heated panel on emergency exit door? 25-001
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.
How can you control the position of the Capitan and First Officer seats in different direction? 25-003
a. only manually
b. only electrically
c. electrically and manually
ATA 25A. Electronic Equipment
Including emergency equipment (LVL 3)
5.Heated floor panel system… 25A-009
a) is switched on manually from the Flight Attendant Panel (FAP)
b) comprises two overtemperature switches (55°C & 70°C)
c) temperature regulation is set manually by the flight attendant
ATA 27. FLIGHT CONTROLS (LVL 3)
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 .
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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
c. The elevator surface is still controlled by adjacent servo control.
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.
What flight control law is introduced if the aircraft is on the ground? 27-067
a. Direct Law.
b. Alternate Law.
c. Normal Law.
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
12.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.
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 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.
The available modes of the aileron servo actuator are: 27-065
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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
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