The A 330 is in a slight climb in normal law; immediatly after the pilot releases the stickto neutral, the flight controls will :
B.
All flight controls are actuated by hydraulic servos which are controlled by computers :
A.
All flight controls are :
B.
The A 330 is being hand flown in normal law. It is established in a 20° left bank turn,to maintain the altitude, the pilot :
A.
Your A 330 is in level flight in normal law, with stick released and airspeed slowed by 20 kt, the flight controls will :
C.
THS auto trim function is active :
B.
THS auto trim function is neutralized when :
B.
On A 330, pitch attitude protection limits pitch attitude of the aircraft to :
C.
On A 330, G Load protection limits G Load of the A/C to :
A.
Your A 330 is in a 45° bank turn and has entered high speed protection; if the stick is released to neutral protection, the A/C will :
A.
You fly your A 330 in a high pitch climb (AP disengaged); airspeed is dropping close to alpha max; if you maintain the sidestick in the full aft position :
C.
If alarm " SPEED SPEED SPEED " sounds in the cockpit :
A.
You fly your A 330 in level flight (AP disengaged) in alternate law 1 ; idle power is selected and sidestick is free :
C.
You fly your A 330 in descent (AP disengaged) in alternate law 1 ; airspeed becomes greater than VMO/MMO :
B.
If red message " MAN PITCH TRIM ONLY " appears on PFD :
B.
When the A 330 is hand flown, on normal law, with A/THR on speed mode, high angle attack protection :
B.
Amber message " USE MAN PITCH TRIM " appears on PFD :
B.
Loss of hydraulic power to one of the single spoiler servos will cause that surface to :
A.
Aileron droop :
C.
In case of loss of electrical power on PRIM 1, the corresponding spoiler(s) will :
A.
You select FLAP 1 in TAKE OFF PERF page in the MCDU, and you select flaps 2 selector :
"FLAP/MCDU DISAGREE" will happen.
C.
When the RAT is extended to recover hydraulic or electrical power, the servo jacks that revert to damping mode, control :
C.
Normal pitch control uses :
control motor.
A.
If neither PRIM 1 or PRIM 2 are available, pitch control is transferred to :
A.
If all three PRIM computors are failed :
C.
With yaw damping or turn coordination functions :
A.
You fly your A330 in steady FL, with ADR 1 + 2 failure :
B.
When hydraulic failure occurs, the associated slats and flaps :
B.
When retracting slats from 1 to 0 position, if A - LOCK message appears on EW/D, it means :
B.
The sidesticks are used to :
to the neutral position.
C.
The " RESET " p/b on the rudder trim control panel, when pushed :
A.
The use of the manual trim wheel is :
A.
In normal operations, roll control is made by :
C.
Which are required for Manoeuver Load Alleviation (MLA) ?
C.
Amber ECAM message " F/CTL FLAPS LOCKED " means :
C.
Pitch control is provided by :
B.
The ailerons are each actuated by :
B.
The speed brakes surfaces are :
C.
Each ELEVATOR servo jack has :
B.
ON elevators, if an active servo jack fails, the damped one becomes active. What happens to the failed jack ?
C.
The AP function is lost in case of :
C.
Each SEC provides at least :
A.
If one hydraulic system is inoperative :
B.
Ground spoilers extension may be done :
A.
The SIDE STICK PRIORITY signal is flashing green, it means :
C.
Speed brakes lever has been set to " ARM " position; during an abort take off over 72 kts, to extend the speed brakes, it is necessary for the pilot to :
A.
The pilot forgot to set Speed brakes Lever to " ARM " position; when landing, ground spoilers will :
A.
In flight, with FLAP 1 configuration, in order to select FLAPS 2 :
A.
Today, your A 330 is very heavy, and " S " speed is above 215 kts; during initial climb, when airspeed reaches 200 kts, if you don't touch the flap handle :
C.
When landing, reverse thrust selected at least on 1 Engine (other thrust at idle),
if one main landing gear is compressed :
C.
If " RELIEF " appears blinking on the EW/D :
A. Flaps will automatically retract to the next position because the flap load relief
function is active.
B. You have to retract flaps otherwise a flap overspeed will occur.
C. You may extend flaps to the next position.
A
In flight, speed brakes cannot be detend if :
A.
All A330 flight controls are actuated by hydraulic servos which are controlled by computers:
C.
The autopilot will disconnect if the side stick takeover push button is depressed.
A. True.
B. False.
A
Ailerons are deflected down when flaps are:
A. Extended.
B. Retracted.
A
Flight control normal law provides:
D.
The rudder is actuated by _____ independent hydraulic jacks which operate in parallel.
D.
Which of the following statements is correct concerning the side stick takeover push button?
B.
Are there any control surfaces with a mechanical backup?
B.
Which of the following will automatically reset after landing?
A.
The alpha speed lock function:
C.
In normal law, if one stick is rapidly pulled fully back, can the aircraft's maximum allowable 'G' load be exceeded?
A.
Each aileron hydraulic servojack has two control modes: active and damping.
A. True.
B. False.
A
Which controls are used for the mechanical backup?
A.
Mechanically backed-up control surfaces:
A.
Selection of flaps one prior to takeoff will select which of the following?
A.
Which of the following statements best describes the Maneuver Load Alleviation function (MLA)?
C.
When ground spoilers deploy automatically:
A.
The slats alpha / speed lock function inhibits slats retraction at high angle-of-attack and/or low speed.
A. True.
B. False.
A
Each SEC provides at least:
C.
Which altitude limitation is associated with high lift devices?
D.
The message WING TIP BRK ON appears on the E/WD. What does it mean?
B.
Where does the SFCCs obtain AOA and air data information from?
D.
The wing tip brakes, once activated:
D.
Which of the following controls and monitors flaps and slats?
C.
The spoiler panels are the only flight control surfaces with no redundant control.
A. True.
B. False.
A
What happens in the side stick-neutral high speed protection mode?
B.
Can the crew make a flight control input that will over-stress the airplane in direct law?
A. No. The system is designed to avoid such an attempt.
B. Yes, there are no protections provided in direct law.
B
The stabilizer is actuated by a screw jack driven by two hydraulic motors, which in turn are controlled by:
A.
Can you manually trim the rudder with the autopilot engaged?
A. Yes.
B. No.
B
When is the Flight Mode active?
D.
OVERSPEED ECAM warning is provided at:
B.
Automatic pitch trim is provided both on ground and in flight.
A. True.
B. False.
B
The Ground Mode is different in Alternate Law.
A. True.
B. False.
B
In normal law, what is the maximum bank angle you can reach with the side stick fully deflected?
B.
Failure to retract the flaps after takeoff will:
C.
MLA (maneuver load alleviation) becomes active when side stick is pulled less than 8 degrees and the load factor is more than 2 g.
A. True
B. False.
A
SFCC generated slat and flap extension, retraction, and limiting speeds are visually displayed on which of the following?
C.
The wing tip brakes are:
A.
Selection of flaps 1 in flight will select which of the following configurations?
C.
The aircraft rudder can be manually trimmed with the autopilot engaged.
A. True.
B. False.
B
What happens if you release the stick at 40 degrees of bank?
A.
The elevators are ______ controlled.
A. Mechanically.
B. Electrically.
B
When is alpha floor not available?
D.
What kinds of protections are provided if the aircraft is in Alternate Law?
D.
In Normal Law, what are the limits of Pitch Attitude protections with flaps Full
D.
The rudder trim rotary switch is not active when autopilot is engaged.
A. True
B. False.
A
You can degrade directly from Normal Law to Direct Law with gear down and a dual radio altimeter fault.
A. True.
B. False.
A
Turn coordination is available in Alternate Law.
A. True.
B. False.
B
If both pilots deflect their side sticks fully back:
D.
To disable a side-stick, you have to depress the red take-over button on the active stick. Holding the button down for 40 seconds will electrically lock the other stick out until its own red take-over button is pushed again.
A. True.
B. False.
A
Let's assume the F/O presses his takeover pushbutton and releases it after more than 40 seconds.
D.
The speed brakes are _____ controlled.
A. Electrically
B. Mechanically
A
Ailerons max deflection is:
D.
What happens to the rudder limits if both SEC's fault?
C.
What happens to high speed (VMO/MMO) when you are in Alternate Law?
D.
If all three PRIM computers are not available with B or Y hydraulic system available:
A.
In flight, spoilers max deflection is:
A.
The FLAP lever sends signal to Slat Flap Control Computer (SFCC) to command movement.
A. True.
B. False.
A
When the RAT is extended to recover hydraulic pressure or electrical power, the servo jacks that revert to damping mode control:
A. The outboard ailerons.
B. The inboard ailerons.
A
The speedbrake surfaces are:
C.
The autopilot function is lost in case of:
C.
Each PRIM provides:
B.
For elevators control, each servo jack has:
C.
When you set rudder trim, the input:
A.
Loss of hydraulic power to one of the single spoiler servos will cause that surface to:
