A330F Test

A runaway is given as a positional differential between both APPU and FPPU (i.e. broken output shaft). The SFCCs monitor the system for runaway. If a SFCC detects a runaway it does the same actions as an asymmetry. True. False.

Which of the following LRUs can only compute Normal control laws?. FCPCs. PRIM and SEC. FCSC.

Where are shown all indication of Flight control system?. Upper ECAM NDs Flight control page. ECAM SD flight control page. ECAM SD Wheel page.

When the function of WTB hold the transmission?. The WTBs stop and hold the transmission if the FCPCs detect some type of failures such as, runaway or over speed and uncommanded. The WTBs stop and hold the transmission if the SFCCs detect some type of failures such as asymmetry, runaway or POB fail. The WTBs stop and hold the transmission if the SFCCs detect some type of failures such as asymmetry, runaway, over speed and uncommanded movement.

Which computers are the interfaces between EIS and primary, secondary computers?. FCPCs. FCSCs. FCDCs.

The THS mechanical control can be used: On ground, for maintenance or take-off trim setting. & in flight, as a standby system if automatic control (autotrim) is not available. In flight, for maintenance or take-off trim setting & in flight, as a standby system if automatic control (autotrim) is not available. On ground, for maintenance or take-off trim setting. & not use in flight.

A third mode sets the elevator surfaces in neutral position in case of specific failure it is called?. Active mode. Re-centering mode. Damping Mode.

How is the THS powered?. By 3 electric motors. By 2 hydraulic motors. By 3 hydraulic actuators.

The Backup Control Module (BCM) is an electronic module, which fulfills: The roll control in case of flight control computer failures. The pitch control in case of flight control computer failures. The yaw control in case of flight control computer failures.

The THS is controlled by: Controlled FCSCs and override by FCPC control through the trim wheels. Controlled FCPCs and override electrical control through the trim wheels. Controlled FCPCs and override mechanical control through the trim wheels.

MLA function raises symmetrically the ailerons and the spoilers ______?. 4,5,6. 2 to 5. 1 to 6.

here are installed the WTBs?. Slat 7RH and 14LH in track 16. Slat 7RH and 7LH between track 15 and installed on the PCU. Slat 7RH and 7LH between track 15 and 16 installed on the transmission.

What is the surface that helps the aircraft to perform the LIFTH DUMPING?. Flaps. Spoilers. Elevators.

Why should the Side Stick assembly be kept in vertical position during maintenance procedures?. Risk of disengaged laterally. Risk of skydrol leakage. Risk of damage of mechanical parts.

At HIGH SPEED (Vc higher than190 kt), in clean configuration (slat/flap Retracted) the outboard ailieron ar servoed to zero. True. False.

What conditions are required to activate the partial lift dumping logic?. A/C on ground with both MLG compressed, ground spoiler armed or reverse selection. A/C on ground with one MLG compressed, both throttles at idle, at least one thrust lever in reverse, ZRA 5ft or below. A/C on ground with one MLG compressed, both throttles at idle, at least one thrust lever in reverse, ZRA lower than 6ft and wheel speed higher than 72 KTS.

There are two servo controls for each aileron and elevator surface. In normal Configuration, one servo control actuates the surface. Which is this mode?. Active Mode. Damping Mode. Recentering Mode.

Which is the procedure to extend the spoilers for maintenance; install the spoiler maintenance key in the maintenance device and: Turn it in the "O" position. Turn it in the "M" position. Turn it in the "Y" position.

If a Checkeable Shear Pin (CSP) is actuated and failure message is displayed on ECAM, What does it means?. THS is operating at 50%. Secondary Load Pad engaged. THS is uncommanded.