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Additional info for Airbus A330 and A340 Flight Crew Training Manual
Nose-up with thrust increase and nose down with thrust reduction. In pitch, elevator deflection is proportional to sidestick deflection. It is important to note that the controls are very powerful. Consequently, use small inputs when at high speed. As there is no auto-trim, use manual trim making small inputs on the trim wheel. In roll, aileron and spoiler deflection is proportional to sidestick deflection. Direct law works with the yaw damper to provide a minimal turn coordination. Protections No protections are available but overspeed and stall aural warnings remain available.
The downwind track should be set on the FCU. Place the tail of the bird on the blue track index on the PFD to maintain the desired track downwind. On the final inbound approach, the track index should be set to the runway final approach course. A standard 3° approach path is indicated by the top of the bird's tail being just below the horizon and the bottom of the bird being just above the 5° pitch down marker. 4 REV 1 (6 JUN 05) A330/A340 FCTM General Information Flight Path Vector FPV CONSIDERATIONS Dynamic Manoeuvres The pilot must take care when performing a go-around with the FPV selected, as on some aircraft the HDG-V/S FD is not automatically displayed upon the selection of TOGA.
Any tendency to roll stick free can be corrected by conventional use of the rudder. Rudder trim can be used in the conventional way, but note that the sideslip index may be slightly displaced from the centre once the rudder forces have been trimmed out. e. nose-up with thrust increase and nose down with thrust reduction. In pitch, elevator deflection is proportional to sidestick deflection. It is important to note that the controls are very powerful. Consequently, use small inputs when at high speed.