Airbus A330 and A340 Flight Crew Training Manual

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This mode only operates automatically during an autoland. The thrust levers must be retarded manually in the flare following a manual approach. 3 REV 1 (6 JUN 05) When armed, the A/THR is ready to control the thrust once the thrust levers are moved into the active range. Normally the A/THR is armed on the application of take-off thrust, at which point "A/THR" is displayed in blue in the right hand column of the FMA. After take-off, A/THR is activated by selecting the thrust levers to the CL detent.

With reference to the diagram below, if a dive is achieved with stick free, the aircraft will slightly overshoot VMO/MMO and fly back into the flight envelope. If a dive is achieved with the sidestick fully forward, the aircraft will significantly overshoot VMO/MMO but without reaching design speed limits, VD/MD. 9 REV 1 (6 JUN 05) When high speed protection is triggered, the autopilot disconnects, the pitch trim is frozen, the spiral static stability is reduced from 33° to 0° of bank and the limit bank angle is reduced from 67° to 45°.

Ensure that the main aircraft control surfaces are in the correct position relative to cockpit control selection and that there is n o evidence of fuel, oil or hydraulic leaks. g. AOA, pitot and static probes. g. wheel/tyre condition, safety pins removed, brake wear, and oleo extension. g. fan blades, turbine exhaust, engine cowl and pylon status. Check all access panels are closed. 05 refers COCKPIT TO GROUND COMMUNICATION It is essential that good communication is established with the ground personnel prior to engine start or pushback.

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