baconsmuggler

During departure when Wing A-Ice is selected ON ENG1 and ENG2 bleed faults are triggered. The BLEED page shows 0psi bleed pressure from both engines and both IP and HP valves are closed (XBLEED switch is set to AUTO): Switching off Wing anti-ice returns the bleed system to a normal state: Wing anti-ice can only be selected on when the xfeed valve is setting is changed from AUTO to CLOSE: This appears to be a bug since it is not necessary to close the xbleed valve for wing anti-ice to be available; It remains closed except for engine start, on ground and a few other situations. When both engines, packs and bleed systems are operating normally it's closed with the xbleed selector switch in the AUTO position.

(on V1.0.4) After a flight time of ~ 4:45h the FU figures for both engines differ significantly: The FU value for ENG2 is roughly within expected limits but the value for ENG1 is far too low. Apart from 2 IFSD events for less than 1 minute on ENG1 both engines have been simultaneously during the flight. EDIT: Cycling the ENG MASTER switch in flight resets the fuel used figure for the engine. (Normal on ground but not in flight)

1 - Quick relight function: Currently the A/C doesn't perform a quick relight, the ENG START selector has to be set to IGN/START manually and the complete startup sequence is initated just like on the ground. 1.1 - Windmilling start: In reference to point 1, windmilling start is currently not working. With IAS above 250kt and N3 well above 6% the ENG START selector has to be set to the IGN/START position in order to relight the engine, i.e. a complete start sequence has to be initiated. 2 - Continuous ignition: When setting the ENG START switch to IGN/START during flight no continuous ignition is taking place, the ENG SD page shows no ignition indication (should show both igniters A and B) and no associated IGNITION memo is displayed.

When leaving TCAS in STBY mode a master caution with associated ECAM message should be triggered after the T.O. inhibition phase.