![]() So, if the weather at our destination is below CAT I, this can lead to a diversion. ![]() The main consequence here is that we have only one autopilot left so we are restricted to CAT I landing as we need both autopilots for a CAT III approach (autoland). With a total loss of hydraulic system B, autopilot B is not available anymore. Thrust reverser will deploy and retract at a slower rate and some thrust asymmetry can be anticipated during thrust reverser deployment. Once extended, they can not be retracted.Įngine 2 thrust reverser normal hydraulic pressure The leading edge flaps can be extended with standby pressure. Leading edge flaps and slats normal hydraulic Alternate flap extension time to flaps 15 is approximately 2 minutes. The trailing edge flaps can be operated with the alternate electrical system. Trailing edge flaps normal hydraulic system Roll rate and speed brake effectiveness may be reduced in flight
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