时间:2012-10-14 13:07来源:蓝天飞行翻译 作者:航空 点击:次
Engine bleed valve reset in case of BLEED LEAK EICAS message due to overpressure peaks Flight controls reversion to direct mode and the associated recovery procedures Autoflight high commands during ILS captures STEER FAIL EICAS message displayed under some conditions Mismatch of all airspeed indications Temperature adjustment with single pack operation AP quick disconnect button malfunctions Mode S transponder reversion to standby mode Radio Altimeter misbehavior BLEED FAIL due to REF ECS OFF Aileron control stiffness Differences in the Cabin Pressurization System’s operation in AUTO and MAN mode ENG EXCEEDANCE occurrence due to engine vibration Dual BLEED overpressure events Engine chevron nozzle oil puddle Thrust reverser deployment techniques Guidelines on brake use during taxi Combined bleed overpressure and leak events ENG EXCEEDANCE occurrence due to engine vibration |