时间：2012-10-30 12:45来源：蓝天飞行翻译 作者：航空 点击：次
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PRESSURE REFUELING SYSTEM INFORMATION USE OF PORTABLE ELECTRONIC DEVICES ABOARD EMB-145, ERJ-140 AND EMB-135 AIRPLANES HIGH-SPEED OPERATION CIRCUIT BREAKER RESETTING GUIDELINES FOR AUTOPILOT APPROACHES TRANSPONDER COMMUNICATION FAILURE CONTACTOR SWITCHING NOISE ASSOCIATED WITH UNUSUAL GENERATOR INDICATION PRESSURE REFUELING SYSTEM INFORMATION WINDSHIELD STRUCTURAL AND NONSTRUCTURAL LAYERS FAILURE DIFFERENTIATION THALES ISIS MIRROR EFFECT AT POWER UP LAVATORY DOOR UNLOCKING PROCEDURES ELECTRICAL LOADS LOSS ASSOCIATED WITH ENGINES SHUT DOWN LG/LEVER DISAGREE EICAS MESSAGE WITH THREE GREEN LANDING GEAR POSITION INDICATION TAILPLANE DEICING/ANTI-ICING EGPWS WARNING DURING QFE OPERATION ELECTRICAL EMERGENCY ABNORMAL EICAS MESSAGE DUE TO ROTARY SWITCH INTERNAL SHORT CIRCUIT CDU DATA BUS FAIL MESSAGE EFFECTS ON EGPWS UNRELIABLE AIRSPEEDS DU-875 MISBEHAVIOR MEL RESTRICTION DUE TO DU-875 P/N K9321060A10 (REVISION 03 AND HIGHER) FAILURE RATE INCREASE |
