曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

¦ ¦ ¦ ¦ a) Both Engine Driven ¦
¦ ¦ ¦ ¦ Alternators are operative, ¦
¦ ¦ ¦ ¦ b) Both Converters are ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ c) TRU is operative, ¦
¦ ¦ ¦ ¦ d) Standby Electrical System is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ e) Procedures do not require | ¦
¦ ¦ ¦ ¦ its use, | ¦
¦ ¦ ¦ ¦ f) APU Alternator 115 VAC | ¦
¦ ¦ ¦ ¦ circuit breaker is pulled | ¦
¦ ¦ ¦ ¦ and collared, and | ¦
¦ ¦ ¦ ¦ g) APU is operated on ground | ¦
¦ ¦ ¦ ¦ only. | ¦
¦ ¦ ¦ ¦ | ¦
¦ ¦ ¦ ¦ NOTE: APU may be used as a | ¦
¦ ¦ ¦ ¦ pneumatic source. | ¦
¦ ¦ ¦ ¦ | ¦
¦ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided APU | ¦
¦ ¦ ¦ ¦ is not utilized. | ¦
¦ ¦ ¦ ¦ ¦
¦ 3. Converters B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ ¦ ¦ ¦ a) TRU is operative, ¦
¦ ¦ ¦ ¦ b) APU Alternator is used for ¦
¦ ¦ ¦ ¦ takeoff, enroute and ¦
¦ ¦ ¦ ¦ landing, and | ¦
¦ ¦ ¦ ¦ c) Airplane is operated at or | ¦
¦ ¦ ¦ ¦ below FL 300 or up to FL 350 | ¦
¦ ¦ ¦ ¦ and below with Electrical | ¦
¦ ¦ ¦ ¦ Load Warning System (ELWS) | ¦
¦ ¦ ¦ ¦ installed or ASC 420 | ¦
¦ ¦ ¦ ¦ installed. | ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 10/11/2001 ¦ 24-3 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 4. Transformer- B ¦ 1 ¦ 0 ¦ (M)May be inoperative provided: ¦
¦ Rectifier ¦ ¦ ¦ a) Both Converters are ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) APU Alternator is operative, ¦
¦ ¦ ¦ ¦ c) Both Battery chargers are ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ d) Both Main Airplane Batteries ¦
¦ ¦ ¦ ¦ are operative, and ¦
¦ ¦ ¦ ¦ e) TRU (R-AC) circuit breaker ¦
¦ ¦ ¦ ¦ on the Power Distribution ¦
¦ ¦ ¦ ¦ Box is pulled and collared. ¦
¦ ¦ ¦ ¦ ¦
¦ 5. Battery Chargers B ¦ 2 ¦ 1 ¦ (M)One may be inoperative provided: ¦
　
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