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) Engine-driven alternators ¦
¦ ¦ ¦ ¦ and both converters are ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) APU Alternator is operative, ¦
¦ ¦ ¦ ¦ c) Associated Battery Charger ¦
¦ ¦ ¦ ¦ circuit breaker on the Power ¦
¦ ¦ ¦ ¦ Distribution Box is pulled ¦
¦ ¦ ¦ ¦ and collared, and ¦
¦ ¦ ¦ ¦ d) Standby Electrical System is ¦
¦ ¦ ¦ ¦ operative. ¦
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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 ¦ 24-4 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 6. Main Airplane B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ Batteries ¦ ¦ ¦ a) Airplane is operated in day ¦
¦ ¦ ¦ ¦ VMC, ¦
¦ ¦ ¦ ¦ b) There are no other ¦
¦ ¦ ¦ ¦ electrical power source ¦
¦ ¦ ¦ ¦ failures, ¦
¦ ¦ ¦ ¦ c) Associated Battery cables ¦
¦ ¦ ¦ ¦ are disconnected and ¦
¦ ¦ ¦ ¦ secured, ¦
¦ ¦ ¦ ¦ d) Associated Battery Charger ¦
¦ ¦ ¦ ¦ circuit breaker on the Power ¦
¦ ¦ ¦ ¦ Distribution Box is pulled ¦
¦ ¦ ¦ ¦ and collared, and ¦
¦ ¦ ¦ ¦ e) Associated battery circuit ¦
¦ ¦ ¦ ¦ breaker is pulled and ¦
¦ ¦ ¦ ¦ collared. ¦
¦ ¦ ¦ ¦ ¦
¦ 7. SEL/AUTO Buttons C ¦ 6 ¦ 5 ¦ (O)One may be inoperative provided ¦
¦ on EPMP ¦ ¦ ¦ affected bus is manually selected ¦
¦ ¦ ¦ ¦ ON. ¦
¦ ¦ ¦ ¦ ¦
¦ 8. Battery Ammeters C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦
¦ ¦ ¦ ¦ a) The associated voltmeter is ¦
¦ ¦ ¦ ¦ operative, and ¦
¦ ¦ ¦ ¦ b) Both battery charger fail ¦
¦ ¦ ¦ ¦ lights are operative. ¦
¦ ¦ ¦ ¦ ¦
¦ 9. Battery Voltmeters C ¦ 2 ¦ 1 ¦ One may be inoperative provided ¦
　
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