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¦ 1) EICAS or C ¦ 1 ¦ 0 ¦ (M)(O)Either Left or Right Fuel ¦
¦ Standby ¦ ¦ ¦ Quantity display may be inoperative ¦
¦ ¦ ¦ ¦ provided: ¦
¦ (cont'd) ¦ ¦ ¦ a) Affected tank is defueled ¦
¦ ¦ ¦ ¦ before each refueling, ¦
¦ ¦ ¦ ¦ b) Affected tank is fueled with ¦
¦ ¦ ¦ ¦ a known quantity of fuel, ¦
¦ ¦ ¦ ¦ c) Both fuel flow meters are ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ d) After takeoff, power is set ¦
¦ ¦ ¦ ¦ by matching fuel flow ¦
¦ ¦ ¦ ¦ indications on both engines, ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ e) Flight crew maintains a log ¦
¦ ¦ ¦ ¦ of fuel burned. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ NOTE: Total fuel indication will ¦
¦ ¦ ¦ ¦ be incorrect with an ¦
¦ ¦ ¦ ¦ inoperative indicator. ¦
¦ ¦ ¦ ¦ ¦
¦ 3. Fuel Low Quantity C ¦ 2 ¦ 0 ¦ (O)Both may be inoperative ¦
¦ Warning Systems ¦ ¦ ¦ provided: ¦
¦ (EICAS - Message) ¦ ¦ ¦ a) Both Fuel Quantity ¦
¦ (Standby Indicator ¦ ¦ ¦ Indicating Systems are ¦
¦ Lights) ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) All Fuel Boost Pumps are ¦
¦ ¦ ¦ ¦ operative, and ¦
¦ ¦ ¦ ¦ c) Fuel Crossflow Valve is ¦
¦ ¦ ¦ ¦ OPENED when either wing tank ¦
¦ ¦ ¦ ¦ contains 2,000 pounds or ¦
¦ ¦ ¦ ¦ less fuel. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 10/11/2001 ¦ 28-3 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 28 FUEL ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 4. Fuel Boost Pumps C ¦ 4 ¦ 3 ¦ (O)One may be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Fuel Crossflow Valve is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) Fuel Intertank Valve is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ c) Both Fuel Low Quantity ¦
¦ ¦ ¦ ¦ Warning Systems are ¦
¦ ¦ ¦ ¦ operative, and ¦
¦ ¦ ¦ ¦ d) Airplane is operated in ¦
¦ ¦ ¦ ¦ accordance with AFM ¦
¦ ¦ ¦ ¦ Limitations. ¦
¦ ¦ ¦ ¦ ¦
¦ 5. Fuel Intertank C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Valve ¦ ¦ ¦ a) All Fuel Boost Pumps are ¦
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湾流4主最低设备清单MMEL GULFSTREAM G-IV Master Minimum Equip(43)
