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¦ AIRCRAFT: ¦ REVISION NO: 4 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 05/31/1996 ¦ 77-2 ¦
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¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 77 ENGINE INDICATING ¦ ¦ ¦ ¦
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¦ 6. Standby Engine C ¦ 1 ¦ 0 ¦ May be inoperative provided ¦
¦ Instruments ¦ ¦ ¦ associated EICAS indications are ¦
¦ Indicating System ¦ ¦ ¦ operative. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ NOTE: Individual standby ¦
¦ ¦ ¦ ¦ indications may be ¦
¦ ¦ ¦ ¦ inoperative provided ¦
¦ ¦ ¦ ¦ associated EICAS indication ¦
¦ ¦ ¦ ¦ is operative. See ¦
¦ ¦ ¦ ¦ individual indications for ¦
¦ ¦ ¦ ¦ other authorized ¦
¦ ¦ ¦ ¦ configurations. ¦
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 4 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 05/31/1996 ¦ 78-1 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 78 ENGINE EXHAUST ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 1. Thrust Reverser C ¦ 2 ¦ 1 ¦ (M)One may be inoperative provided ¦
¦ Arm Lights (Green) ¦ ¦ ¦ the associated REV UNLOCK message ¦
¦ ¦ ¦ ¦ on the EICAS is verified to be ¦
¦ ¦ ¦ ¦ operative. ¦
¦ ¦ ¦ ¦ ¦
　
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