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¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 73 ENGINE FUEL & CONTROL ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 1. Fuel Flow B ¦ 2 ¦ 1 ¦ (M)One may be inoperative provided: ¦
¦ Indication Systems ¦ ¦ ¦ a) Associated EPR, LP and HP ¦
¦ (EICAS) ¦ ¦ ¦ indicating systems are ¦
¦ ¦ ¦ ¦ operative, and ¦
¦ ¦ ¦ ¦ b) Fuel Quantity Indicating ¦
¦ ¦ ¦ ¦ Systems are operative. ¦
¦ ¦ ¦ ¦ ¦
¦ 2. Engine Top C ¦ 2 ¦ 0 ¦ (O)Both may be inoperative provided ¦
¦ Temperature Control ¦ ¦ ¦ TGT is monitored and manually ¦
¦ Systems ¦ ¦ ¦ controlled to appropriate limits. ¦
¦ ¦ ¦ ¦ ¦
¦ 3. Fuel Low Pressure C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ Warning Systems ¦ ¦ ¦ a) Associated fuel boost pumps ¦
¦ (EICAS and Standby) ¦ ¦ ¦ are operative, and ¦
¦ ¦ ¦ ¦ b) Airplane is operated at or ¦
¦ ¦ ¦ ¦ below FL 250. ¦
¦ ¦ ¦ ¦ ¦
¦ 4. Approach Idle C ¦ 2 ¦ 0 ¦ (M)(O)Both may be inoperative ¦
¦ Systems ¦ ¦ ¦ provided: ¦
¦ ¦ ¦ ¦ a) Both Systems are de- ¦
¦ ¦ ¦ ¦ energized (Approach Idle ¦
¦ ¦ ¦ ¦ Mode), ¦
¦ ¦ ¦ ¦ b) Both Systems are in the ¦
¦ ¦ ¦ ¦ Approach Idle Mode, and ¦
¦ ¦ ¦ ¦ c) Field length requirements ¦
¦ ¦ ¦ ¦ for takeoff and landing are ¦
¦ ¦ ¦ ¦ increased by 500 feet. ¦
¦ ¦ ¦ ¦ ¦
¦ 5. Fuel Filter A ¦ 2 ¦ 1 ¦ (M)One may be inoperative provided: ¦
¦ Differential ¦ ¦ ¦ a) Fuel Low Pressure System for ¦
¦ Pressure Warning ¦ ¦ ¦ the affected engine is ¦
¦ Systems ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) Associated Filter is ¦
¦ ¦ ¦ ¦ verified free of clogging ¦
¦ ¦ ¦ ¦ before each flight, and ¦
¦ ¦ ¦ ¦ c) Repairs are made within 3 ¦
¦ ¦ ¦ ¦ flight days. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 4 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 05/31/1996 ¦ 74-1 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 74 IGNITION ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
　
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