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¦ ¦ ¦ ¦ failed, flight time with one ¦
¦ ¦ ¦ ¦ engine inoperative must not ¦
¦ ¦ ¦ ¦ exceed 1 hour cruise from a ¦
¦ ¦ ¦ ¦ suitable airport, and | ¦
¦ ¦ ¦ ¦ c) One Standby Magnetic Compass | ¦
¦ ¦ ¦ ¦ System (Flux Valves) is ¦
¦ ¦ ¦ ¦ operative. | ¦
¦ ¦ ¦ ¦ ¦
¦ 2. Attitude Reference B ¦ 3 ¦ 2 ¦ (O)One may be inoperative provided: ¦
¦ Sensors ¦ ¦ ¦ a) Both PFD Attitude Indicating ¦
¦ ¦ ¦ ¦ Systems operate ¦
¦ ¦ ¦ ¦ independently, ¦
¦ ¦ ¦ ¦ b) Standby Attitude Indicator ¦
¦ ¦ ¦ ¦ is operative, and ¦
¦ ¦ ¦ ¦ c) If number 1 or 2 System is ¦
¦ ¦ ¦ ¦ failed, flight time with one ¦
¦ ¦ ¦ ¦ engine inoperative must not ¦
¦ ¦ ¦ ¦ exceed 1 hour cruise from a ¦
¦ ¦ ¦ ¦ suitable airport. ¦
¦ ¦ ¦ ¦ ¦
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¦ ¦ ¦ ¦ ¦
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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 ¦ 34-2 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 34 NAVIGATION ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 3. Standby Flight ¦ ¦ ¦ | ¦
¦ Displays ¦ ¦ ¦ | ¦
¦ ¦ ¦ ¦ | ¦
¦ 1) Standby Attitude B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦
¦ *** Indicator (Electro- ¦ ¦ ¦ airplane is operated in day VMC | ¦
¦ Mechanical Gyro ¦ ¦ ¦ only. | ¦
¦ Horizon) ¦ ¦ ¦ | ¦
¦ ¦ ¦ ¦ | ¦
¦ a) Glideslope/ C ¦ 1 ¦ 0 ¦ | ¦
¦ *** Localizer ¦ ¦ ¦ | ¦
¦ Indicator ¦ ¦ ¦ | ¦
¦ ¦ ¦ ¦ | ¦
¦ 2) Standby Altimeter/ C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦
¦ *** Airspeed Indicator ¦ ¦ ¦ airplane is operated in day VMC | ¦
¦ (combined unit) ¦ ¦ ¦ only. | ¦
¦ ¦ ¦ ¦ | ¦
¦ 3) Standby Altimeter C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided | ¦
¦ (stand alone) ¦ ¦ ¦ airplane is operated in Day VMC | ¦
¦ ¦ ¦ ¦ only. | ¦
　
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