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¦ Control Systems ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ c) Airplane is operated at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. | ¦
¦ ¦ ¦ ¦ ¦
¦ 1) Automatic C ¦ 2 ¦ 0 ¦ Both automatic control systems may ¦
¦ System ¦ ¦ ¦ be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Associated manual control ¦
¦ ¦ ¦ ¦ system is operative, and ¦
¦ ¦ ¦ ¦ b) Associated temperature ¦
¦ ¦ ¦ ¦ indicator is operative. ¦
¦ ¦ ¦ ¦ ¦
¦ 2) Manual System C ¦ 2 ¦ 0 ¦ Both manual control systems may be ¦
¦ ¦ ¦ ¦ inoperative provided: ¦
¦ ¦ ¦ ¦ a) Associated automatic control ¦
¦ ¦ ¦ ¦ system is operative, and ¦
¦ ¦ ¦ ¦ b) Associated temperature ¦
¦ ¦ ¦ ¦ indicator is operative. ¦
¦ ¦ ¦ ¦ ¦
¦ 10. Cockpit/Cabin D ¦ 1 ¦ 0 ¦ Both displays on indicator may be ¦
¦ Temperature ¦ ¦ ¦ inoperative provided associated ¦
¦ Indicator ¦ ¦ ¦ Automatic Temperature Control ¦
¦ ¦ ¦ ¦ System is operative. | ¦
¦ ¦ ¦ ¦ | ¦
¦ D ¦ 1 ¦ 0 ¦ Both displays on indicator may be | ¦
¦ ¦ ¦ ¦ inoperative provided associated | ¦
¦ ¦ ¦ ¦ Manual Temperature Control 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 ¦ 21-5 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 11. Environmental ¦ ¦ ¦ ¦
¦ Control System ¦ ¦ ¦ ¦
¦ (ECS) Packs ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 1) Pressurized C ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ Configuration ¦ ¦ ¦ a) Inoperative ECS Pack is ¦
¦ ¦ ¦ ¦ selected OFF, ¦
¦ ¦ ¦ ¦ b) Bleed Air Isolation Valve is ¦
¦ ¦ ¦ ¦ CLOSED and OPERATIVE, and ¦
¦ ¦ ¦ ¦ c) Airplane is operated in ¦
¦ ¦ ¦ ¦ accordance with AFM ¦
¦ ¦ ¦ ¦ Limitations. ¦
¦ ¦ ¦ ¦ ¦
¦ 2) Unpressurized C ¦ 2 ¦ 0 ¦ (O)Both may be inoperative ¦
¦ Configuration ¦ ¦ ¦ provided: ¦
¦ ¦ ¦ ¦ a) Outflow valve is operative, ¦
　
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