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¦ *** Computers (PZ) ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 4. Yaw Damper System C ¦ 1 ¦ 0 ¦ (M)May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Airplane is operated in ¦
¦ ¦ ¦ ¦ accordance with AFM ¦
¦ ¦ ¦ ¦ Limitations, and ¦
¦ ¦ ¦ ¦ b) Procedures are established ¦
¦ ¦ ¦ ¦ to deactivate Yaw Damper ¦
¦ ¦ ¦ ¦ System. ¦
¦ ¦ ¦ ¦ ¦
¦ 5. Control Wheel C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦
¦ Autopilot ¦ ¦ ¦ a) Autopilot is not utilized at ¦
¦ Disconnect Buttons ¦ ¦ ¦ less than initial approach ¦
¦ ¦ ¦ ¦ altitude, and ¦
¦ ¦ ¦ ¦ b) Airplane is piloted from | ¦
¦ ¦ ¦ ¦ side with operative button. | ¦
¦ ¦ ¦ ¦ ¦
¦ 6. Takeoff/Go-Around C ¦ 2 ¦ 0 ¦ Both may be inoperative provided ¦
¦ (TOGA) Buttons ¦ ¦ ¦ alternate procedures are ¦
¦ ¦ ¦ ¦ established and used. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ NOTE: Autothrottles and Flight ¦
¦ ¦ ¦ ¦ Director are unavailable for ¦
¦ ¦ ¦ ¦ takeoff and go-around. ¦
¦ ¦ ¦ ¦ ¦
¦ 7. Autothrottle C ¦ 2 ¦ 0 ¦ (O)Both may be inoperative provided ¦
¦ Disconnect Buttons ¦ ¦ ¦ autothrottle is not utilized. ¦
¦ (on Thrust Lever ¦ ¦ ¦ ¦
¦ Knobs) ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 8. Autothrottle C ¦ 2 ¦ 0 ¦ Both may be inoperative provided ¦
¦ Engage/Disengage ¦ ¦ ¦ Autothrottle is considered ¦
¦ Switches (on ¦ ¦ ¦ inoperative. ¦
¦ Thrust Lever Stem) ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 10/11/2001 ¦ 22-3 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 9. Touch Control D ¦ 2 ¦ 0 ¦ NOTE: If Honeywell HUD is ¦
¦ Steering Switches ¦ ¦ ¦ installed and the left TCS ¦
¦ (TCS) ¦ ¦ ¦ is inoperative, the HUD TCS ¦
¦ ¦ ¦ ¦ "clear" function will be ¦
¦ ¦ ¦ ¦ inoperative. ¦
¦ ¦ ¦ ¦ ¦
¦ 10. Remote Heading C ¦ - ¦ 0 ¦ May be inoperative provided manual | ¦
¦ *** and Course Select ¦ ¦ ¦ Heading and Course Selectors | ¦
¦ Control System ¦ ¦ ¦ operate normally. | ¦
¦ ¦ ¦ ¦ ¦
　
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