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¦ Magnetic Compass ¦ ¦ ¦ combination of three Gyro or INS | ¦
¦ (Standby) ¦ ¦ ¦ (IRU) Stabilized Compass Systems | ¦
¦ ¦ ¦ ¦ are operative. | ¦
¦ ¦ ¦ ¦ | ¦
¦ B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided: | ¦
¦ ¦ ¦ ¦ a) Any combination of two Gyro | ¦
¦ ¦ ¦ ¦ or INS (IRU) Stabilized | ¦
¦ ¦ ¦ ¦ Compass Systems operate | ¦
¦ ¦ ¦ ¦ normally, and | ¦
¦ ¦ ¦ ¦ b) Airplane is operated with | ¦
¦ ¦ ¦ ¦ Dual Independent Navigation | ¦
¦ ¦ ¦ ¦ Capability and under | ¦
¦ ¦ ¦ ¦ Positive Radar Control by | ¦
¦ ¦ ¦ ¦ ATC on the enroute portion | ¦
¦ ¦ ¦ ¦ of the flight. | ¦
¦ ¦ ¦ ¦ | ¦
¦ B ¦ 1 ¦ 0 ¦ (O)May be inoperative for flights | ¦
¦ ¦ ¦ ¦ that are entirely within areas of | ¦
¦ ¦ ¦ ¦ magnetic unreliability provided at | ¦
¦ ¦ ¦ ¦ least two Stabilized Directional | ¦
¦ ¦ ¦ ¦ Gyro Systems are installed, operate | ¦
¦ ¦ ¦ ¦ normally, and used in conjunction | ¦
¦ ¦ ¦ ¦ with approved Free Gyro Navigation | ¦
¦ ¦ ¦ ¦ Techniques. | ¦
¦ ¦ ¦ ¦ ¦
¦ 27. Head Up Display D ¦ 1 ¦ 0 ¦ May be inoperative provided ¦
¦ *** System ¦ ¦ ¦ approach minimums or operating ¦
¦ ¦ ¦ ¦ procedures are not dependent on its ¦
¦ ¦ ¦ ¦ use. ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
-------------------------------------------------------------------------------
-------------------------------------------------------------------------------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ --------------------------------------------------------------------------- ¦
¦ AIRCRAFT: ¦ REVISION NO: 5 ¦ PAGE: ¦
¦ G-IV ¦ ¦ ¦
¦ ¦ DATE: 10/11/2001 ¦ 34-13 ¦
¦ --------------------------------------------------------------------------- ¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ -------------------------------------------- ¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ --------------------------------------- ¦
¦ ------------------------- ¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 34 NAVIGATION ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 28. Airborne Flight D ¦ - ¦ 0 ¦ ¦
¦ *** Information System ¦ ¦ ¦ ¦
¦ (AFIS) ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 1) AFIS Printer D ¦ - ¦ 0 ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 29. Slip-Skid ¦ ¦ ¦ ¦
¦ Indicator ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ (SN 1000-1252 B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ except 1236 ¦ ¦ ¦ a) Third attitude indicator is ¦
¦ without ASC 345 ¦ ¦ ¦ installed and operative, or ¦
¦ installed) ¦ ¦ ¦ b) Airplane is operated during ¦
¦ ¦ ¦ ¦ day VMC conditions. ¦
¦ ¦ ¦ ¦ ¦
¦ (SN 1236, SN 1253 B ¦ 2 ¦ 1 ¦ (O)One may be inoperative provided: ¦
¦ and subs and SN ¦ ¦ ¦ a) Third attitude indicator is ¦
　
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