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| Page | 18/60 | | Date | 02.02.2017 | | Size | 6.47 Mb. | | #15690 |
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
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AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 8
DATE: 11/07/2014
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PAGE NO:
24-6
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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24
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ELECTRICAL POWER
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8.
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Electrical Power System EICAS Displays (continued)
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11)
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Ext AC Pwr Frequency Meter
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D
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1
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0
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May be inoperative if the voltmeter and loadmeter are operative.
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D
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1
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0
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May be inoperative if external AC power is not used.
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12)
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Ext AC Loadmeter
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D
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1
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0
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May be inoperative if the frequency and voltmeter are operative.
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D
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1
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0
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May be inoperative if external AC power is not used.
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13)
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Main, Essential and AUX TRU Voltmeters
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C
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5
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0
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May be inoperative if loadmeters are operative.
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14)
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Main, Essential and AUX TRU Loadmeters
(GV-SP, GIV-X)
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C
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5
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0
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Maybe inoperative if the voltmeters are operative.
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(GV)
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C
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5
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0
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May be inoperative provided:
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Voltmeters are operative, and
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Airplane is operated in accordance with AFM Limitations.
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15)
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Ext DC Pwr Voltmeter
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D
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1
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0
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May be inoperative if the loadmeter is operative.
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D
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1
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0
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May be inoperative if external DC power is not used.
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16)
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Ext DC Pwr Loadmeter
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D
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1
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0
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May be inoperative if the voltmeter is operative.
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D
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1
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0
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May be inoperative if external DC power is not used.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
|
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 7a
DATE: 11/08/2010
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PAGE NO:
24-7
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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24
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ELECTRICAL POWER
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9.
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Master Power Switch Lights (Left, Right, APU, EXT)
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C
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4
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3
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May be inoperative provided associated AC loadmeter and voltmeter are operative and selected for monitoring on the AC Synoptic.
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10. ***
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Battery Temperature Indicating System
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D
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1
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0
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11.
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Standby Electrical System
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C
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1
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0
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May be inoperative provided both engine driven generators and APU generator are operative.
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12.
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External Power System
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D
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1
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0
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13. ***
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Low Battery Power Audible Warning System (Sonalert)
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D
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1
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0
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14.
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Ground Service Bus System
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D
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1
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0
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15. ***
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50Hz/60Hz AC Electrical Power Systems
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D
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-
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0
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(M)(O) May be inoperative provided affected circuit breaker is pulled and collared.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
|
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 7
DATE: 02/04/2010
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PAGE NO:
24-8
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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24
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ELECTRICAL POWER
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16.
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IRU Back Up Batteries (GV)
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A
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2
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0
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May be inoperative provided:
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Airplane is operated in day VMC conditions, and
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Repairs are made within one (1) flight day.
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A
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2
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0
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May be inoperative provided:
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All other components of the Electrical Power system are operative, and
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Repairs are made within one (1) flight day.
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IRU Back Up Batteries (GV-SP, GIV-X)
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B
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2
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1
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(M) May be inoperative provided that the affected battery is located in the #2 or #3 IRU back up battery position.
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A
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2
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0
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May be inoperative provided:
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Airplane is operated in day VMC conditions, and
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Repairs are made within one (1) flight day.
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NOTE: EICAS message “IRU Sec Pwr Fail” will be displayed.
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A
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2
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0
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May be inoperative provided:
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All other components of the Electrical Power system are operative, and
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Repairs are made within one (1) flight day.
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