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1
1
1
1
1
1
1
1
2
0
0
0
0
0
0
0
0
1
Only one of Items 1 through 9 may be
inoperative.
None required. Flight crew will select and
monitor Voltmeter or
Loadmeter, as appropriate
for affected display.
NOTE: Only one (1) of the
Items contained in Column 1
may be inoperative.
An Inoperative Placard will
be placed on affected Display
and will be noted on ADLS.
24-7
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-7
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
11. Battery Charger C
Fail Lights
2 1 One may be inoperative provided:
a) Associated charger is operative,
b) Associated ammeter is operative,
and
c) Associated voltmeter is operative.
None required. None required. An Inoperative Placard will
be placed on affected Battery
Charger Fail Light and will
be noted on ADLS.
12. Master Power C
Switch Lights
(Left, Right, AUX)
3 2 (O) One may be inoperative provided the
associated AC loadmeter and voltmeter are
operative and selected for monitoring.
None required. Flight crew will ensure
associated AC Loadmeter
and Voltmeter are operative
and selected for monitoring.
AFM, Normal Procedures .
An Inoperative Placard will
be placed on affected Master
Power Switch Light and will
be noted on ADLS.
13. APU Alternator D
OFF Warning
System
1 0 None required. None required. An Inoperative Placard will
be placed on APU Alternator
OFF Light and will be noted
on ADLS.
14. Battery Temperature D
*** Indicating System
1 0 None required. None required. An Inoperative Placard will
be placed on affected
Temperature Indicator and
will be noted on ADLS.
15. Standby Electrical C
System
1 0 None required. None required. An Inoperative Placard will
be placed on Standby
Electrical System Control
Panel and will be noted on
ADLS.
24-8
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-8
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
16. Converter Cooling C
Fans
10 9 (M) One may be inoperative provided:
a) Normal operation of remaining
fans is verified before each
departure, and
b) Airplane is operated in
accordance with AFM.
Maintenance will verify normal
operation of remaining Fans is
verified prior to departure. GIV
Maintenance Manual ,
Chapter 24-01-02 .
None required. An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
17. External Power D
Systems
1 0 None required. None required. An Inoperative Placard will
be placed above AUX Power
Switch and will be noted on
ADLS.
18. Electrical Load D
*** Warning System
(ELWS)
1 0 None required. None required. An Inoperative Placard will
be displayed on ELWS
Indicator and will be noted
on ADLS.
24-9
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-9
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
19. APU Alternator C
Overheat Warning
System
1 0 (M) (O) May be inoperative provided:
a) APU is not operated,
b) Both Engine Driven Alternators
are operative,
c) Both Converters are operative,
d) TRU is operative, and
e) Standby Electrical System is
operative.
Maintenance will ensure APU
CONT circuit breaker is pulled
　
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