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NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
24. ELECTRICAL POWER
4. Transformer- B
Rectifier
1 0 (M) May be inoperative provided:
a) Both Converters are operative,
b) APU Alternator is operative,
c) Both Battery chargers are
operative,
d) Both Main Airplane Batteries are
operative, and
e) TRU (R-AC) circuit breaker on
the Power Distribution Box is
pulled and collared.
Maintenance will pull and tywrapped
TRU (R-AC)
CONTROL circuit breaker
(located on PDB).
Flight crew will comply with
provisos in remarks column.
An Inoperative Placard will
be placed on TRU Switch
and will be noted an ADLS.
5. Battery Chargers B 2 1 (M) One may be inoperative provided:
a) Engine-driven alternators and
both converters are operative,
b) APU Alternator is operative,
c) Associated Battery Charger
circuit breaker on the Power
Distribution Box is pulled and
collared, and
d) Standby Electrical System is
operative.
Maintenance will pull and tywrap
associated Battery
Charger circuit breaker (located
on PDB).
Flight crew will comply with
provisos in remarks column.
An Inoperative Placard will
be placed above affected
Battery Switch and will be
noted on ADLS.
24-5
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-5
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
6. Main Airplane B
Batteries
2 1 (O) One may be inoperative provided:
a) Airplane is operated in day VMC,
b) There are no other electrical
power source failures,
c) Associated Battery cables are
disconnected and secured,
d) Associated Battery Charger
circuit breaker on the Power
Distribution Box is pulled and
collared, and
e) Associated battery circuit breaker
is pulled and collared.
Maintenance, if available, will
pull and ty-wrap associated
BATT CHGR and BATT
circuit breakers. In addition,
associated battery cables will be
disconnected, labeled and
secured. GIV Maintenance
Manual, Chapter 24-02-03 .
Flight crew will ensure:
a) Maintenance procedures
are accomplished, if
maintenance personnel
are not available.
b) Affected BATTery
Switch is selected OFF.
b) Airplane is operated in
Day, VMC conditions.
c) There are no other
electrical power source
failures. AFM, Normal
Procedures.
An Inoperative Placard will
be placed on affected Battery
Switch and will be noted on
ADLS.
7. SEL/AUTO Buttons C
on EPMP
6 5 (O) One may be inoperative provided
affected bus is manually selected ON.
None required. Flight crew will ensure
affected Bus is manually
selected ON to its primary
source of power.
An Inoperative Placard will
be placed on affected
SEL/AUTO Switch and will
be noted on ADLS.
8. Battery Ammeters C 2 1 One may be inoperative provided:
a) The associated voltmeter is
operative, and
b) Both battery charger fail lights
are operative.
None required. None required. An Inoperative Placard will
be placed on affected Battery
Ammeter and will be noted
on ADLS.
9. Battery Voltmeters C 2 1 One may be inoperative provided the
associated ammeter is operative.
None required. None required. An Inoperative Placard will
be placed on Voltmeter and
will be noted on ADLS.
24-6
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-6
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
10. Electrical Power
Monitor Panel
(EPMP) Displays
1) AC Voltmeter C
2) Frequency Meter C
3) DC Voltmeter C
4) Left AC C
Loadmeter (%)
5) AUX PWR AC C
Loadmeter (%)
6) Right AC C
Loadmeter (%)
7) Left DC C
Loadmeter (%)
8) AUX PWR DC C
Loadmeter (%)
9) Right DC C
Loadmeter (%)
　
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