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f) Inoperative Alternator drive shaft
is removed and alternator is
reinstalled, or a blanking plate is
installed in place of alternator.
Maintenance will remove
affected alternator, then remove
Drive Shaft or Spline Adapter
and replace alternator.
Associated electrical cables will
be disconnected, labeled and
secured. For Alternator, Drive
Shaft and Spline Adapter
removal, refer to GIV
Maintenance Manual ,
Chapter 24-01-01 .
Flight crew will ensure will
comply with provisos in
remarks column.
An Inoperative Placard will
be placed on or above
affected Alternator’s Power
Switch and will be noted on
ADLS.
(continued on next page) (continued on next page)
24-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-2
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
1. Engine Alternators
(cont’d)
Remove Alternator and install
Blanking Cover on engine.
Associated electrical cables will
be disconnected, labeled and
secured. For Alternator
removal, refer to GIV
Maintenance Manual ,
Chapter 24-01-01 .
2. APU Alternator B 1 0 (O) May be inoperative provided:
a) Both Engine Driven Alternators
are operative,
b) Both Converters are operative,
c) TRU is operative,
d) Standby Electrical System is
operative,
e) Procedures do not require its use,
f) APU Alternator 115 VAC circuit
breaker is pulled and collared,
and
g) APU is operated on ground only.
NOTE: APU may be used as a pneumatic
source.
Maintenance, if available, will
pull and collar #1 circuit breaker
on AC BPCU.
Flight crew will comply with
provisos in remarks column.
Flight crew will ensure #1
circuit breaker on AC BPCU
is pulled and collared.
An Inoperative Placard will
be placed on or above APU
Alternator’s Power Switch or
on APU Master Switch and
will be noted on ADLS.
C 1 0 (O) May be inoperative provided APU is
not utilized.
None required. Flight crew will ensure will
comply with provisos in
remarks column.
An Inoperative Placard will
be placed on or above APU
Alternator’s Power Switch or
on APU Master Switch and
will be noted on ADLS.
24-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-3
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
3. Converters B 2 1 (O) One may be inoperative provided:
a) TRU is operative,
b) APU Alternator is used for
takeoff, enroute and landing, and
c) Airplane is operated at or below
FL 300 or up to FL 350 and
below with Electrical Load
Warning System (ELWS)
installed or ASC 420 installed.
None required. Flight crew will ensure:
a) Affected alternator’s
Power Switch is selected
OFF.
b) TRU is operative. With
APU powering airplane,
check EPMP for DC load
indication. If value is
greater than zero and
TRU capsules are lighted,
TRU is operative.
c) Auxiliary Power Unit
(APU) Alternator is
used for all phases of
flight.
d) Airplane is operated at
FL 300 or below or up to
FL 350 with Electrical
Load Warning System
(ELWS) installed or with
ASC 420 installed.
e) QRH ELWS
Operational
Procedures , are followed
on airplanes equipped
with ELWS or ASC 420
when flights are
conducted above FL 300.
An Inoperative Placard will
be placed on affected
Alternator’s Power Switch
and will be noted on ADLS.
24-4
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 24-4
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
　
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