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System is operative.
AFM Emergency
Procedures , (Alternator/
Converter Failure –
Dual).
d) Flight crew may perform
maintenance procedures
if maintenance personnel
are not available.
3. APU Tachometers C
(EICAS and Overhead
Indicator)
2 0 (M) (O) Both 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
and ty-wrapped.
Flight crew will ensure:
a) BOTH Engine Driven
Alternators and BOTH
Converters are operative.
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.
An Inoperative Placard will
be placed on APU Master
Switch and will be noted on
ADLS.
(continued on next page) (continued on next page)
49-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 49-3
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
49. AIRBORNE AUXILIARY
POWER
3. APU Tachometers
(EICAS and Overhead
Indicator) (cont’d)
. c) Standby Electrical
System is operative.
AFM Emergency
Procedures , (Alternator/
Converter Failure –
Dual).
d) Flight crew may perform
maintenance procedures
if maintenance personnel
are not available.
4. APU Low Oil Pressure C
Warning Light
1 0 (M) (O) Both 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
and ty-wrapped.
Flight crew will ensure:
a) BOTH Engine Driven
Alternators and BOTH
Converters are operative.
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) Standby Electrical
System is operative.
AFM Emergency
Procedures , (Alternator/
Converter Failure –
Dual).
An Inoperative Placard will
be placed on APU Master
Switch and will be noted on
ADLS.
(continued on next page) (continued on next page)
49-4
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 49-4
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
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
49. AIRBORNE AUXILIARY
POWER
4. APU Low Oil Pressure
Warning Light (cont’d)
d) Flight crew may perform
maintenance procedures
if maintenance personnel
are not available.
5. APU Oil Pressure D
*** Gauges
 0 None required. None required. An Inoperative Placard will
be placed on APU Oil
Pressure Gauges and will be
noted on ADLS.
6. APU Oil Temperature D
*** Gauges
 0 None required. None required. An Inoperative Placard will
be placed on APU Oil
Temperature Gauges and
will be noted on ADLS.
7. APU Fuel Pressure D
*** Gauges
 0 None required. None required. An Inoperative Placard will
be placed on APU Fuel
Pressure Gauges and will be
noted on ADLS.
8. APU Overspeed C
Indicator Light
1 0 May be inoperative provided APU RPM
indicator is operative and APU RPM is
monitored whenever used in flight.
None required. Flight crew will ensure:
a) Overspeed Shutdown is
operative.
b) APU RPM Indicator is
operative and monitored
whenever used in flight.
AFM, Normal
Procedures .
An Inoperative Placard will
be placed on APU Overspeed
Indicator Light and will be
noted on ADLS.
49-5
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 49-5
　
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