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ADLS.
2. Lavatory Waste C
System (Including
Wheelchair
Accessible Lavatories)
  (M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system components
are verified not to have leaks.
Maintenance will ensure
appropriate procedures are
established to deactivate
applicable system components
and verify that components do
not have leaks.
None required. An Inoperative Placard will
be placed on Lavatory
Waste System and will be
noted on ADLS.
NOTE: Any portion of system which
operates normally may be used.
(continued on next page)
38-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 38-2
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
38. WATER/WASTE
2. Lavatory Waste
System (Including
Wheelchair
Accessible Lavatories)
(cont’d)
C   (M) Associated Lavatory system(s) may be
inoperative provided:
a) Associated components are
deactivated or isolated to prevent
leaks, and
b) Associated lavatory door(s) is
secured CLOSED and placarded
inoperative.
Maintenance will ensure
appropriate procedures are
established to deactivate
applicable system components.
None required. An Inoperative Placard will
be placed on Lavatory
Waste System and will be
noted on ADLS.
NOTE: These provisos are not intended to
prohibit inspections by crewmembers.
49-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 49-1
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
1. Auxiliary Power C
Unit (APU)
1 0 (O) May be inoperative provided:
a) Both Engine Driven alternators
are operative,
b) Both Converters are operative,
c) TRU is operative, and
d) Standby Electrical System is
operative.
None required. 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.
2. APU EGT Indicators C
(EICAS and Overhead
Indicator)
(continued on next page)
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.
(continued on next page)
An Inoperative Placard will
be placed on APU Master
Switch and will be noted on
ADLS.
49-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 49-2
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
49. AIRBORNE AUXILIARY
POWER
2. APU EGT Indicators
(EICAS and Overhead
Indicator) (cont’d)
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
　
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