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on ADLS.
NOTE: Individual standby indications may
be inoperative provided associated EICAS
indication is operative. See individual
indications for other authorized
configurations.
78-1
PAGE NUMBER: 78-1
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
78 ENGINE EXHAUST
1. Thrust Reverser C
Arm Lights (Green)
2 1 (M) One may be inoperative provided
associated REV UNLOCK message on the
EICAS is verified to be operative.
Maintenance will verify
associated EICAS "REV
UNLOCK" message is
operative.
NOTE: Airplane will need to be
placed in an "AIR MODE"
utilizing nutcracker switch with
Thrust Reverser(s) deployed to
obtain message. GIV
Maintenance Manual ,
Chapter 32-07-00 ("Air Mode"
procedures).
If maintenance personnel are
not available, flight crew will
ensure associated EICAS
"REV UNLOCK" message
is operative by utilizing
procedure listed Column 5.
An Inoperative Placard will
be placed on or next to
affected Thrust Reverser
Arm Light and will be noted
on ADLS.
OR
Maintenance will ensure
affected Thrust Reverser is
deactivated, stowed and
LOCKED in forward thrust
position. GIV Maintenance
Manual, Chapter 78-00-00.
OR
Flight crew will ensure
airplane is operated in
accordance with AFM
Limitation and Procedures .
Flight crew should be aware
of asymmetrical thrust during
single Thrust Reverser
operation on landing.
NOTE: AFM Landing
Distances are not affected by
inoperative Thrust Reversers.
78-2
PAGE NUMBER: 78-2
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
78 ENGINE EXHAUST
2. Thrust Reverser C 2 0 (M) Both may be inoperative provided:
a) Affected Thrust Reverser is
deactivated, stowed and
LOCKED in forward thrust
position, and
b) Airplane is operated in
accordance with AFM Limitation
and Procedures.
Maintenance will ensure
affected Thrust Reverser is
deactivated, stowed and
LOCKED in forward thrust
position. GIV Maintenance
Manual, Chapter 78-00-00.
Flight crew will ensure
airplane is operated in
accordance with AFM
Limitation and Procedures .
Flight crew should be aware
of asymmetrical thrust during
single Thrust Reverser
operation on landing.
NOTE: AFM Landing
Distances are not affected by
inoperative Thrust Reversers.
An Inoperative Placard will
be placed on affected Reverse
Thrust Lever Handle and
will be noted on ADLS.
79-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 79-1
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
79 ENGINE OIL
1. Low Oil Pressure B
Warning Systems
2 1 (O) One may be inoperative provided Oil
Pressure Indicators for both engines are
operative.
None Required. Flight crew will ensure Oil
Pressure Indication for both
engines are operative and
monitored during flight.
AFM, Normal Procedures ,
(Starting Engines).
An Inoperative Placard will
be placed on affected
Standby Oil Pressure
Warning Light and will be
noted on ADLS.
2. Engine Oil C
Replenishment System
1 0 Maintenance will provide a
method to service engine oil at
destination airfield.
None Required. An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3. Oil Filter Bypass C
Indication Systems
2 0 Both may be inoperative provided
　
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