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SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
73 ENGINE FUEL & CONTROL
1. Fuel Flow B
Indication Systems
(EICAS)
2 1 (M) One may be inoperative provided:
a) Associated EPR, LP and HP
indicating systems are operative,
and
b) Fuel Quantity Indicating Systems
are operative.
Maintenance will ensure
associated EPR, LP, HP and
Fuel Quantity Indicating
Systems are operative. AFM ,
Normal Procedures .
None required. An Inoperative Placard will
be placed on or next to
affected Standby Engine
Instrument FF Indicator
and will be noted on ADLS.
2. Engine Top Temperature C
*** Control Systems
2 0 (O) Both may be inoperative provided TGT
is monitored and manually controlled to
appropriate limits.
None required. Flight crew will select
affected ENGINE TEMP
CONTROL Switch(s) to
OFF. Flight crew will
monitor TGT and Manually
Control TGT within limits.
AFM, Limitations .
An Inoperative Placard will
be placed on affected Engine
Temp Control Switch and
will be noted on ADLS.
3. Fuel Low Pressure C
Warning Systems
(EICAS and Standby)
2 1 (O) One may be inoperative provided:
a) Associated fuel boost pumps are
operative, and
b) Airplane is operated at or below
FL 250.
None required. Flight crew will ensure
associated Fuel Boost Pumps
are operative. Flight crew will
ensure airplane is operated at
or below FL 250 and will
monitor Fuel Flow
Indications to ensure proper
pressure.
An Inoperative Placard will
be placed on affected
Standby Fuel Press
Warning Light and will be
noted on ADLS.
73-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 73-2
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
73 ENGINE FUEL & CONTROL
4. Approach Idle Systems C 2 0 (M) (O) Both may be inoperative provided:
a) Both Systems are de-energized
(Approach Idle Mode),
b) Both Systems are in the
(Approach Idle Mode), and
c) Field length requirements for
takeoff and landing are increased
by 500 feet.
Maintenance will ensure BOTH
Approach Idle Systems are deenergized
by pulling and
collaring (ty-wrapping) BOTH
ENG IDLE circuit breakers.
Flight crew will monitor
engine start TGTs as both
Approach Idle Systems are
in Approach Idle Mode.
Flight crew will plan an
additional 500 feet into
required field length for
takeoff and landing.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
5. Fuel Filter Differential A
Pressure Warning
Systems
2 1 (M) One may be inoperative provided:
a) Fuel Low Pressure System for the
affected engine is operative,
b) Associated Filter is verified free
of clogging before each flight ,
and
c) Repairs are made within 3 flight
days.
Maintenance will ensure:
a) Fuel Low Pressure
Warning System for
affected engine is operative.
b) Associated engine LP Filter
is verified free of clogging
prior to first flight with this
condition.
c) Repairs are made within
three flight days.
None required. An Inoperative Placard will
be placed on affected
Standby Fuel Filter
Warning Light and will be
noted on ADLS.
74-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 74-1
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
74 IGNITION
1. Ignition Systems
1 No. 1 Igniters C 2 1 (O) One may be inoperative provided:
a) Both No. 2 Igniters are operative,
and
b) Takeoff runway does not have
standing water, slush, or snow.
None required. Flight crew will ensure:
a) Both No. 2 Igniters are
operative.
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