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d) Flight crew maintains a log of
fuel burned.
Maintenance personnel ensure
BOTH tanks are completely
filled using overwing method of
refueling. GIV Maintenance
Manual, Chapters 12-01-04 .
NOTE: Do not pull Fuel Qty
circuit breaker as this disables
Fuel Level Low caution
message.
Flight crew will ensure
a) Both Fuel Flow
Indicating Systems are
operative.
b) After takeoff, power is
set by matching Fuel
Flow indications on both
engines.
c) A log of fuel burned is
maintained.
NOTE: Total fuel indication
will be INCORRECT with an
inoperative indicator.
(continued on next page)
28-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 28-2
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
28. FUEL
2. Fuel Quantity Indicating
Systems (cont’d)
1) EICAS or Standby C 1 0 (M) (O) Either Left or Right Fuel Quantity
display may be inoperative provided:
a) Affected tank is defueled before
each refueling,
b) Affected tank is fueled with a
known quantity of fuel,
c) Both fuel flow meters are
operative,
d) After takeoff, power is set by
matching fuel flow indications on
both engines, and
e) Flight crew maintains a log of
fuel burned.
NOTE: Total fuel indication will be
incorrect with an inoperative indicator.
Maintenance will Defuel
affected tank before each
refueling and refuel tank with a
Known quantity of fuel.
Flight crew will ensure
a) Both Fuel Flow
Indicating Systems are
operative.
b) After takeoff, power is
set by matching Fuel
Flow indications on both
engines.
c) A log of fuel burned is
maintained.
NOTE: Total fuel indication
will be INCORRECT with an
inoperative indicator.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3. Fuel Low Quantity C
Warning Systems
(EICAS - Message)
Standby Indicator
Lights)
2 0 (O) Both may be inoperative provided:
a) Both Fuel Quantity Indicating
System are operative,
b) All Fuel Boost Pumps are
operative, and
c) Fuel Crossflow Valve is
OPENED when either wing tank
contains 2,000 pounds or less
fuel.
None required. Flight crew will ensure:
a) BOTH Fuel Quantity
Indicating Systems and
all Fuel Boost Pumps
are operative. AFM ,
Normal Procedures .
b) Fuel Crossflow Valve is
opened when either wing
tank contains 2,000
pounds or less.
An Inoperative Placard will
be placed next to affected
Standby Fuel Low Quantity
Warning Light and will be
noted on ADLS.
28-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 28-3
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
28. FUEL
4. Fuel Boost Pumps C 4 3 (O) One may be inoperative provided:
a) Fuel Crossflow Valve is
operative,
b) Fuel Intertank Valve is operative,
c) Both Fuel Low Quantity Warning
Systems are operative, and
d) Airplane is operated in
accordance with AFM
Limitations.
None required. Flight crew will ensure:
a) Fuel Crossflow Valve
and Intertank Valve are
operative. AFM, Normal
Procedures .
b) BOTH Fuel Quantity
Low Warning Systems
are operative. AFM ,
Normal Procedures .
c) Airplane is operated in
accordance with AFM ,
Abnormal Procedures ,
(Fuel Boost Pump
Failure), and
d) Pump switch is selected
OFF.
An Inoperative Placard will
be placed on affected Fuel
Boost Pump Switch and will
be noted on ADLS.
5. Fuel Intertank C
Valve
1 0 May be inoperative provided:
a) All Fuel Boost Pumps are
operative,
b) Fuel Crossflow Valve is
operative, and
c) Fuel Quantity Indicating System
is operative.
None required. None required. An Inoperative Placard will
　
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