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prior to EACH flight. GIV
Maintenance Manual ,
Chapter 12-01-05 .
If maintenance personnel are
not available, flight crew shall
check hydraulic quantity level
on Flight Hydraulic System
Reservoir Sight Gauge prior
to EACH flight.
An Inoperative Placard will
be placed on Flight
Hydraulic System Quantity
Gauge and will be noted on
ADLS.
8. Combined Hydraulic C
System Quantity
Indication (EICAS)
1 0 (M) May be inoperative provided quantity
is checked by reservoir sight gauge or
fuselage located Combined and Flight
Hydraulic Quantity gauges before each
departure.
Maintenance will ensure
hydraulic quantity level is
checked by Reservoir Sight
Gauge or fuselage located
Combined System Gauge prior
to EACH flight. GIV
Maintenance Manual ,
Chapter 12-01-05 .
If maintenance personnel are
not available, flight crew shall
check hydraulic quantity level
on Combined Hydraulic
System Reservoir Sight
Gauge or fuselage located
Combined System Gauge
prior to EACH flight.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
29-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 29-3
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
29. HYDRAULIC POWER
9. Flight Hydraulic C
System Quantity
Indication (EICAS)
1 0 (M) May be inoperative provided quantity
is checked by reservoir sight gauge or
fuselage located Combined and Flight
Hydraulic Quantity gauges before each
departure.
Maintenance will ensure
hydraulic quantity level is
checked by Reservoir Sight
Gauge or fuselage located
Flight System Gauge prior to
EACH flight. GIV
Maintenance Manual ,
Chapter 12-01-05 .
If maintenance personnel are
not available, flight crew shall
check hydraulic quantity level
on Flight Hydraulic System
Reservoir Sight Gauge or
fuselage located Combined
System Gauge prior to
EACH flight.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
10. Hydraulic Reservoir D
Replenishing System
1 0 (M) May be inoperative provided
maintenance personnel replenish the
hydraulic reservoirs as needed using
approved servicing techniques.
Airplane may continue in
service provided maintenance
personnel replenish the
hydraulic reservoirs as needed
using approved servicing
techniques.
None required. An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
30-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 30-1
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
30. ICE AND RAIN PROTECTION
1. Cowl Anti-Ice B
Pressure Indicators
2 0 (O) May be inoperative provided SAT is
greater than +8 degrees C for entire flight,
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on affected Cowl
Anti-Ice Pressure Gauge
and will be noted on ADLS.
B 2 0 (O) Both may be inoperative provided:
a) Airplane is operated in VMC,
and
b) Airplane is not operated in
visible moisture.
None required. Flight crew will comply with
provisos in remarks column.
An Inoperative Placard will
be placed on affected Cowl
Anti-Ice Pressure Gauge
and will be noted on ADLS
B 2 0 (O) Both may be inoperative provided Both
EICAS Cowl Anti-Ice Indications are
operative.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on affected Cowl
Anti-Ice Pressure Gauge
and will be noted on ADLS
2. Wing Anti-Ice C
Systems
2 0 (O) Both may be inoperative provided
　
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