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b) Takeoff runway does not
have standing water,
slush, or snow.
An Inoperative Placard
indicating affected system
will be displayed in a
prominent position to be seen
by flight crew and will be
noted on ADLS.
2) No. 2 Igniters C 2 1 (O) One may be inoperative provided:
a) Both No. 1 Igniters are operative,
and
b) Takeoff runway does not have
standing water, slush, or snow.
None required. Flight crew will ensure:
a) Both No. 1 Igniters are
operative.
b) Takeoff runway does not
have standing water,
slush, or snow.
An Inoperative Placard
indicating affected system
will be displayed in a
prominent position to be seen
by flight crew and will be
noted on ADLS.
76-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 76-1
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
76 ENGINE CONTROLS
1. Engine Synchronizer D
System
1 0 None required. None required. An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
77-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 77-1
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
77 ENGINE INDICATING
1. HP Tachometer C
Indications EICAS
2 1 None required. Flight crew will ensure
affected Engine LP, EPR,
and Fuel Flow Indicating
Systems are operative and
monitored. AFM, Normal
Procedures , (Starting
Engines).
NOTE: Standby HP
Indication may also be
inoperative on both engines.
An Inoperative Placard will
be placed on or next to
affected Standby Engine
Instrument HP% Indicator
and will be noted on ADLS.
2. Engine Vibration Monitoring
Systems Sensors
1) Primary C
Sensors
4 0 All may be inoperative provided associated
Secondary Sensor System is operative.
None required. Flight crew will ensure
associated Secondary Sensor
System is operative. AFM ,
Normal Procedures .
An Inoperative Placard will
be placed on or next toVib
Monitor Sensor Switch and
will be noted on ADLS.
2) Secondary C
Sensors
4 0 All may be inoperative provided associated
Primary Sensor System is operative.
None required. Flight crew will ensure
associated Primary Sensor
System is operative. AFM ,
Normal Procedures .
An Inoperative Placard will
be placed on or next toVib
Monitor Sensor Switch and
will be noted on ADLS.
4. Engine Pressure Ratio C
(EPR) Indicating Systems
2 0 (O) Both may be inoperative provided
airplane is dispatched in accordance with
GIV AFM Supplement No. GIV-95-05.
None required. Flight crew will ensure
airplane is operated in
accordance with AFM
L imitations and Procedures
and A FM Supplement No .
GIV-95-05 .
An Inoperative Placard will
be placed on or next to
affected Standby Engine
Instrument EPR Indicator
and will be noted on ADLS.
77-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 77-2
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
77 ENGINE INDICATING
5. LP Tachometer C
EICAS
2 1 None required. None required. An Inoperative Placard will
be placed on or next to
affected Standby Engine
Instrument LP% Indicator
and will be noted on ADLS.
6. Standby Engine C
Instruments Indicating
System
1 0 May be inoperative provided associated
EICAS indications are operative.
None required. None required. An Inoperative Placard will
be placed on or next to
affected Standby Engine
Instrument and will be noted
　
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