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hour cruise from a suitable
airport.
c) One Standby Magnetic
Compasses Systems (Flux
Valves) are operative.
None required. Flight crew will comply with
provisos in remarks column.
An Inoperative Placard will
be placed on Mode Select
Unit (MSU) and will be
noted on ADLS.
2. Attitude Reference B
Sensors
3 2 (O) One may be inoperative provided:
a) Both PFD Attitude Indicating
System operate independently,
b) Standby Attitude Indicator is
operative, and
c) If number 1 or 2 System is failed,
flight time with one engine
inoperative must not exceed 1
hour cruise from a suitable
airport.
None required. Flight crew will comply with
provisos in remarks column.
An Inoperative Placard will
be placed on Mode Select
Unit (MSU) and will be
noted on ADLS.
3. Standby Flight
Displays
*** 1) Standby Altitude B
Indicator (Electro-
Mechanical Gyro
Horizon)
1 0 (O) May be inoperative provided airplane is
operated in day VMC only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on Standby
Attitude Indicator and will
be noted on ADLS.
(continued on next page)
34-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 34-2
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
34. NAVIGATION
3. Standby Flight
Displays (cont’d)
*** a) Glideslope/ C
Localizer
Indicator
1  None required. None required. An Inoperative Placard will
be placed on Glideslope/
Localizer Indicator and will
be noted on ADLS.
*** 2) Standby Altimeter/ C
Airspeed Indicator
(combined unit)
1 0 (O) May be inoperative provided airplane is
operated in day VMC only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will be
placed on Standby
Altimeter/Airspeed Indicator
and will be noted on ADLS.
3) Standby Altimeter C
(stand alone)
1 0 (O) May be inoperative provided airplane is
operated in Day VMC only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on Standby
Altimeter and will be noted
on ADLS.
*** 4) Standby Airspeed C
Indicator (stand
Alone)
1 0 (O) May be inoperative provided airplane is
operated in Day VMC only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on Standby
Airspeed Indicator and will
be noted on ADLS.
*** 5) Secondary Flight B
Display (3-in-1
Color Video Standby
Attitude, Altitude,
Airspeed Indicator)
(SFDS)
1 0 (O) The Attitude function may be
inoperative provided airplane is operated in
day VMC only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be placed on Standby
Attitude Indicator and will
be noted on ADLS.
(continued on next page)
34-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 34-3
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
34. NAVIGATION
3. Standby Flight
Displays (cont’d)
a) Standby Air C
Data Unit
1 0 (O) The Air Data Unit may be inoperative
provided airplane is operated in day VMC
only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
b) Standby Heading C
Display
1 0 The Heading Display may be inoperative
provided airplane is operated in day VMC
only.
None required. Flight crew will comply with
proviso in remarks column.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
　
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