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This action will cause isolation
valve to close; however, cockpit
annunciation will indicate open.
d) Inoperative Left Bleed Air
Control Valve is CLOSED
and electrically deactivated
by selecting left Bleed Air
Valve Switch OFF and
pulling L Bleed Air circuit
breaker.
Flight crew will ensure
airplane is operated at FL 410
or lower in accordance with
AFM Limitations .
NOTE: Autothrottle will be
inoperative with Isolation
Valve OPEN.
An Inoperative Placard will
be placed above affected
system’s Bleed Air Control
Switch and will be noted on
ADLS.
(continued on next page)
36-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 36-2
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
36. PNEUMATIC
1. HP Bleed Air System (cont’d)
2) Unpressurized
Configuration (cont’d)
2 0 (M) (O) Both may be inoperative provided:
a) Both Bleed Air Valves are
CLOSED and deactivated
electrically,
b) Airplane is not operated in
forecast or known icing
conditions,
c) Airplane is operated at or below
10,000 feet MSL, and
d) Airplane is operated in
accordance with AFM
Limitations.
Maintenance will ensure:
a) Right Bleed Air Control
Valve is CLOSED and
electrically deactivated by
selecting right Bleed Air
Valve Switch OFF.
NOTE: Isolation valve will
close if right bleed air circuit
breaker is pulled, however,
cockpit annunciation will
indicate open.
b) Left Bleed Air Control
Valve is CLOSED and
electrically deactivated by
selecting left Bleed Air
Valve Switch OFF and
pulling L Bleed Air circuit
breaker. G IV Maintenance
Manual, Chapter 36-01-
00 .
Flight crew will ensure
airplane is NOT operated in
known or forecast icing
conditions. To operate the
airplane unpressurized, select
manual pressurization and
slew the outflow valve to the
full open position with both
engine bleeds and air
conditioning packs selected
on. Monitor cabin differential
pressure to be nominally zero
psid during the flight.
An Inoperative Placard will
be placed above BOTH
Bleed Air Control
Switches and will be noted
on ADLS.
36-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 36-3
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
36. PNEUMATIC
2. Bleed Air Hot
Warning Systems
1) Pressurized C
Configuration
2 1 (M) One may be inoperative provided:
a) Associated Bleed Control Valve
is CLOSED and deactivated
electrically when associated
Engine Bleed Air System is
selected OFF,
b) Opposite Engine Bleed Air
System is operative,
c) Isolation Valve is verified
operative and selected OPEN,
and
d) Airplane is operated in
accordance with AFM
Limitations.
NOTE: Auto-throttle will be inoperative
with Isolation Valve OPEN.
Maintenance will ensure:
a) Opposite Engine Bleed Air
System and Isolation Valve
is verified operative.
b) Isolation Valve is selected
and verified OPEN.
c) Inoperative Right Bleed
Air Control Valve is
CLOSED and electrically
deactivated by selecting
right Bleed Air Valve
Switch OFF.
CAUTION: Do not pull right
bleed air circuit breaker when
deactivating right hand system.
This action will cause isolation
valve to close; however, cockpit
annunciation will indicate open.
d) Inoperative Left Bleed Air
Control Valve is CLOSED
and electrically deactivated
by selecting left Bleed Air
Valve Switch OFF and
pulling L Bleed Air circuit
breaker.
Flight crew will ensure
airplane is operated at FL 410
or lower in accordance with
AFM Limitations .
NOTE: Autothrottle will be
inoperative with Isolation
Valve OPEN.
An Inoperative Placard will
　
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