2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared.
Opposite Engine Bleed Air System is operative,
Isolation Valve is verified to be operative and selected OPEN, and
Airplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2 -
1.
CAS Message
2.
Limitations and/or Procedures
BAS Fail, L-R B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
(GIV-X):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared.
Opposite Engine Bleed Air System is operative,
Isolation Valve is verified to be operative and selected OPEN,
Airplane is not operated in forecast or known icing conditions, and
Airplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2 -
1.
CAS Message
2.
Limitations and/or Procedures
BAS Fail, L-R B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Except for ER operations, airplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided
(GV-SP):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared.
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Airplane is not operated in known or forecast icing conditions, and
Airplane is operated in accordance with AFM Limitations.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2 -
1.
CAS Message
2.
Limitations and/or Procedures
BAS Fail, L-R B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
(GIV-X):
Affected Valve(s) are verified CLOSED,
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Airplane is not operated in forecast or known icing conditions, and
Airplane is operated in accordance with AFM Limitations.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2 -
1.
CAS Message
2.
Limitations and/or Procedures
BAS FAIL, L-R B
(Amber – Caution)
(GV)
(O)
Except for ER operations, airplane may be dispatched in the pressurized configuration with one Bleed Air System inoperative provided
(GV):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared.
Opposite Engine Bleed Air System is operative,
Isolation Valve is verified to be operative and selected OPEN, and
Airplane is operated in accordance with AFM Limitations.
NOTE: Auto-throttle will be inoperative with Isolation Valve OPEN.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
REVISION NO: 8
DATE: 11/07/2014
PAGE NO:
2 -
1.
CAS Message
2.
Limitations and/or Procedures
BAS FAIL, L-R B
(Amber – Caution)
(GV)
(O)
Except for ER operations, airplane may be dispatched in the unpressurized configuration with both Bleed Air Systems inoperative provided
(GV):
Inoperative Bleed Control Valve is CLOSED and deactivated electrically when associated Engine Bleed Air System is selected OFF as follows:
1. Affected Bleed Air Valve is selected OFF
2. Affected R BLEED AIR CONT: REER, E-9 and R WING ANTI-ICE: REER, D-13 or L BLEED AIR CONT: LEER, E-10 and L WING ANTI-ICE: LEER, D-4 circuit breakers are pulled and collared.
Manual pressurization control is selected,
Outflow valve is slewed to the full OPEN position,
RAM Air is selected ON,
Cabin differential pressure is monitored to be nominally zero psid during the flight,
Airplane is not operated in known or forecast icing conditions, and
Airplane is operated in accordance with AFM Limitations.
Airplane may be dispatched with one inoperative battery charger provided:
Both Engine Generators are operative,
APU Generator is operative,
Associated L BATT CHGR: Left PDB, Left Main AC section or R BATT CHGR: Right PDB, Right Main AC section circuit breaker on the Power Distribution Box is pulled and collared,
