Airplane is operated in accordance with AFM Limitations.
Alt FuelPump Fail, L-R B
(Amber – Caution)
(GIV-X)
(O)
Except for ER operations, airplane may be dispatched with a single pump inoperative provided:
Fuel Crossflow Valve is operative,
Fuel Intertank Valve is operative,
Both Fuel Low Quantity Warning Systems are operative,
Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, and
Airplane is operated in accordance with AFM Limitations.
ALT PUMP FAIL, L-R B
(Amber – Caution)
(GV)
(O)
Except for ER operations, airplane may be dispatched with a single pump inoperative provided:
Fuel Crossflow Valve is operative,
Fuel Intertank Valve is operative,
Both Fuel Low Quantity Warning Systems are operative,
Flight crew comply with AFM, Section 3, Abnormal Procedures, Fuel Boost Pump Failure, 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:
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CAS Message
2.
Limitations and/or Procedures
Antiskid Fail B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched provided:
ANTI-SKID is selected “OFF”,
Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, Anti-Skid Failure are followed,
No WOW Power Faults exist,
If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and
Airplane is operated in accordance with AFM Limitations.
NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance.
ANTISKID FAIL B
(Amber – Caution)
(GV)
(O)
Airplane may be dispatched provided:
ANTI-SKID is selected “OFF”,
Anti-skid off braking procedures, AFM Section 3, Abnormal Procedures, Anti-Skid Failure are followed,
No WOW Power Faults exist,
If Auto mode of the AUX Hydraulic Pump is inoperative, AUX pump is selected ON for takeoff and landing, and
Airplane is operated in accordance with AFM Limitations.
NOTE: Anti-Skid inoperative AFM performance penalties must be applied. Refer to AFM, Section 5, Performance, Reference Accelerate-Stop Distance.
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
AP 1-2 Fail B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Except for ER operations or where en route operations or approach minimums require its use, Airplane may be dispatched with one (1) Autopilot inoperative provided the airplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
AP 1-2 Power Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Except for ER operations or where en route operations or approach minimums require its use, Airplane may be dispatched with one (1) inoperative provided airplane is operated in accordance with AFM Limitations in the event operative FGC fails and Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
AP/Trim Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched with one (1) elevator trim servo inoperative provided the inoperative trim servo circuit breaker(s) is pulled and collared.
APM 1-2-3-4 Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched with one (1) APM inoperative.
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
APU Fail B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Except for ER operations, airplane may be dispatched provided:
Both Engine Driven generators are operative, and
Standby Electrical System is operative.
APU FAIL B
(Amber – Caution)
(GV)
(O)
Except for ER operations, airplane may be dispatched provided:
Both Engine Driven generators are operative, and
Standby Electrical System is operative.
APU Fire Bottle DischargeB
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Except for ER operations, airplane may be dispatched provided:
Except for ER operations, airplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
APU GCU FAIL A
(Blue – Advisory)
(GV)
(O)
Except for ER operations, airplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
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
APU Generator Fail A
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Except for ER operations, airplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
APU Generator Maint ReqdC
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched.
APU GEN FAIL A
(Blue – Advisory)
(GV)
(O)
Except for ER operations, airplane may be dispatched provided:
APU GCU PWR circuit breaker on left EER, G-11 is pulled and collared,
Both Engine Driven generators are operative as verified by reference to the AC synoptic and the absence of failure messages on CAS,
Standby Electrical System is operative, and
Repairs are made within two (2) flight days.
APU GEN MAINT REQD C
(Blue – Advisory)
(GV)
Airplane may be dispatched.
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
APU Maintenance RequiredC
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched.
APU MAINT REQD C
(Blue – Advisory)
(GV)
Airplane may be dispatched.
APU Shutoff Valve Fail B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Except for ER operations, may be inoperative provided:
Both Engine Driven generators are operative,
Standby Electrical System is operative, and
APU is not used.
ATC 1-2 Fail C
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched with any in excess of those required by 14 CFR inoperative.
NOTE 1: Flight Director, Autopilot, and Transponder must use the same Air Data source for flight into RVSM airspace.
NOTE 2: Transponder and altitude reporting capability must be operative for flight into RVSM airspace.
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
BAROSET 1 Fail C
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched provided:
None of the following CAS messages are also posted:
ADS 2 Fail
ADS 3 Fail
BAROSET 2 Fail
BAROSET 3 Fail
b) Manual Pressurization Control System is operative,
c) Cabin Altitude and Differential Pressure Indicators are operative,
d) Cabin Rate of Climb Indicator is operative,
e) Flight crew select ADS sources that are independent and not associated with the BAROSET failure,
f) Autopilot is operative, and
g) Airplane is operated in accordance with AFM Limitations.
NOTE 1: Two systems are required for operation in RVSM airspace.
NOTE 2: Transponder and Flight Director/Autopilot must use same ADC data for RVSM.
