Airplane may be dispatched.
NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures.
HYD TMP SEN FL, L-R B
(Blue – Advisory)
(GV)
Airplane may be dispatched.
NOTE: Accuracy of hydraulic quantity indication will be degraded during long flights in cold soak conditions. If Right Hydraulic System (R SYS) sensor has failed in flight, there is no protection against overheating R SYS pumps during Power Transfer Unit (PTU) operation. In flight, with either or both sensors failed, there is no warning of hot hydraulic system temperatures.
b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and
c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges.
NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available.
ICE DETECT FL, L-R B
(Amber – Caution)
(GV)
(O)
Airplane may be dispatched provided:
a) Airplane is operated in accordance with alternate AFM procedures,
b) Cowl Anti-Ice shall be selected ON manually any time visible moisture is present and SAT is +10 deg C or less, and
c) Wing Anti-Ice should be selected ON manually if icing conditions are imminent or immediately upon detection of ice formation on the wings, winglets or windshield edges.
NOTE: With Ice Detection Systems inoperative, automatic anti-ice is not available.
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
IRS 1-2-3 Fail A
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched with one (1) IRS inoperative provided:
Both PFD attitude indicating systems operate independently,
Flight crew ensure same IRS is NOT used as attitude source for both pilots,
Airplane may be dispatched with one (1) IRS inoperative provided:
Both PFD attitude indicating systems operate independently,
Flight crew ensure same IRS is NOT used as attitude source for both pilots,
Standby Attitude Indicator is operative, and
Repairs are made within two (2) flight days.
IRS 1-2-3 ON DC A
(Blue – Advisory)
(GV)
Airplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day.
IRU On Sec Pwr A
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched provided only one (1) IRU / IRS is on Secondary Power provided repairs are made within one (1) flight day.
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
IRU Sec Pwr 1-2-3 Fail A
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched with one back-up battery inoperative provided:
a) The affected battery is located in the
#2 or #3 IRU back up battery
position, and
b) Repairs are made within one (1)
flight day.
A
Airplane may be dispatched with both back-up batteries inoperative provided:
Airplane is operated in day VMC conditions, and
Repairs are made within one (1) flight day.
A
Airplane may be dispatched with both back-up batteries inoperative provided:
All other components of the Electrical Power system are operative, and
Repairs are made within one (1) flight day.
LASERTRAK FAIL B
(Blue – Advisory)
(GV)
Airplane may be dispatched provided at least one Flight Management System is operative.
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
L PSU Fan Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched provided;
Ambient Temperature is 95 degrees F (35 degrees C) or cooler,
Both Environmental Control System (ECS) Packs are operative,
Flight crew minimize ground operation time, and
For ground operations longer than 15 minutes, flight crew ensure main and baggage doors are closed, APU air is selected “ON” and outflow valve is fully OPEN.
LX Fail C
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched.
Mach Trim 1-2 Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched with one (1) Mach Trim System 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
MADC 1-2-3 FAIL B
(Blue – Advisory)
(GV)
(O)
Airplane may be dispatched with a one (1) micro air data computer inoperative provided:
Manual Pressurization Control System is operative,
Cabin Altitude and Differential Pressure
Indicators are operative,
Cabin Rate of Climb Indicator is operative,
Autopilot is operative,
Airplane is operated in accordance with AFM limitations,
MADC 1: POP A-9, MADC 2: CPOP A-9, and MADC 3: POP A-10 circuit breakers associated with the failed Micro Air Data Computer (MADC) are pulled and collared, and
Flight crew selects operative and different MADC sources prior to departure.
NOTE 1: Two systems are required for operation in RVSM airspace.
NOTE 2: For MADC 1 FAIL, expect the L Engine Backup Air Data advisory and associated Engine Maintenance message to post.
NOTE 3: For MADC 2 FAIL, expect the R Engine Backup Air Data advisory and associated Engine Maintenance message to post.
B
(O)
Airplane may be dispatched with one (1) micro air data computer inoperative provided airplane is operated in unpressurized configuration.
