The weather at the destination is forecast to be VFR (1,000 ft ceiling and three (3) miles visibility),
An alternate airport is specified in the flight plan which has VFR weather forecast (1,000 ft ceiling and three (3) miles visibility),
Both VOR and ADF navigation receivers are operative,
Flight is conducted based on short range navigation sources only being available,
Navigation suffix in the IFR flight plan clearly indicates that the airplane is not capable of any RNP required navigation capability,
Flight is conducted in airspace where the availability of navigation by short range navigation receivers (VOR/ADF) is assured,
One DBDI or Standby RMI or Secondary Navigation Display is operative,
Alternate procedures are established and used,
Flight crew pull and collar associated Display Controller circuit breaker,
Flight crew prepare and display a TOLD (Takeoff and Landing Data) card prior to takeoff and prior to approach and landing (GV only),
Flight crew verify required approaches are available at the destination and alternate airports without being NOTAMed out of service or unusable,
Pilot-Not-Flying (PNF) is prepared to announce approach minimums in the event the operative Display Controller fails en route, and
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
DME 1-2 Fail C
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched except where en route operations or approach minimums require its use. Any in excess of those required by 14 CFR may be inoperative.
EGPWM SYS 1-2 Fail B
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched.
NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction.
Elevator Trim 1-2 Fail B
(Amber – Caution)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched with electric elevator trim inoperative provided:
Electric Elevator Trim remains OFF,
Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and
Airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach).
ELEV TRIM INOP B
(Amber – Caution)
(GV)
(O)
Airplane may be dispatched with electric elevator trim inoperative provided:
Electric Elevator Trim remains OFF,
Both Flap/Stabilizer Control Channels are operative (no messages on CAS), and
Airplane is operated in accordance with AFM Limitations (Maximum Operating Limit Speed 0.80 Mach).
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
Engine Maintenance ###, L-RA
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided:
Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and
FADEC faults are reviewed by flight crew before each takeoff.
NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours.
Engine Maintenance LTD, L-RA
(Blue – Advisory)
(GV-SP/GIV-X)
(O)
Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided:
Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and
FADEC faults are reviewed by flight crew before each takeoff.
NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours.
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
ENG MAINT ###, L-R A
(Blue – Advisory)
(GV)
(O)
Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided:
Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and
FADEC faults are reviewed by flight crew before each takeoff.
NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours.
ENG MAINT LTD, L-R A
(Blue – Advisory)
(GV)
(O)
Airplane may be dispatched with Blue “Engine Maintenance STD (###)” and/or “Engine Maintenance LTD” messages displayed on EICAS provided:
Repairs are made in accordance with times (hours) established by the BR 710-A1 Time Limits Manual (GV), Chapter 5 or BR 710-C4 Time Limits Manual (GV-SP), Chapter 5 (no extensions are authorized), and
FADEC faults are reviewed by flight crew before each takeoff.
NOTE: Blue “Engine Maintenance STD (###) messages require maintenance action within 150 hours and Blue “Engine Maintenance LTD” messages required maintenance action within 500 hours.
Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and
Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and
Repairs are made within three (3) flight days.
FDR System Fail A
(Blue – Advisory)
(GV-SP/GIV-X)
Airplane may be dispatched provided:
Cockpit Voice Recorder (CVR) is operative,
Airplane is not dispatched from a designated airport as listed in the operator’s MEL unless the FDR failure occurs after pushback but before takeoff, and
Repairs are made within three (3) flight days.
FGC 1-2 FAIL B
(Amber – Caution)
(GV)
(O)
Except for ER operations or where en route operations or approach minimums require its use, airplane may be dispatched with one (1) failed provided airplane is operated in accordance with AFM Limitations in the event the operative FGC fails and the Yaw Damper is inoperative.
NOTE: FGC is required for MNPS, RVSM, RNP and PRNAV operations.
