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| Page | 26/60 | | Date | 02.02.2017 | | Size | 6.47 Mb. | | #15690 |
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
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AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 7
DATE: 02/04/2010
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PAGE NO:
27-2
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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27
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FLIGHT CONTROLS
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8. ***
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Elevator Trim Actuator Heater Systems
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C
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2
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0
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(M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared.
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9. ***
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Aileron Trim Actuator Heater
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C
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1
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0
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(M)(O) May be inoperative provided affected circuit breaker(s) are pulled and collared.
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10.
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Autopilot Elevator Servos, (GV-SP,
GIV-X)
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C
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2
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1
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(M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared.
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11.
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Autopilot Pitch Trim Servos (GV-SP,
GIV-X)
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C
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2
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1
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(M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared.
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12.
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Autopilot Aileron Servos (GV-SP,
GIV-X)
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C
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2
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1
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(M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared.
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13.
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Autopilot Yaw Damper Servos (GV-SP,
GIV-X)
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C
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2
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1
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(M) May be inoperative provided the inoperative servo circuit breaker(s) is pulled and collared.
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14.
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Stall Barrier Systems
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A
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2
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1
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(M)(O) May be inoperative provided:
a) Angle of Attack indication is available on both PFD’s,
b) Alternate procedures are established and used,
c) The inoperative stall barrier system is electrically disabled, and
d) Repairs are made within two (2) flight days.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
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AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 8
DATE: 11/07/2014
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PAGE NO:
27-3
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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27
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FLIGHT CONTROLS
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15.
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Flight Control Synoptic Display (GV)
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C
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1
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0
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May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight.
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(GV-SP, GIV-X)
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C
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-
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0
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May be inoperative provided the affected control surface is visually checked for full, free and correct movement prior to each flight.
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16.
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Gust Lock
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C
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1
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0
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(O) May be inoperative provided flight controls are secured in an alternate manner.
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C
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1
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0
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(O) May be inoperative provided airplane is parked in sheltered area unaffected by atmospheric conditions.
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
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AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 7
DATE: 02/04/2010
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PAGE NO:
28-1
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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28
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FUEL
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1.
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Fuel Tank Temperature Systems
(GV, GV-SP)
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C
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2
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0
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(O) May be inoperative provided:
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Total Air Temperature is used as an indication of fuel temperature, and
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Airplane is operated in accordance with AFM Limitations.
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Fuel Tank Temperature System
(GIV-X)
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C
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1
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0
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(O) May be inoperative provided:
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Total Air Temperature is used as an indication of fuel temperature, and
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Airplane is operated in accordance with AFM Limitations.
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2.
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EICAS or Standby RFMU (GV) /
MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems
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C
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2
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1
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(M)(O) May be inoperative provided associated Standby Fuel Quantity Indicating System or EICAS Fuel Quantity Indicating System is operative.
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(continued)
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
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AIRCRAFT:
GULFSTREAM G-V, GV-SP,
GV-SP (G550), GV-SP (G500),
GIV-X, GIV-X (G450),
GIV-X (G350)
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REVISION NO: 7
DATE: 02/04/2010
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PAGE NO:
28-2
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1. SYSTEM,
SEQUENCE NUMBERS & ITEM
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REPAIR CATEGORY
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2. NUMBER INSTALLED
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3. NUMBER REQUIRED FOR DISPATCH
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4. REMARKS OR EXCEPTIONS
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28
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FUEL
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2.
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EICAS or Standby RFMU (GV) /
MCDU (GV-SP, GIV-X) Fuel Quantity Indicating Systems (continued)
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C
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2
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1
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(M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided:
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Both tanks are completely filled using overwing refueling,
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Both fuel flow meters are operative,
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After takeoff, power is set by matching fuel flow indications on both engines, and
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Flight crew maintains a log of fuel burned.
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C
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2
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1
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(M)(O) Except for ER operations, either Left or Right Fuel Quantity display may be inoperative provided:
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Affected tank is defueled before each refueling,
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Affected tank is fueled with a known quantity of fuel,
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Both fuel flow meters are operative,
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After takeoff, power is set by matching fuel flow indications on both engines, and
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Flight crew maintains a log of fuel burned.
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NOTE: Total Fuel indications will be invalid with an inoperative indicator.
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