Aircraft General - Gulfstream G650

Aircraft General

• The Gulfstream G650 has a total fuel capacity of 44,200 lbs.
• The cabin length for the Gulfstream G650 is 46.88 feet.
• The maximum ramp weight for the Gulfstream G650ER is 104,000 lbs.
• The single-point pressure fueling adapter for the Gulfstream G650 is located on the forward right wing-to-body fairing.
• The optimal range for fueling nozzle pressure during fueling operations is 35 to 55 psi.
• The parking brake accumulator pressure should read 3,000 psi for a full charge.
• The APU oil tank holds 4.5 quarts of oil.
• The Gulfstream G650 hydraulic system uses Phosphate-Ester Type IV/V (SKYDROL) hydraulic fluid.
• The left hydraulic system reservoir holds 4.5 gallons when serviced.
• The nose jacking point on the Gulfstream G650 is located at Fuselage Station (FS) 224.1.
• The optimal tire pressure for the Gulfstream G650 is 216 psig.
• The hydraulic service panel is located on the aircraft belly, just forward of the tail compartment access door.
• The Integrated Drive Generator (IDG) oil system has a capacity of 3.4 to 4.15 quarts.
• The measurement used to locate points, components, and distances above a theoretical datum line on the Gulfstream G650 is Waterline (WL).
• The exterior wingspan of the G650 is 99.6 feet.
• The maximum allowable aft center of gravity for the Gulfstream G650 is FS 708.8.
• The landing gear blowdown bottles are located in the nose wheel well.
• The total baggage compartment volume of the Gulfstream G650 is 195 cu ft.
• Electronic equipment should be energized once a week during storage.
• The Gulfstream G650 uses a high-pressure gaseous oxygen system.
• The right hydraulic system has a total capacity of 14.8 U.S. gallons.
• The leveling bracket for longitudinal leveling is located at Fuselage Station (FS) 148.5.
• The standard servicing fluid for the landing gear struts on the Gulfstream G650 is MIL-PRF-5606.