As of printing time, the Super Hornet's flight test data on loadout possibilities are largely inconclusive. However, takeoff weights have already exceeded 33 tons. At NAS Patuxent River, Maryland, Northrop Grumman test pilot Jim Sandberg flew test plane E1 with an "Aero Servo Elasticity" stores configuration weighing in at 62,400 lbs (28,364 kg). This loadout comprised three 480-gallon tanks, two 2,000-lb Mk 84 bombs, two AIM-9s and two HARM missiles. Compare this to the Hornet's maximum gross takeoff weight of 51,900 lbs (23,537 kg), an increase of 10,500 lbs (4,287 kg).
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4.2.3 Fuel Consumption
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Whereas all these hardpoints are capable of receiving various offensive weaponry, they infrequently do so operationally. One reason is the F/A-18's propensity for high fuel consumption. As one of the Fleet's more consistent "gas hogs", Hornets rarely undertake a flight without two, or even three, drop tanks. Usually wing stations 3 and 7 are devoted to them, consuming 5,000+ lbs (2,273+ kg) of loadout weight outright. This also applies to the centerline station. In additon, the two intake stations are often reserved for sensors. This leaves but the two outboard wing pylons and wingtip rails for ordnance.