The F/A-18L version followed to coincide with the US Navy's F/A-18A as a land-based export alternative. This was essentially an F/A-18A lightened by approximately 2,500 to 3,000 pounds (1,130 to 1,360 kg); weight was reduced by removing the folding wing and associated actuators, by implementing a simpler landing gear (single wheel nose gear and
cantilever oleo main gear), and change to a land-based tail-hook. The revised F/A-18L included wing fuel tanks and fuselage stations of the F/A-18A. Its weapons capacity would increase from 13,700 to 20,000 pounds (6,210 to 9,070 kg); largely due to the addition of a third underwing pylon and strengthened wingtips (11 stations in total vs 9 stations of the F/A-18A). Compared to the F-18L, the outboard weapons pylons are moved closer to the wingtip missile rails. Because of the strengthened non-folding wing, the wingtip missile rails were designed to carry either the
AIM-7 Sparrow or
Skyflash medium-range air-to-air missiles, in addition to the
AIM-9 Sidewinder as found on the F/A-18A. The F/A-18L was strengthened for a 9 g design load factor compared to the F/A-18A's 7.5 g factor
now couldn't you do the same weight reduction to the F/A-18 E/F?? knocking off 2,500 to 3,000 pounds and making it faster, longer ranged and more maneuverable seems very attractive option to me. especially for India and Canada who would use it from the ground and not on a carrier.