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Old 28th Aug 2021, 12:45
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Goldenrivett
 
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Hi tcasblue,

Wikipedia has a good explanation.

Another weight-saving concept the designers came up with was detachable wingtips. The wings were designed to fold at a point about 2⁄3 out along the span, reducing the space taken up on the carrier. Normally the hinge system would have to be built very strong in order to transmit loads from the outer portions of the wing to the main spar in the inner section, which adds considerable weight. Instead of building the entire wing to be able to withstand high-g loads, only the inner portion of the wing was able to do this. The outer portions were more lightly constructed, and designed to snap off at the hinge line if the g-force exceeded 7.5 g. In this case the aircraft would still be flyable and could be repaired after returning to the carrier. This saved 230 pounds (100 kg) of weight.”
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