The problem with any heavy G load, momentary or sustained, is that the air is seldom glassy smooth. Any "bump" in the air, whether due to thermal action, mountain wave, or shears or vorticity, or even somebody else's wake turbulence, while near the flight load limit will flex the structure into its plastic range, where it won't immediately fail, but will accumulate stress cracks which weaken its reserve strength. Repeated excursions will increase its range of flexibility and lower the plastic threshold at which damage accumulates. Eventually you have a "clapped out" aircraft that has a dramatically lowered ultimate G load.As far as momentary G forces, like pulling out of a dive, I don't know how they weigh or rate momentary versus sustained "G" forces.
Now put said aircraft in a high G maneuver and start punching .50 cal or 20 MM holes in critical structural members, and you're likely to see some pretty drastic consequences. Contrary to popular conception, the first things to fail are apt to be the horizontal stabilizer or the engine mount structure, either of which will generate a pitch up or down that instantly overstresses the wings.
I'm not an engineer, so I may have misused some of the terminology here. Any of you who are, feel free to correct me on this. (In "everyday language" if you can.)
Cheers,
Wes
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