Stricter structural limits are in place for Navy aircraft to avoid premature airframe wearing.
Actually NO! everybody wants their bird to pull 9g's, but the Navy F-35C has larger wings and stabilator in order to create more lift at a given airspeed, the F-35C needed larger wings to meet the maximum over the fantail speed of 145 knots,, the A model would prolly want to be pulling 165 knots over the fantail, so the wing area had to be increased and the stabilator size was also increased to get that girl to have similar pitch transitions to the A model, which has been to 9.9Gs in test.
The Navy bird is indeed heavier, and that is also a big factor, more wing, more lift, more weight, more fuel,, all adds up to a lower g limit in order not to break the wing attach/center fuselage juncture.
The B model with small wings is limited to 7gs as the lift fan, STOVL equipment displaces the back-bone of the airframe, which is split in order to run around the lift fan and associated hardware...
The Super Hornet is prolly rated at 7 to 7.5gs positive as well, so not a new thing for Navy, but the airframe life on traditional fighters is limited by the number of CAT's and TRAP's as they put a great deal of additional stress on the airframe,,,, once they reach that limit, they are no longer carrier qualed, they are then land based for the rest of their airframe lives until they "time-out".