The fwd entry door is the biggest and heaviest one, and the hinges and mechanisms tend to wear out much more due to the heavy load of the door.
My experience is that it is possible to close the door, but due to the upper hinge wear the upper aft guide latch may be turned but not into the recess. So the door looks closed (from the inside) but the upper half is still an inch inward and not flush with the fuselage at the aft latch. The fwd latch is always ok, the aft upper latch isnt.
So you may close the door normally and it is still not flush at the upper half aft side.
That gives a false idea of a closed door while it is not. The original switch may then be closed so the cockpit crew thinks it is ok.
The others doors are much smaller and lighter and especially the aft doors move in a horizontal line which wears out the hinges much less.
The fwd rh door is smaller and lighter as well and so far it may not have caused so many issues with th hinges as the big lh fwd door,
So the extra switch is a typical boeing solution. Not making the hinges stronger but installing an extra switch to monitor the latch.
(do you remember the flap input cable switch at the aft rh side under the cabin floor on the 737 classic? Typical a boeing solution. Making a switch to monitor if the cable breaks giving you a flap bypass situation. pfff)
I always refer to this boeing solution: Its not looking for the headache cause but gives a pill against the headache. Problem solved.
