I have investigated both FAA and EASA regulations and am unable to conclude if there is any restriction or limitation to the validity of an FAA 8130-3 or EASA Form 1 release. So technically, any of these release documents remain valid for as long as the end-user is willing to accept them.
My question refers to aircraft components without any Time/Life limitations so OC/CM. This is just in case someone deems it relevant.
Is there any contradictory information that someone can provide or am I assessing this correctly?