Aging Airplane Program: Widespread Fatigue Damage; Technical Amendment
The FAA is correcting a final rule published on November 15, 2010. That rule required design approval holders of certain existing airplanes and all applicants for type certificates of future transport category airplanes to establish a limit of validity of the engineering data that supports the structural maintenance program (hereinafter referred to as LOV). It also required that operators of any affected airplane incorporate the LOV into the maintenance program for that airplane. This document corrects errors in codified text of that document.