Summary
The FAA proposes to adopt a new airworthiness directive (AD) for General Electric Company Model CF6-80C2D1F turbofan engines. This proposed AD would require modifying the latching system of the fan reverser. This proposed AD results from 13 reports of released thrust reverser hardware. We are proposing this AD to prevent release of the thrust reverser cascade on landing, which could result in runway debris and a possible hazard to other aircraft.