AD 2006-06-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | General Electric | Company Model CF6-80C2D1F | Airworthiness Directives; General Electric Company Model CF6-80C2D1F Turbofan Engines |
Unsafe Condition
13 reports of released thrust reverser hardware. Release of the thrust reverser cascade on landing could result in runway debris and a possible hazard to other aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the latching system of the fan reverser using the Accomplishment Instructions of either MRAS Service Bulletin No. CF6-80C2 S/B 78-1068, Revision 2, or SB No. CF6-80C2 S/B 78-1077, Revision 1, dated May 16, 2005 (but not both).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,200 flight hours for paragraph (f), within 6,000 flight hours for paragraphs (g) and (h).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
General Electric Company Model CF6-80C2D1F turbofan engines that have not incorporated specific Middle River Aircraft Systems Service Bulletins (SBs) as listed in the AD. These engines are installed on, but not limited to, McDonnell Douglas Corporation MD-11 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.