2011-23-04: Forward engine mount assembly side links
FAA order 2011-23-04 is an airworthiness directive in force since December 12, 2011. The FAA's subject line: Forward engine mount assembly side links. It names the General Electric CF6-45A2, General Electric CF6-50C, General Electric CF6-50C2, General Electric CF6-80 series, General Electric CF6-80A, General Electric CF6-80A2 engines: about 263 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.
What it applies to as the FAA lists it
- Kind of product
- Engine
- Makes
- General Electric Company
- Models
- CF6-45A, CF6-45A2, CF6-50A, CF6-50C, CF6-50C1, CF6-50C2, CF6-50C2B, CF6-50C2D, CF6-50CA, CF6-50E, CF6-50E1, CF6-50E2, CF6-50E2B, CF6-80A, CF6-80A1, CF6-80A2, CF6-80A3
- Engine series
- General Electric CF6-45A2 1 aircraft
General Electric CF6-50C 1 aircraft
General Electric CF6-50C2 10 aircraft
General Electric CF6-80 series 237 aircraft
General Electric CF6-80A 9 aircraft
General Electric CF6-80A2 5 aircraft
Dates and paperwork
- In force since
- December 12, 2011
- Published
- November 7, 2011 (signed October 26, 2011)
- Docket
- FAA-2010-1151
- Replaces
- 2006-12-24
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The FAA's summary their words, unchanged
We are superseding an existing airworthiness directive (AD) for the engines identified above. That AD currently requires initial and repetitive visual inspections of the forward engine mount assembly side links for cracks, stripping and reapplying the Sermetel W coating on the side links at every exposure of the side link. This new AD requires those same inspections, stripping and reapplying the Sermetel W coating, and adds two part numbers [[Page 68635]] to the applicability. This AD was prompted by a review of the inspection program, which revealed that GE had omitted two affected side link part numbers from the applicability. We are issuing this AD to prevent failure of the side links and possible engine separation from the airplane.
The order itself the regulatory text, as published
Show the full text (4,473 characters)
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/2011-23-04.json · aircraft systems.
