Summary
The FAA is adopting a new airworthiness directive (AD) for a GE CF6-80C2B1 turbofan engine, serial number (SN) 690203, with fan disk, part number (P/N) 1703M78P11, SN RPMDA662, installed. This AD requires stripping of thermal spray coating, inspection of dovetail slots, and reapplication of thermal spray coating on certain stage 1 fan disks. This AD results from a report that a repair shop did not meet the process requirements when applying copper-nickel-indium (Cu- Ni-In) thermal coating to certain stage 1 fan disks. We are issuing this AD to prevent possible uncontained release of multiple fan blades, resulting in damage to the airplane.
Directive Details
AD Number
FAA-2007-0193
Document Number
E7-22922
Type
Rule
Publication Date
November 28, 2007
Effective Date
January 2, 2008
Affected Manufacturer
General Electric Company (GE) CF6-80C2B1 Turbofan
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2007-0193
Topics
Official Documents
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