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AD FAA-2007-0193

Airworthiness Directives; General Electric Company (GE) CF6-80C2B1 Turbofan Engine

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

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for General Electric Company (GE) CF6-80C2B1 Turbofan →

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