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Sun, Oct 09, 2011

AD: General Electric Company

AD NUMBER: 2011-19-03

MANUFACTURER: General Electric Company (GE) CT7-8, CT7-8A, CT7-8A1, CT7-8E, and CT7-8F5 Turboshaft Engines
SUBJECT: Airworthiness Directive 2011-19-03
ACTION: Final rule

SUMMARY: This AD was prompted by four reports of unrecoverable engine stalls, during hover in a left-roll attitude. This AD requires the installation of an accessory gearbox (AGB) axis-A oil slinger nut to the axis-A shaft assembly. The FAA is issuing this AD to prevent an unrecoverable engine stall, leading to a helicopter forced landing or accident.

DATES: This AD is effective November 9, 2011

FMI: http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/E145658453EC8AA38625792000485D11?OpenDocument

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