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importantRule

AD FAA-2011-0187

Airworthiness Directives; General Electric Company CF34-10E2A1; CF34-10E5; CF34-10E5A1; CF34-10E6; CF34-10E6A1; CF34-10E7; and CF34-10E7-B Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for the products listed above with certain part number (P/N) fan rotor spinners installed. This AD requires removing from service certain fan rotor blade retainers, and removing from service the fan rotor spinner support that was installed with those fan rotor blade retainers. This AD was prompted by a fan rotor spinner support found cracked at the attachment lugs. We are issuing this AD to prevent high-cycle fatigue cracking of the fan rotor spinner support attachment lugs, leading to separation of the fan rotor spinner assembly, uncontained failure of the engine, and damage to the airplane.

Directive Details

AD Number

FAA-2011-0187

Document Number

2011-21313

Type

Rule

Publication Date

August 22, 2011

Effective Date

September 26, 2011

Affected Manufacturer

General Electric Company CF34-10E2A1

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2011-0187

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for General Electric Company CF34-10E2A1 →

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