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AD FAA-2017-1000

Airworthiness Directives; General Electric Company Turbofan Engines

Summary

We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) CF34-8C1, CF34-8C5, CF34-8C5A1, and CF34- 8C5B1 engines. This AD requires an inspection of the bleed air manifold link rod assemblies and the supply, return, and drain fuel fittings on the operability bleed valve (OBV). This AD was prompted by an engine fire that occurred as a result of malfunctions related to the OBV. We are issuing this AD to address the unsafe condition on these products.

Directive Details

AD Number

FAA-2017-1000

Document Number

2017-24700

Type

Rule

Publication Date

November 15, 2017

Effective Date

November 30, 2017

Affected Manufacturer

General Electric Company Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2017-1000

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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