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Airworthiness Directives; General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2007-04-06 · Effective 2007-04-23 · 72 FR 16998

Document

Document number
E7-6345
Federal Register citation
72 FR 16998
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2007-04-06
Effective date
2007-04-23
FAA docket
Docket No. FAA-2007-27687

Abstract

The FAA is superseding an existing airworthiness directive (AD) for General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines. That AD requires a onetime inspection of certain fan disks for electrical arc-out indications, replacing fan disks with electrical arc-out indications, and reducing the life limit of certain fan disks. This AD requires the same reduced life limit of certain fan disks, but requires on-wing inspection of certain fan disks installed on regional jets within 500 flight hours after the effective date of this AD. This AD also requires more enhanced shop-level inspections of all fan disks for electrical arc-out defects. This AD results from a report that in January 2007, a CF34-3B1 turbofan engine experienced an uncontained fan disk failure during flight operation. We are issuing this AD to prevent an uncontained fan disk failure and airplane damage.

Source

Authoritative
Federal Register document
Machine
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