Kevin Allen Murray

Document ID: FAA-2009-0328-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: April 15 2009, at 11:34 AM Eastern Daylight Time
Date Posted: April 15 2009, at 12:00 AM Eastern Standard Time
Comment Start Date: April 8 2009, at 12:00 AM Eastern Standard Time
Comment Due Date: June 8 2009, at 11:59 PM Eastern Standard Time
Tracking Number: 809544b9
View Document:

This is comment on Rule

Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines

View Comment

This comment concerns the purposed AD (Docket No. FAA–2009–0328; Directorate Identifier 2008–NE–44–AD; RIN 2120–AA64) for the CF-34 engine fan blades. The initial Eddy current inspection for the CF34–1A, CF34–3A, CF34– 3A2, CF34–3B, and CF34–3A1 Engines does not contain instruction for fan blades that have more than 1200 cycles on the effective date of the AD. These instructions must be included in the final version of said AD.