Virgin America

Document ID: FAA-2008-0174-0003
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: June 16 2008, at 10:35 AM Eastern Daylight Time
Date Posted: June 17 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: May 7 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: July 7 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 80628c70
View Document:

This is comment on Rule

Airworthiness Directives; CFM International, S.A. CFM56-5B1/P; - 5B2/P; -5B3/P; -5B3/P1; -5B4/P; -5B4/P1; -5B5/P; -5B6/P; -5B7/P; -5B8/ P; and -5B9/P Turbofan Engines

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This proposed AD would require initial and repetitive eddy current inspections (ECIs) of certain part number (P/N) low-pressure (LP) turbine rear frames P/Ns 338-171-703- 0; 338-171-704- 0; 338-171-705-0; and 338-171-706-0. Please consider expanding the applicability section to include model 5B4/3 and 5B6/3 since review of recent delivery records of these engines shows installation of P/N 338- 171-705-0 LP turbine rear Frames installed.

Related Comments

Total: 3

Airbus
Public Submission Posted: 05/16/2008 ID: FAA-2008-0174-0002

Comment Period Closed
Jul 07,2008 11:59 PM ET

Virgin America
Public Submission Posted: 06/17/2008 ID: FAA-2008-0174-0003

Comment Period Closed
Jul 07,2008 11:59 PM ET

CFM International
Public Submission Posted: 07/08/2008 ID: FAA-2008-0174-0004

Comment Period Closed
Jul 07,2008 11:59 PM ET