Southwest Airlines has two comments for AD 2012-26-14.
1. Southwest Airlines request that the AD include the part numbers of the affected HPC Stage 1-6 Rotor Disk Assemblies.
2. In addition please clarify Paragraph (f), which states that performing the one-time removal from service is terminating action. Per this AD is it acceptable to reinstall parts with less than the cycle limits called out in paragraph (e)? Please clarify if it is the intent of this AD to establish a new life limit for the affected parts?
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Total: 1
Southwest Airlines Public SubmissionPosted: 02/27/2013
ID: FAA-2012-1202-0002
Southwest Airlines
This is comment on Rule
Airworthiness Directives: Rolls-Royce Deutschland Ltd and Co. KG Turbofan Engines
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Public Submission Posted: 02/27/2013 ID: FAA-2012-1202-0002
Feb 25,2013 11:59 PM ET