FedEx Express has conducted a review of our fleet and stock and determined that
we have no Stage 1 HPT disks with the subject suspect part numbers in our
system. This proposed rule will therefore not directly affect our operation and at
this time we feel that no further action on our part will be required to meet future
compliance requirements if the AD is released in its current form.
FedEx would, however, like to make a general comment on one aspect of the
proposed rule both in general support of the industry and as a potential hedge
against similar requirements in future rules. We feel that the FAA has greatly
underestimated the actual cost impact that accomplishment of this AD would
impose on an operator required to comply with it. The NPRM states that it is
estimated that removal of the Stage 1 HPT disk would require only 1 work-hour
and hence the labor cost of the proposed AD is only $80 per engine. This work
estimate is only accurate if the engine is already removed and disassembled to
the point of piece part exposure of the disk. As this AD would require removal of
the affected disks within 30 days of issuance (as opposed to at next part
exposure), in all likilihood compliance would neccessitate early removal of an
engine from service and an unplanned shop visit to perform the required operation.
The true cost to an airline, both in disruption to the operation and in the
subsequent shop visit, would vastly exceed the given estimate of $300,080 per
engine and $900,240 total.
Related Comments
Total: 2
FedEx Express Public SubmissionPosted: 09/25/2008
ID: FAA-2008-0827-0002
FedEx Express
This is comment on Rule
Airworthiness Directives; General Electric Company (GE) CF6-80A Series Turbofan Engines
View Comment
Related Comments
Public Submission Posted: 09/25/2008 ID: FAA-2008-0827-0002
Nov 03,2008 11:59 PM ET
Public Submission Posted: 10/15/2008 ID: FAA-2008-0827-0003
Nov 03,2008 11:59 PM ET