Docket No. FAA-2012-0860;
Directorate Identifier 2012-NM-123-AD
In paragraph of (h) "Parts Installation Prohibition" , it is described that only TA0930034-10 can be installed
within the left ECS bay of any airplane,
however, SB 737-28-1303 directs to inspect the clamp on the specified one or two loacation(s) depending on the group of airplanes.
Thus, JAL believes that the location should be specified where the TA0930034-10 clamp shoud be installed in the AD.
Japan Airlines
This is comment on Proposed Rule
Airworthiness Directives: The Boeing Company Airplanes
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