JAL Engineering

Document ID: FAA-2012-0856-0010
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: October 04 2012, at 12:00 AM Eastern Daylight Time
Date Posted: October 11 2012, at 12:00 AM Eastern Standard Time
Comment Start Date: August 21 2012, at 12:00 AM Eastern Standard Time
Comment Due Date: October 5 2012, at 11:59 PM Eastern Standard Time
Tracking Number: 1jw-817j-kp63
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This is comment on Proposed Rule

Airworthiness Directives: The Boeing Co. Airplanes

View Comment

JAL Engineering is a MRO and has a contract with JAG to do all heavy maintenances for JAG747-400 (RT681, 682) airplanes. When we evaluate the BSB747-25-3381 R1, we had a question about FWD & Aft cargo compartment light area per this SB Figure16 view I. When we researched the airplane, there was no foam installed around cargo light as attached photos. Also the cargo light p/n BR7203-701 doesn't contain any foam as attached. Thus JAL can't identify the existence of the foam pad which is required to remove by SB747-25-3381 R1 Figure 16 View I. So we asked Boeing if the SB revise to indicate that these light areas are typical locations as attached. But the revised SB doesn't reflect this comment. So we would like FAA to give a permission for the applicability of the SB Figure 16 View I only if the foam pad exists. Regards, Egami JAL Engineering

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