Summary
We are adopting a new airworthiness directive (AD) for certain Boeing Model 767-200 and 767-300 series airplanes. This AD requires detailed inspections of the aft pressure bulkhead for damage, mid- frequency eddy current (MFEC) and low frequency eddy current (LFEC) inspections of radial web lap splices, tear strap splices, and super tear strap splices for cracking, and corrective actions if necessary. This AD results from analysis that indicates fatigue cracks of the web lap splice, tear strap splice, or super tear strap splice of the aft bulkhead are expected to occur on certain Boeing Model 767-200 and 767- 300 series airplanes. We are issuing this AD to detect and correct fatigue cracks of the aft pressure bulkhead, which could result in rapid decompression of the passenger compartment and possible damage or interference with airplane control systems that penetrate the bulkhead, and consequent loss of controllability of the airplane.
Directive Details
AD Number
FAA-2008-0898
Document Number
E9-5961
Type
Rule
Publication Date
March 24, 2009
Effective Date
April 28, 2009
Affected Manufacturer
Boeing Model 767-200 and 767-300 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2008-0898
Topics
Official Documents
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