Summary
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for discrepancies of the elevator tab control rod assemblies and/or damage to the surrounding structure, and related corrective action. This AD results from reports indicating loose jam nuts and/or thread wear at the rod ends on the elevator tab control rod assembly. We are issuing this AD to find and fix discrepancies of the elevator tab control rod assembly, which could result in excessive freeplay in the elevator tab control rods. Such freeplay could cause loss of both load paths, subsequent elevator tab flutter, and consequent reduced structural integrity and loss of controllability of the airplane.
Directive Details
AD Number
FAA-2004-18814
Document Number
E7-15220
Type
Rule
Publication Date
August 9, 2007
Effective Date
September 13, 2007
Affected Manufacturer
Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2004-18814
Topics
Official Documents
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