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Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes

airworthiness · Rule · Final rule. · Published 2007-08-09 · Effective 2007-09-13 · 72 FR 44744

Document

Document number
E7-15220
Federal Register citation
72 FR 44744
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-08-09
Effective date
2007-09-13
FAA docket
Docket No. FAA-2004-18814

Abstract

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.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown