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Airworthiness Directives; McDonnell Douglas Model 717-200 Airplanes

airworthiness · Rule · Final rule. · Published 2004-04-14 · Effective 2004-05-19 · 69 FR 19758

Document

Document number
04-8299
Federal Register citation
69 FR 19758
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model 717-200
Publication date
2004-04-14
Effective date
2004-05-19
FAA docket
Docket No. 2002-NM-212-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model 717-200 airplanes, that requires a general visual inspection to detect corrosion of the left- and right-hand horizontal stabilizer hinge fitting bolts, barrel nuts, and the associated holes in the horizontal stabilizer structure, and to detect corrosion of the left- and right-hand elevator sector pinch bolts and associated holes, as applicable; and corrective actions, if necessary. This action is necessary to detect and correct corrosion of the left- and right-hand horizontal stabilizer hinge fitting bolts, barrel nuts, and associated holes in the horizontal stabilizer structure, and the left- and right-hand elevator sector pinch bolts and associated holes, which could lead to loss of a hinge fitting and reduced structural integrity of the horizontal stabilizer. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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