Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F Airplanes
airworthiness · Rule · Final rule. · Published 2008-05-02 · Effective 2008-06-06 · 73 FR 24155
Document
Document number
E8-9439
Federal Register citation
73 FR 24155
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-05-02
Effective date
2008-06-06
FAA docket
Docket No. FAA-2008-0015
Abstract
We are adopting a new airworthiness directive (AD) for certain McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, and MD-10-10F airplanes. This AD requires repetitive inspections for the presence of stray nickel or chrome plating deposits on the air filler valve bore of certain main landing gear (MLG) shock strut cylinders, and if necessary, related investigative and corrective actions. Doing the corrective action terminates the repetitive inspections. This AD results from a report of a left MLG collapse during landing rollout. We are issuing this AD to detect and correct stray nickel and chrome plating deposits, corrosion, and cracking of the air filler valve bore on the MLG cylinder, which could result in landing gear failure, significant damage to the airplane, and injury to personnel.