Airworthiness Directives; McDonnell Douglas Model MD-90-30 Airplanes
airworthiness · Rule · Final rule. · Published 2005-06-24 · Effective 2005-07-29 · 70 FR 36479
Document
Document number
05-12313
Federal Register citation
70 FR 36479
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model MD-90-30
Publication date
2005-06-24
Effective date
2005-07-29
FAA docket
Docket No. FAA-2004-19867
Abstract
The FAA is adopting a new airworthiness directive (AD) for all McDonnell Douglas Model MD-90-30 airplanes. This AD requires replacing existing dual anti-skid control manifolds (DACM) with new, improved or reworked and reidentified DACMs; inspecting the inlet filters and other components of the DACMs for damage; replacing any damaged DACM components with new or serviceable components; and flushing/cleaning the braking system prior to replacing the inlet filters. This AD is prompted by reports of multiple incidents of blown tires on landing while using maximum autobrake. We are issuing this AD to prevent metallic fibers from the first stage filter of the servo valves inside the DACM from becoming lodged in the first stage nozzle of the servo valve, which could lead to tire failure during high speed/high energy braking and possible subsequent runway departure.