Airworthiness Directives; McDonnell Douglas Model MD-90-30 Series Airplanes
airworthiness · Rule · Final rule. · Published 2000-02-16 · Effective 2000-03-22 · 65 FR 7719
Document
Document number
00-3396
Federal Register citation
65 FR 7719
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model MD-90-30 Series
Publication date
2000-02-16
Effective date
2000-03-22
FAA docket
Docket No. 99-NM-210-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-90-30 series airplanes, that requires repetitive fluorescent penetrant and magnetic particle inspections to detect fatigue cracking of the main landing gear (MLG) piston, and repair, if necessary. This amendment is prompted by reports of MLG failures during towing of in-service airplanes due to fatigue cracks. The actions specified by this AD are intended to detect and correct fatigue cracking of MLG pistons, which could result in failure of the pistons, and consequent damage to the airplane structure and injury to flight crew, passengers, or ground personnel.