# Airworthiness Directives; McDonnell Douglas Model MD-90-30 Series Airplanes
> **Rule** · Final rule. · Published 2000-02-16 · Effective 2000-03-22 · 65 FR 7719
## Document
- **Document number:** 00-3396
- **Category:** airworthiness
- **Manufacturer:** McDonnell Douglas Model MD-90-30 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 7719
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/02/16/00-3396/airworthiness-directives-mcdonnell-douglas-model-md-90-30-series-airplanes)
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