# Airworthiness Directives; Boeing Model 767 Series Airplanes
> **Rule** · Final rule. · Published 1998-07-31 · Effective 1998-09-04 · 63 FR 40814
## Document
- **Document number:** 98-20340
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 767 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 40814
- **Publication date:** 1998-07-31
- **Effective date:** 1998-09-04
- **FAA docket:** Docket No. 97-NM-52-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 767 series airplanes, that requires repetitive inspections to detect corrosion or plating cracks of the pin assemblies in the forward trunnion support of the main landing gear (MLG), and replacement of the pin assembly with a new assembly, if necessary. Such replacement, if accomplished, constitutes terminating action for the repetitive inspections. This amendment is prompted by reports indicating that these pin assemblies were found to have corroded as a result of plating cracks. The actions specified by this AD are intended to detect and correct such corrosion and plating cracks, which could cause breakage of these assemblies, and consequent collapse of the MLG.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/07/31/98-20340/airworthiness-directives-boeing-model-767-series-airplanes)
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