# Airworthiness Directives; Fokker Model F.28 Mark 0100 Series Airplanes
> **Rule** · Final rule. · Published 1998-06-25 · Effective 1998-07-30 · 63 FR 34581
## Document
- **Document number:** 98-16498
- **Category:** airworthiness
- **Manufacturer:** Fokker Model F.28 Mark 0100 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 34581
- **Publication date:** 1998-06-25
- **Effective date:** 1998-07-30
- **FAA docket:** Docket No. 97-NM-329-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Fokker Model F.28 Mark 0100 series airplanes, that requires interim inspections to detect discrepancies of the main fitting subassembly of the main landing gear, and follow-on corrective actions, if necessary. This amendment also requires a one-time inspection to detect discrepancies of the fitting, repair of the fitting, if necessary, and application of new surface protection on the fitting, which would terminate the interim inspections. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent cracking of the main fitting subassembly of the main landing gear, which could result in collapse of the main landing gear.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/06/25/98-16498/airworthiness-directives-fokker-model-f28-mark-0100-series-airplanes)
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