# Airworthiness Directives; Fokker Model F27 Series Airplanes Equipped With Walter Kidde Nose Wheel Steering System
> **Rule** · Final rule. · Published 1997-02-24 · Effective 1997-03-31 · 62 FR 8156
## Document
- **Document number:** 97-4201
- **Category:** airworthiness
- **Manufacturer:** Fokker Model F27 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 62 FR 8156
- **Publication date:** 1997-02-24
- **Effective date:** 1997-03-31
- **FAA docket:** Docket No. 96-NM-38-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Fokker Model F27 series airplanes, that requires increasing the torque value of the bolt that connects the gearbox housing assembly of the steering unit to the pivot bracket of the nose landing gear (NLG). This amendment also requires that periodic inspections of that torque value be incorporated into the FAA-approved maintenance program. This amendment is prompted by several reports that the dowel pins in the Walter Kidde nose wheel steering system were found broken and/or had elongated holes due to a reduced torque value of the subject bolt. The actions specified by this AD are intended to prevent such a reduction in the torque value, which could result in failure of the dowel pins in the Walter Kidde nose wheel steering system; this situation could result in reduced controllability of the airplane or the collapse of the NLG during landing.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1997/02/24/97-4201/airworthiness-directives-fokker-model-f27-series-airplanes-equipped-with-walter-kidde-nose-wheel)
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