Airworthiness Directives; Fokker Model F27 Series Airplanes Equipped With Walter Kidde Nose Wheel Steering System
airworthiness · Rule · Final rule. · Published 1997-02-24 · Effective 1997-03-31 · 62 FR 8156
Document
Document number
97-4201
Federal Register citation
62 FR 8156
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Model F27 Series
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.