Airworthiness Directives; Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 Series Airplanes
airworthiness · Rule · Final rule. · Published 2007-06-05 · Effective 2007-07-10 · 72 FR 30959
Document
Document number
E7-10670
Federal Register citation
72 FR 30959
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-06-05
Effective date
2007-07-10
FAA docket
Docket No. FAA-2007-27713
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD requires, for certain airplanes, modification of the upper bearing of the main landing gear (MLG) shock strut. This AD also requires, for certain airplanes, revising the de Havilland DHC-8 Maintenance Program Manual to include the MLG shock strut servicing task. This AD results from reports of over-extension of the MLG shock strut piston, which allows the torque links to go over-center and rest on the piston. We are issuing this AD to prevent loss in shock absorption during touchdown and failure of the shock strut housing, which could result in a subsequent loss of directional control.