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Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes; and Model DHC-8-200 and DHC-8-300 Series Airplanes

airworthiness · Rule · Final rule. · Published 2007-02-27 · Effective 2007-04-03 · 72 FR 8619

Document

Document number
E7-2972
Federal Register citation
72 FR 8619
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-02-27
Effective date
2007-04-03
FAA docket
Docket No. FAA-2006-26558

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100 (as described above), DHC-8-200, and DHC-8-300 series airplanes. This AD requires doing a one-time inspection for damage of the electrical cable harness assembly located on the left and right wing root-to-fuselage aft seal, and repair if necessary; and reworking the fuselage aft seal assembly (left and right) to create a clearance between the electrical cable assemblies and the edge of the fairing panel. This AD results from a report that an airplane encountered an uncommanded propeller feathering during climb, which resulted in an emergency landing. We are issuing this AD to prevent chafing or grounding of the wiring against the aft seal assemblies, which, if not corrected, could interrupt the operation of various systems, including the propeller feather control, alternating current (AC) electrical power, and standby hydraulic power, and result in reduced controllability of the airplane.

Source

Authoritative
Federal Register document
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