Airworthiness Directives; Bombardier Model DHC-8-100, -200, and -300 Series Airplanes
airworthiness · Rule · Final rule. · Published 2001-11-30 · Effective 2002-01-04 · 66 FR 59690
Document
Document number
01-29343
Federal Register citation
66 FR 59690
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2001-11-30
Effective date
2002-01-04
FAA docket
Docket No. 2001-NM-129-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100, -200, and -300 series airplanes, that requires installation of a backup pressure regulating valve on the oil pump of the propeller control unit (PCU) on both engines. The actions specified by this AD are intended to prevent a build-up of oil pressure in the oil pump of the PCU should the existing valve fail. Such failure of the pressure regulating valve could lead to oil leaks, fracture of the pump, inability to maintain engine oil pressure, and inability to feather the propeller, with consequent reduced controllability of the aircraft. This action is intended to address the identified unsafe condition.