Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes
airworthiness · Rule · Final rule. · Published 2003-07-18 · Effective 2003-08-22 · 68 FR 42581
Document
Document number
03-18083
Federal Register citation
68 FR 42581
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-07-18
Effective date
2003-08-22
FAA docket
Docket No. 2001-NM-391-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, - 202, -301, -311, and -315 airplanes. This AD requires modification of the No. 3 electrical equipment panel behind the avionics rack, and modification of the No. 2 propeller de-ice timer. This action is necessary to prevent incorrect altitude information transmitted by the Mode S transponder and simultaneous loss of the Traffic Alert and Collision Avoidance System (TCAS), and increasing the possibility of an air traffic conflict. This action is intended to address the identified unsafe condition.