Airworthiness Directives; Bombardier Model CL-215-6B11 (CL-215T) Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1998-03-06 · Effective 1998-03-23 · 63 FR 11108
Document
Document number
98-5347
Federal Register citation
63 FR 11108
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Bombardier Model CL-215-6B11 (CL-215T) Series
Publication date
1998-03-06
Effective date
1998-03-23
FAA docket
Docket No. 97-NM-328-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Bombardier Model CL-215-6B11 (CL-215T) series airplanes. This action requires either replacement of the switching valve-to-rear inlet case sealing air tube assembly with a tube assembly that includes an integral fire detector (intercompressor case [ICC] fire detector loop), and modification of the nacelle fire detection system; or modification of the No. 5 bearing air system. This amendment is prompted by the issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect internal engine fire within the ICC; or to prevent air/oil from leaking into the ICC, which could result in such fire.