Airworthiness Directive

AD 98-05-11 63 FR 11108

Federal Aviation Administration · 14 CFR part 39

FR document
98-5347
Amendment
39-10372
Published
1998-03-06
Models covered
1
Last live check
2026-08-17
AD

98-05-11

FR doc 98-5347 · 63 FR 11108

AD 98-05-11Published 1998-03-06Effective 1998-03-23

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…

Full official 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.

Applies to 1 model in our index