Airworthiness Directive

AD 98-05-11 63 FR 11108 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-5347
Amendment
39-10372
Published
1998-03-06
Effective
1998-03-23
Models covered
1
Last live check
2026-10-01
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AD

98-05-11

FR doc 98-5347 · 63 FR 11108

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

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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.

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All Canadair CL-215 / CL-415 directives

Applies to 1 model in our index