Airworthiness Directive

AD 98-20-14 63 FR 50501

Federal Aviation Administration · 14 CFR part 39

FR document
98-25119
Amendment
39-10781
Published
1998-09-22
Models covered
1
Last live check
2026-08-17
AD

98-20-14

FR doc 98-25119 · 63 FR 50501

AD 98-20-14Published 1998-09-22Effective 1998-10-27

Requires a one-time inspection to detect chafing of electrical wires in the cable trough below the cabin floor; repair, if necessary; installation of additional tie-mounts and tie-wraps; and application of sealant to rivet heads.

Full official 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 series airplanes, that requires a one-time inspection to detect chafing of electrical wires in the cable trough below the cabin floor; repair, if necessary; installation of additional tie-mounts and tie-wraps; and application of sealant to rivet heads. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent chafing of electrical wires, which could result in an uncommanded shutdown of an engine during flight.

Applies to 1 model in our index