Airworthiness Directive

AD 98-20-14 63 FR 50501 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-25119
Amendment
39-10781
Published
1998-09-22
Effective
1998-10-27
Models covered
1
Last live check
2026-10-03
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AD

98-20-14

FR doc 98-25119 · 63 FR 50501

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

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 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.

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Applies to 1 model in our index