Airworthiness Directive

AD 99-21-09 64 FR 54199

Federal Aviation Administration · 14 CFR part 39

FR document
99-25768
Amendment
39-11352
Published
1999-10-06
Models covered
1
Last live check
2026-08-17
AD

99-21-09

FR doc 99-25768 · 64 FR 54199

AD 99-21-09Published 1999-10-06Effective 1999-11-10

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 supersedes an existing airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, - 201, -202, -301, -311, and -315 series airplanes, that currently 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 requires the accomplishment of these same actions on additional airplanes. 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