← FAA Federal Register actions

Airworthiness Directives; Cessna Model 680 Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2008-01-03 · Effective 2008-01-18 · 73 FR 395

Document

Document number
07-6265
Federal Register citation
73 FR 395
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Cessna Model 680
Publication date
2008-01-03
Effective date
2008-01-18
FAA docket
Docket No. FAA-2007-0379

Abstract

We are adopting a new airworthiness directive (AD) for certain Cessna Model 680 airplanes. This AD requires inspecting the routing of the aft fairing wire bundle assembly for adequate separation between the wiring and the hydraulic line; inspecting for chafing or damage of the wire bundle assembly and for damage to the hydraulic line, and doing corrective actions if necessary. This AD results from an incident report which indicated that a hydraulic leak and wire chafing, including signs of heat damage, were found within the lower tail cone fairing area. Similar wire chafing has also been found on other airplanes. We are issuing this AD to detect and correct wire chafing, and inadequate separation of the wiring and hydraulic line, which could lead to electrical arcing and a hydraulic leak and could result in a potential source of ignition and consequent fire.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown