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Airworthiness Directives; GROB-WERKE Model G120A Airplanes

airworthiness · Rule · Final rule. · Published 2005-11-03 · Effective 2005-12-19 · 70 FR 66747

Document

Document number
05-21800
Federal Register citation
70 FR 66747
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
GROB-WERKE Model G120A
Publication date
2005-11-03
Effective date
2005-12-19
FAA docket
Docket No. FAA-2005-21998

Abstract

The FAA adopts a new airworthiness directive (AD) for all GROB-WERKE Model G120A airplanes. This AD requires you to inspect for signs of any chafing damage to the attachment cables of the switch panels below the left-hand instrument panel, any damaged switch below the switch panels of the left-hand instrument panel, any damaged (that is, sharp) edge of the support tray for the attachment cables of the switch panels below the left-hand instrument panel; correct any damage found during the inspection; and apply a layer of anti-rub (protective padding) strips to the edge of the support tray. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect, correct, and prevent chafing of the cables against the rear lip of the tray that holds the switch panels. Chafing of the electrical cables could result in smoke or fire in the cockpit.

Source

Authoritative
Federal Register document
Machine
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