Airworthiness Directive

AD 2005-22-14 70 FR 66747

Federal Aviation Administration · 14 CFR part 39

FR document
05-21800
Amendment
39-14358
Published
2005-11-03
Models covered
1
Last live check
2026-08-17
AD

2005-22-14

FR doc 05-21800 · 70 FR 66747

AD 2005-22-14Published 2005-11-03Effective 2005-12-19

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…

Full official 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.

Applies to 1 model in our index