Airworthiness Directives; GROB-WERKE Model G120A Airplanes
airworthiness · Rule · Final rule. · Published 2004-11-04 · Effective 2004-12-27 · 69 FR 64251
Document
Document number
04-24522
Federal Register citation
69 FR 64251
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
GROB-WERKE Model G120A
Publication date
2004-11-04
Effective date
2004-12-27
FAA docket
Docket No. FAA-2004-18030
Abstract
The FAA adopts a new airworthiness directive (AD) for all GROB-WERKE (GROB) Model G120A airplanes. This AD requires you to repetitively inspect visually the area between the vertical stabilizer main spar and the nearby vertical stabilizer skin for any disbonding/ crack; repair any disbonding/crack found; and calculate weight and balance after any repair. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct any disbonding/crack in the area between the vertical stabilizer main spar and nearby stabilizer skin, which could result in possible structural failure. This failure could lead to difficulty in airplane flight control.