Airworthiness Directives; EXTRA Flugzeugbau GmbH Model EA-300S Airplanes
airworthiness · Rule · Final rule. · Published 2002-10-25 · Effective 2002-12-17 · 67 FR 65479
Document
Document number
02-26660
Federal Register citation
67 FR 65479
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
EXTRA Flugzeugbau GmbH Model EA-300S
Publication date
2002-10-25
Effective date
2002-12-17
FAA docket
Docket No. 99-CE-85-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain EXTRA Flugzeugbau GmbH (EXTRA) Model EA-300S airplanes. This AD requires you (for all affected airplanes) to inspect the upper longeron at the horizontal stabilizer attachment for cracks using a fluorescent dye check penetrant method, repair any cracks found, and modify the horizontal stabilizer. This AD also requires a limit on operation to the Normal category until accomplishment of the initial inspection and modification on airplanes with less than 200 hours time-in-service (TIS). This AD is the result of reports of fatigue cracks at the horizontal stabilizer attachment on the affected airplanes. The actions specified by this AD are intended to detect and correct cracks in the horizontal stabilizer attachment, which could result in structural failure of the aft fuselage with consequent loss of control of the airplane.