Airworthiness Directives; EXTRA Flugzeugbau GmbH Models EA-300, EA-300S, and EA-300L Airplanes
airworthiness · Rule · Final rule. · Published 1998-11-23 · Effective 1998-12-28 · 63 FR 64603
Document
Document number
98-31013
Federal Register citation
63 FR 64603
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-11-23
Effective date
1998-12-28
FAA docket
Docket No. 98-CE-53-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain EXTRA Flugzeugbau GmbH (EXTRA) Models EA-300, EA- 300S, and EA-300L airplanes. This AD requires repetitively inspecting the rudder pedal for proper alignment, the safety control stop for wear and proper clearance, the rudder cables for elongation, and the rudder pedal footrest for cracks. This AD also requires correcting or replacing any discrepant part, as applicable. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified by this AD are intended to prevent failure of the rudder pedal footrest caused by overloading the rudder pedal safety control stop, which could result in loss of directional control of the airplane.