Airworthiness Directives; Airbus Model A330-301 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1998-05-05 · Effective 1998-05-20 · 63 FR 24740
Document
Document number
98-11563
Federal Register citation
63 FR 24740
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus Model A330-301 Series
Publication date
1998-05-05
Effective date
1998-05-20
FAA docket
Docket No. 97-NM-300-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A330-301 series airplanes. This action requires a one-time visual inspection to measure clearances between the engine forward feed pipe and shroud sleeve in the engine pylon; and repetitive operational tests for fuel leakage, and replacement of the shroud sleeve with a new improved part, if necessary. This amendment is prompted by the issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to prevent fuel from leaking into the pylon primary structure and into the engine nacelle core zone, which could result in a fire in the engine.