airworthiness · Rule · Final rule. · Published 2004-05-21 · Effective 2004-06-25 · 69 FR 29210
Document
Document number
04-11406
Federal Register citation
69 FR 29210
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Lycoming
Publication date
2004-05-21
Effective date
2004-06-25
FAA docket
Docket No. 89-ANE-10-AD
Abstract
The FAA is adopting a new airworthiness directive (AD) that supersedes an existing AD, for Lycoming Engines (formerly Textron Lycoming), direct-drive reciprocating engines (except O-145, O-320H, O- 360E, LO-360E, LTO-360E, O-435, and TIO-541 series engines). That AD currently requires inspection of the crankshaft gear installation and rework or replacement of the gears where necessary after a propeller strike, sudden stoppage, at overhaul, or whenever gear train repair is required. This AD requires the same actions but makes the correction that the existing gear retaining bolt and lockplate be removed from service and new hardware installed, and revises the definitions for sudden stoppage and propeller strike. This AD results from a change to the definition of a propeller strike or sudden stoppage. We are issuing this AD to prevent loosening or failure of the crankshaft gear retaining bolt, which may cause sudden engine failure.