airworthiness · Rule · Final rule; request for comments. · Published 2002-09-18 · Effective 2002-10-03 · 67 FR 58686
Document
Document number
02-23652
Federal Register citation
67 FR 58686
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2002-09-18
Effective date
2002-10-03
FAA docket
Docket No. 2001-NE-42-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to Turbomeca S.A. Makila Models 1A, 1A1, and 1A2 turboshaft engines with exhaust pipes incorporating modification TU 200A installed. This action requires visual inspections of exhaust pipes for cracks and tears, upon completion of the last flight of each day, and replacement of cracked and torn exhaust pipes before further flight. This action also requires removal from service of modification TU 200A exhaust pipes at the next shop visit or no later than a certain date. This amendment is prompted by several reports of modification TU 200A exhaust pipes cracking at several of the ejector attachment tabs. The actions specified in this AD are intended to prevent the ejector from becoming loose from the exhaust pipe, resulting in damage to the main rotor and tail rotor and loss of helicopter control.