Airworthiness Directives; MD Helicopters, Inc. Model 369D, 369E, 369F, and 369FF Helicopters
airworthiness · Rule · Final rule. · Published 2002-06-27 · Effective 2002-08-01 · 67 FR 43227
Document
Document number
02-16057
Federal Register citation
67 FR 43227
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
MD
Publication date
2002-06-27
Effective date
2002-08-01
FAA docket
Docket No. 2001-SW-40-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for specified MD Helicopters, Inc. (MDHI) helicopters with a tailboom modified according to Aerometals Supplemental Type Certificate (STC) SH5055NM or SH4801NM. This AD requires an inspection to identify the part number (P/N) of the bolts that attach the tail rotor gearbox to the tailboom and replacing any bolt of inadequate grip length with an airworthy bolt. This AD also requires determining the number of bolt threads protruding from each nutplate and adding an additional washer if more than four threads protrude. This amendment is prompted by the discovery that bolts of inadequate grip length were specified to attach the tail rotor gearbox to the tailboom. The actions specified by this AD are intended to prevent loss of a tail rotor gearbox due to attaching bolts of inadequate grip length and subsequent loss of control of the helicopter.