Airworthiness Directives; Eurocopter France Model EC 120 Helicopters
airworthiness · Rule · Final rule. · Published 2001-12-03 · Effective 2002-01-07 · 66 FR 60143
Document
Document number
01-29592
Federal Register citation
66 FR 60143
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Eurocopter France Model EC 120
Publication date
2001-12-03
Effective date
2002-01-07
FAA docket
Docket No. 2001-SW-23-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD) that applies to Eurocopter France (ECF) Model EC120B helicopters and currently requires adjusting the clearance of the cabin sliding door if necessary. This amendment requires adding an end stop to the front rail and modifying the rear stop of the middle rail to increase its adjustment range for certain cabin sliding doors. This amendment is prompted by an in-flight loss of a cabin sliding door, which had been locked in the open position. The actions specified by this AD are intended to prevent in-flight loss of a cabin sliding door, impact with the horizontal stabilizer or fenestron tail rotor, and subsequent loss of control of the helicopter.