Airworthiness Directives; Eurocopter France Model EC 155B, SA-365N and N1, AS-365N2, and AS 365 N3 Helicopters
airworthiness · Rule · Final rule. · Published 2003-09-08 · Effective 2003-10-14 · 68 FR 52832
Document
Document number
03-22619
Federal Register citation
68 FR 52832
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-09-08
Effective date
2003-10-14
FAA docket
Docket No. 2002-SW-53-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) model helicopters that requires inspecting the hydraulic brake hose (hose) for crazing, pinching, distortion, or leaks at the torque link hinge and replacing the hose, if necessary. This amendment also requires inspecting the hose and the emergency flotation gear pipe to ensure adequate clearance, and adjusting the landing gear leg, if necessary. This amendment is prompted by a report of a hose compression due to interference with a clamp that attaches the emergency flotation gear pipe. The actions specified by this AD are intended to prevent failure of the hose, resulting in failure of hydraulic pressure to the brakes on the affected landing gear wheel, and subsequent loss of control of the helicopter during a run-on landing.