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Airworthiness Directives; Airbus Helicopters (Type Certificate Previously Held by Eurocopter France)

airworthiness · Rule · Final rule. · Published 2015-05-05 · Effective 2015-06-09 · 80 FR 25589

Document

Document number
2015-09548
Federal Register citation
80 FR 25589
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2015-05-05
Effective date
2015-06-09
FAA docket
Docket No. FAA-2014-0038

Abstract

We are adopting a new airworthiness directive (AD) for Airbus Model EC225LP helicopters. This AD requires repetitive visual and tap test inspections of each main rotor blade (blade) leading edge stainless steel protective strip (strip) for a crack, cut, or blind or open debonding (debonding), and taking approved corrective measures. If there is a crack or if there is debonding that exceeds acceptable limits, this AD requires, before further flight, repairing or replacing the blade with an airworthy part. This AD was prompted by suspected water seepage through a crack in the blade strip resulting in significant debonding. The actions of this AD are intended to prevent loss of the blade strip, excessive vibrations induced by blade weight imbalance, and subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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