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AD FAA-2013-0487

Airworthiness Directives; Eurocopter France Helicopters

Summary

We are adopting a new airworthiness directive (AD) for Eurocopter France (Eurocopter) Model AS332L2 and EC225LP helicopters. This AD requires inspecting the torque value of the bolts that secure the front and rear main gearbox (MGB) suspension bar attaching fittings, and re-torqueing the bolts to the proper value if the torque value is out of tolerance. This AD also requires, if the torque value is out of tolerance by more than 20 percent, inspecting the bolts, frames, and related equipment for a crack and repairing or replacing them if cracked. This AD was prompted by reports of cracks on Frame 5295 of Model AS332L2 helicopters. The actions of this AD are intended to detect the torque loss of the bolts that secure the MGB bar attaching fittings and to prevent cracks that could lead to failure of the MGB supporting structure, detachment of the MGB, and loss of helicopter control.

Directive Details

AD Number

FAA-2013-0487

Document Number

2013-27638

Type

Rule

Publication Date

November 25, 2013

Effective Date

December 30, 2013

Affected Manufacturer

Eurocopter France

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2013-0487

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Eurocopter France →

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