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
Official Documents
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