Summary
The FAA is adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. Arriel 2C, 2C1, 2S1, and 2S2 model turboshaft engines. This AD was prompted by investigations by the manufacturer following level 1 failures in flight (minor anomalies) and level 2 failures on the ground (minor failures), where cracks were found on the soldered joints of torque conformation boxes. This AD requires performing initial and repetitive inspections of the resistance values of the torque conformation box and, depending on the results of the inspections, replacement of the torque conformation box. The FAA is issuing this AD to address the unsafe condition on these products.
Directive Details
AD Number
FAA-2020-1118
Document Number
2021-05046
Type
Rule
Publication Date
March 11, 2021
Effective Date
April 15, 2021
Affected Manufacturer
Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Turboshaft
Criticality
important
Emergency
No
Docket ID
Docket No. FAA-2020-1118
Topics
Official Documents
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