Manufacturer
Airbus Helicopters
Number
EASA 18-144 (Proposed)
Model(s)
AS332, SA330, EC225
Published Date
Effective Date
Summary
Proposed AD would supersede EASA AD 2018-0042 and requires repetitive replacement of the flapping hinge components installed on tail rotor transmission assemblies, in addition to reporting requirements. Prompted by a report of damage of the flapping hinge link on one of five tail rotor blades of a helicopter. An ongoing investigation is seeking to determine the root cause of this damage.
UUID
16