Manufacturer
Airbus Helicopters
Number
EASA 2023-0127
Model(s)
AS350B/B1/B2/B3/BA/BB/D and EC130B4/T2
Published Date
Effective Date
Summary
Requires inspections for inverted installations of the engine flange on the main gearbox engine coupling and, if found, performing necessary corrective actions. Prompted by reports of such inverted installations found on the final assembly line. If not detected and corrected, this condition may lead to loss of power transmission to the main gearbox and main rotor.
UUID
583958405