Manufacturer
Airbus Helicopters
Number
EASA 2023-0147
Model(s)
AS332L
Published Date
Effective Date
Summary
Lowers the life limit of main gearbox fitting pin(s) and rear attachment fitting pin and adds a modification to install shims on the rear sliding cooling rails of the main gearbox. Prompted by a determination that the installation of main gearbox upper deck fittings of the three suspension bars could lead to tightening torque loss on affected pin(s) and fitting(s).
Company Reference
Aircraft Reference