Manufacturer
Airbus Helicopters
Number
FAA 2020-15-13
Model(s)
BK117C-2 and BK117D-2
Published Date
Effective Date
Summary
Retains the initial inspection and torque requirements of AD 2017-02-07 and requires replacing the hydraulic module plate assembly attachment point hardware. Prompted by a terminating action that has been developed to address the unsafe condition.
UUID
341