Manufacturer
Airbus Helicopters
Number
EASA 2023-0064
Model(s)
AS350B/B1/B2/B3/BA/BB/D, AS355E/F/F1/F2/N/NP, SA365C1/C2/C3/N/N1/N2/N3 and EC130B4/T2
Published Date
Effective Date
Summary
Supersedes but retains requirements of ASA AD 2021-0048, which mandates repetitive inspections of the main rotor pitch rod upper links for proper torque, as well as making alignment markings on the pitch rod. Updated AD introduces an optional modification to install a new pitch rod lever axis attachment screw that constitutes a terminating action for the repetitive inspections.
UUID
475