Landing Gear — Skid-Type Landing Gear — Inspection
- Published
- Effective
- Deadline
AI-generated summary of the official EASA document. Verify against the PDF before acting.
What to do
Operators of EC 120 B and EC 130 T2 and B4 helicopters must inspect the landing gear assemblies within the compliance times specified in the directive, based on the date of first installation and operation type. If corrosion or cracks are found, they must follow Airbus Helicopters approved repair instructions or replace affected parts before further flight. Inspection results must be reported to Airbus Helicopters within 30 days of inspection or the directive's effective date.
Summary
EASA Airworthiness Directive 2022-0053 is an airworthiness directive addressing the inspection of skid-type landing gear assemblies on Airbus Helicopters EC 120 B and EC 130 T2 and B4 models. It mandates a one-time external and internal inspection for corrosion and cracks on specified landing gear part numbers. The directive applies to all serial numbers of the affected helicopter models and includes detailed definitions of affected parts and sub-assemblies.
What changed
EASA Airworthiness Directive 2022-0053 introduces mandatory inspections for corrosion and cracks on certain landing gear assemblies of EC 120 B and EC 130 helicopters. It requires operators to perform visual and borescope inspections within specified compliance times based on installation dates and operation types. The directive also outlines corrective actions, including repair or replacement of affected parts, and reporting requirements to Airbus Helicopters.
Why it matters
This directive is critical for aviation professionals to prevent potential landing gear collapse caused by corrosion, which could lead to helicopter damage or occupant injury. Operators and maintenance organizations must ensure compliance to maintain airworthiness and safety. The directive also impacts maintenance planning and parts management by defining serviceable parts and inspection criteria.
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