FAA 2024-04-10

Effective 2024-03-19 · Applies to: Airbus EC135
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Subject

Tail rotor blade crack from intergranular corrosion; repetitive FPI/eddy-current inspections required, remove cracked blades before further flight.

Compliance time

Before further flight if cracked; repetitive otherwise

Referenced Service Bulletins

  • AH EASB EC135-64-11-0001 Issue 001 (2024-01-25)
Source: FAA · scraped 2026-05-06 23:01 UTC