FAA 2024-16-01

Effective 2024-09-04 · Applies to: Bell 412
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Subject

Repetitive inspections of tail-boom upper LH cap angle for fatigue cracks; reduces interval to 25–50 flight hours.

Compliance time

Repetitive 25 or 50 FH (model-dependent)

Referenced Service Bulletins

  • Bell ASB 212-24-169
  • Bell ASB 412-24-197
  • Bell ASB 412CF-24-77
Source: FAA · scraped 2026-05-06 23:01 UTC