2013-12-07
FR doc 2013-14857 · 78 FR 38546AD 2013-12-07Published 2013-06-27Effective 2013-08-01
Superseded by 2022-23-02
Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.
Prompted by a stress analysis of the tailboom skin that revealed that high-stress-concentration areas are susceptible to skin cracking.
Full official abstract
We are adopting a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 407 helicopters with certain tailboom assemblies installed. This AD requires, at specified intervals, inspecting the tailboom assembly for a crack, loose rivet, or other damage. This AD was prompted by a stress analysis of the tailboom skin that revealed that high-stress-concentration areas are susceptible to skin cracking. This condition, if not detected, could result in a crack in the tailboom assembly, failure of the tailboom, and subsequent loss of control of the helicopter.
More directives for Bell 407
- AD 2026-14-07 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-07-17
- AD 2026-10-04 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-05-21
- AD 2025-13-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2025-06-23
- AD 2024-10-12 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2024-07-18
- AD 2023-17-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2023-09-06
