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FAA Proposes New AD On Piper Wing Spars

The April 4, 2018, crash of a Piper PA-28R-201 Arrow V operated by Embry-Riddle Aeronautical University (ERAU) continues to have repercussions. Most recently, the FAA has published a proposed airworthiness directive (AD) that would require inspecting each main wing spar of a wide range of Piper airplanes. The proposed AD is a response to the ERAU crash, which involved the inflight separation of the Piper Arrows left wing. Both aboard died and the airplane was destroyed.

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Key Takeaways:

  • The FAA has proposed an Airworthiness Directive (AD) for numerous Piper PA-28 and PA-32 models, requiring main wing spar inspections for fatigue cracks based on "factored service hours" following a fatal crash caused by in-flight wing separation.
  • Separately, the FAA issued a Safety Alert for Operators (SAFO) providing guidance on identifying and manipulating trim and autopilot circuit breakers during abnormal or emergency situations to prevent accidents caused by system failures.
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The April 4, 2018, crash of a Piper PA-28R-201 Arrow V operated by Embry-Riddle Aeronautical University (ERAU) continues to have repercussions. Most recently, the FAA has published a proposed airworthiness directive (AD) that would require inspecting each main wing spar of a wide range of Piper airplanes. The proposed AD is a response to the ERAU crash, which involved the inflight separation of the Piper Arrow’s left wing. Both aboard died and the airplane was destroyed.

During its investigation, the NTSB found “more than 80 percent of the lower spar cap and portions of the forward and aft spar web doublers exhibited fracture features consistent with metal fatigue. The fatigue features originated at or near the outboard forward wing spar attachment bolt hole.” The NTSB’s investigation included examining a second Piper Arrow, one that “had a similar number of total airframe hours and cycles and was used exclusively for flight training of students.” That examination revealed a crack at the left lower outboard forward wing spar attachment bolt hole similar to the accident airplane.

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