NTSB Cites Fatigue Cracking In Fatal ERAU Crash

Image: NTSB
Gemini Sparkle

Key Takeaways:

  • The NTSB determined that the 2018 Embry-Riddle Piper PA-28 crash, which killed two people, was caused by extensive fatigue cracking in the left-wing main spar, leading to in-flight wing separation.
  • The cracking was attributed to severe loads from flight training maneuvers, low-altitude operations, and frequent landings, causing faster accumulation of damaging stress cycles than expected for training aircraft.
  • A similar fatigue crack was found in another aircraft from the school's fleet, and the cracks were not visible through standard inspections.
  • The FAA proposed mandatory wing spar inspections for thousands of Piper PA-28 series aircraft in response to the issue, though an Airworthiness Directive has not yet been finalized.
See a mistake? Contact us.

The NTSB found that the crash of an Embry-Riddle Aeronautical University Piper PA-28R-201 that killed two people in April 2018 was caused by extensive fatigue cracking in the left-wing main spar, according to the final report (PDF) issued by the board on Tuesday. As previously reported by AVweb, the left wing separated from the aircraft shortly after a touch-and-go at Florida’s Daytona Beach International Airport (DAB). A second ERAU Piper was found to have a similar fatigue crack in its left-wing main spar when the school’s fleet was examined after the accident. The board noted that no anomalies in materials or construction of the wing spars were found on either aircraft.

“The NTSB concludes that, due to flight training maneuvers, significant operation at low altitudes, and frequent landing cycles, the accident airplane (and its sister airplane in the operator’s fleet) likely experienced landing, gust, and maneuver loads that were more severe than expected for training aircraft,” the NTSB said in its summary (PDF) of the report. “Therefore, the low-altitude flight training and frequent landing environment likely resulted in the accident airplane accumulating damaging stress cycles at a faster rate than a personal use airplane.”

The NTSB reported that the accident aircraft had accumulated 7,690.6 hours and 33,276 landing cycles prior to the crash, averaging 4.33 landings per hour of flight time. The board also found reports of reported flap extension overspeed, gear extension overspeed and hard landing events in the aircraft’s logs, but noted that airframe inspections had been performed after each event with no defects noted.

The NTSB further established that, due to its location, the fatigue cracking would not have been visible from either the interior or exterior of the airplane. In response to the potential for such cracking to go unnoticed, the FAA issued a notice of proposed rulemaking (NPRM) eight months after the accident which suggested required wing spar inspections for nearly 20,000 Piper PA-28 series aircraft. The NTSB said it had “expressed … support of the proposed AD’s inspection requirements but urged the FAA to reexamine the proposed AD’s applicability to certain airplanes based on airplane usage.” Comments closed on the NPRM in February 2019, but an AD has not yet been issued.

Kate O'Connor

Kate is a private pilot, certificated aircraft dispatcher, and graduate of Embry-Riddle Aeronautical University.
Sign-up for newsletters & special offers!

Get the latest stories & special offers delivered directly to your inbox

SUBSCRIBE

Please support AVweb.

It looks like you’re using an ad blocker. Ads keep AVweb free and fund our reporting.
Please whitelist AVweb or continue with ads enabled.