The forward outboard, lower wing spar caps were found cracked. The cracks-on both left and righthand assemblies-radiated out from the fourth Huck rivet forward, passing through the wing attach hinge. This aircraft was inspected 15 months /404.2 hours ago by eddy current. No cracks were found at that time. Wing lower spar cap part numbers: l/h: 000-110012-1; r/h: 000-110012-2.
Streams coursing across the New Jersey wetlands.Jonathan Milne/Courtesy Lighthawk
Key Takeaways:
Critical structural cracks were discovered in aircraft components (Beechcraft King Air wing spar caps, Piper Seminole nose cone spar), with some appearing shortly after previous inspections or not covered by existing directives.
Unexpected component failures occurred, including recently manufactured Cessna 172R tire tubes failing due to "weather checking" and a loose turbocharger oil line on a Cirrus SR22.
Persistent safety issues with Cessna turbocharged piston twin exhaust systems highlight a lack of proper compliance with mandatory inspections, underscoring the vital importance of diligent maintenance for flight safety.
The forward outboard, lower wing spar caps were found cracked. The cracks-on both left and righthand assemblies-radiated out from the fourth Huck rivet forward, passing through the wing attach hinge. This aircraft was inspected 15
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