What was found
(2) LONGITUDINAL CRACKS AT SPAR HINGE FITTING. SHAKING AND EXPANDING OF WOOD FIBERS DUE TO MOISTURE OR LACK OF. RECOMMEND USING ALUMINUM SPARS OF SUFFICIENT SIZE AND STRENGTH. (K)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(2) LONGITUDINAL CRACKS AT SPAR HINGE FITTING. SHAKING AND EXPANDING OF WOOD FIBERS DUE TO MOISTURE OR LACK OF. RECOMMEND USING ALUMINUM SPARS OF SUFFICIENT SIZE AND STRENGTH. (K)