What was found
CRACKS (.75 AND .3125) AT RT SPAR DOUBLER AND WEB VERTICAL FITTING AT TRAP PANEL. REMOVED AND INSTALLED FITTING AFTER CRACK REWORK IN ACCORDANCE WITH EA 5761-01003 AND DOUGLAS DRAWING NR 5935248.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS (.75 AND .3125) AT RT SPAR DOUBLER AND WEB VERTICAL FITTING AT TRAP PANEL. REMOVED AND INSTALLED FITTING AFTER CRACK REWORK IN ACCORDANCE WITH EA 5761-01003 AND DOUGLAS DRAWING NR 5935248.