As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SPIDER WEB CRACK ON AFT LEFT SIDE OF AFT (MAIN) CARRY THROUGH SPAR. CRACK WAS APPROX. 1.25 INCHES BY 1 INCH. CRACKED AREA REMOVED TO INVESTIGATE DAMAGE FURTHER, CRACK WENT THROUGH ALL LAYERS OF FIBERGLASS AND DOWN TO(BUT NOT INTO) THE FOAM. AREA OF FIBERGLASS REMOVED IS APPROX. 2 INCHES X 1.5 INCHES. LOCATED 16 INCHES FROM CENTERLINE. SEE PICTURES ATTACHED TO EMAIL SENT TO 9-AMC-SDR-PROGMGR@FAA.GOV