What was found
SKIN CRACKED ON THE TOP OF THE FUSELAGE AT BS 1152 ON THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN CRACK IAW ER/A 555585-14, AND PRI 555585-14, REV 0 AND 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN CRACKED ON THE TOP OF THE FUSELAGE AT BS 1152 ON THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN CRACK IAW ER/A 555585-14, AND PRI 555585-14, REV 0 AND 1.