What was found
PUNCTURE IN THE LEFT HORIZONTAL STAB UPPER SURFACE 20 INCHES AFT OF LEADING EDGE AND 24 INCHES FROM INBD EDGE AT FUSELAGE. INSTALLED A REPAIR IAW SRM 55-10-01, REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PUNCTURE IN THE LEFT HORIZONTAL STAB UPPER SURFACE 20 INCHES AFT OF LEADING EDGE AND 24 INCHES FROM INBD EDGE AT FUSELAGE. INSTALLED A REPAIR IAW SRM 55-10-01, REPAIR 2.