What was found
DURING HEAVY CHECK, STRINGER 1A LT IS CRACKED AT FRAME 20. INSTALLED STRINGER SPLICE IAW SRM REV 86 53-00-00, FIG 426.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY CHECK, STRINGER 1A LT IS CRACKED AT FRAME 20. INSTALLED STRINGER SPLICE IAW SRM REV 86 53-00-00, FIG 426.