What was found
CRACK ON ANGLE LOCATED BS 867, STRINGER 26L, WL 156.1. REPLACED THE ANGLE IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A. MEASURE OF CRACK: 0.833 INCHES.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE LOCATED BS 867, STRINGER 26L, WL 156.1. REPLACED THE ANGLE IAW SRM 51-10-02-0G, SRM 51-40-02-0G-0, AND DWG 149A8102, SHEET 19, REV A. MEASURE OF CRACK: 0.833 INCHES.