What was found
CRACK SUPPORT ANGLE, REAR SPAR, IRSS 140 UPPER POSITION, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, 51-10-02-0G-0, STEP 9, AND DWG-115A2000, SHEET 22, REV A. MEASUREMENT OF CRACK: 1.147 INCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK SUPPORT ANGLE, REAR SPAR, IRSS 140 UPPER POSITION, RT WING. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, 51-10-02-0G-0, STEP 9, AND DWG-115A2000, SHEET 22, REV A. MEASUREMENT OF CRACK: 1.147 INCH.