What was found
CRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 24, REV A. MEASUREMENT OF CRACK IS L= 0.813".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 24, REV A. MEASUREMENT OF CRACK IS L= 0.813".