What was found
DURING H-CHECK FOUND CRACK IN RT MAIN WHEEL WELL SUPPORT AFT ATTACH ANGLE FOR SUPPORT STRUT CRACKED AT BS 832 L20. REPAIRED IAW SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING H-CHECK FOUND CRACK IN RT MAIN WHEEL WELL SUPPORT AFT ATTACH ANGLE FOR SUPPORT STRUT CRACKED AT BS 832 L20. REPAIRED IAW SRM 51-30-5.