What was found
FUSELAGE FRAME AT BS 188 DAMAGED AT WEB AT LBL 14-15 MOD. REPAIRED WED AT BS 188 LBL 14-15, PER SRM 51-70-13-2R-4. THIS IS A TLD REPAIR, WITHIN 30 DAYS AFTER THE AIRPLANE RETURNS TO SERVICE CONTACT THE BOEING COMPANY FOR INSPECTION THRESHOLD PERMANENT ACTON REQUIRED. WITHIN 30 DAYS AFTER THE AIRCRAFT RETURNS TO SERVICE CONTACT THE BOEING COMPANY FOR THE INSPECTION THRESHOLD THIS IS TLD, REF SRM 51-40-13-2R-4.