What was found
FUSELAGE FRAME AT BS 196.5 DAMAGED AT WEB AT LBL 14-15 MOD. REPAIRED WEB AT 196.5 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 REPAIR REQIRED. WITHIN 30 DAYS AFTER THE AIRPLANE RETURNS TO SERVICE. CONTACT THE BOEING COMPANY FOR THE INSPECTION THRESHOLD THIS IS TLD, REF SRM 51-0-13-2R-4.