What was found
FUSELAGE FRAME OUTER CHORD AT BS 196.5 DAMAGED AT LBL 14-15 MOD. REPAIRED CHORD AT 196.5 LBL-14-15, PER SRM 51-70-11-2R-0. THIS IS TLD REPAIR. WITHIN 30 DAYS AFTER THE AIRPLANE RETURNS TO SERVICE CONTACT THE BOEING COMPANY FOR INSPECTION THRESHOLD, PERMANENT ACTION REQUIRED. WITHIN 30 DAYS AFTER THE AIRCRAFT RETURNS TO SERVICE CONTACT THE BOEING COMPANY FOR INSTECTION THRESHOLD, THIS IS TLD, REF SRM 51-70-11-2R-0.