What was found
RT WING FRONT SPAR TERMINAL FITTING CRACKED IN BOTTLE PIN HOLE (APPROX 3 IN CRACK) VERIFIED BY HFEC. REMOVED LEADING EDGE PER SRM 51-30-2. REMOVED WIRING AS PER M/M 27-82-00. REMOVED FUEL LINE S PER M/M 28-22-0. PLACED A/C IN JIG POSITION PER SRM 51-50-1 AND BOEING TELEX DHL-MIA-97-0001RR. REMOVED BOTTLE PIN PER M/M 57-41-1. CUT AND REMOVED FWD SPAR WEB PER BOEING DWG 65C36584. PERFORMED HFEC INSP OF FASTENER HOLES AND SURFACES PER NDT M/M 6-51-00-00, NO CRACK MIGRATION FOUND. COLD WORKED AT HORZ FLANGE PER SRM 51-30-10. TORQUED ALL BOLT UPPER AND LOWER PER SRM 51-30-4. INSTALLED SPLICE REPAIR ON RT WING LOWER SPAR CHORD PER BOEING DWG 65C36584. ALODINED AND PRIMED ALL PARTS PER SRM 51-10-2.