What was found
FASTENER HOLE NR 40 ON THE LEFT SIDE OF THE 1809.5 BULKHEAD OF DRWG 624T0020 FLAG NOTE 1 IS ELONGATED AT THE FUSELAGE, THE FITTING, AND AT THE HORIZONAL STAB. COULD NOT GET AN ACCURATE HFEC SCAN. FAB'D NEW REPAIR WEB IAW ENGINE APPROVAL & BOEING DWG #148T2740, SRM 51-20-01, AMES PROC STND'S. REMOVED & REINSTALLED VERT/HORIZ STIFFNERS, COLLAR, UPPER TENSION FITTING IAW 767 SRM 51-40-02. RMVD & REPL UPPR CHORD SEC. & CHORD BULKHEAD SPLICE FITTING IAW 767 SRM 51-40-02 & S/B 53A0078, INSTALLED & REMOVED STAB JACK EQUIP IAW 767 MM 55-17-51-4. ACFT WAS GROUNDED. S/N: NSN, ATA : 53, LOC: RT SD 1809.5