What was found
DURING TOWING OF THE AIRCRAFT INTO THE HANGAR 8.2, TAIL LH SIDE OF FUSELAGE STA 1768.80 TO STA 1787.45 STRINGER 20L MADE CONTACT WITH THE TAIL STAND. ACCMPLISHED REPAIR IAW EA 757-5380-16-A3665 SECTION 48 - FUSELAGE STA 1768 TO STA 1787.5 S-19L TO S-20L LAP SPLICE - DENT AND GOUGE AND FED EX EA F-5330- T0380366: FUSELAGE - PLATES AND SKIN - TAIL SKIN AT STA 1768.8 AND S19L / 20L DAMAGE WHILE TOWING INTO HANGAR. MAJOR REPAIR