What was found
CRACKS IN SEVERAL HOLES ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 LT, (HOLE G ,I ,L , M, A3, A4 ,A5 ,A6 , A7, A8). REPAIR PERFORMED BY REAM UP THE HOLES UNTIL CRACK REMOVAL IAW EA 6-5315-106504 AND RAS/053351/014/2007 ISS A.