What was found
CRACKS FOUND ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 RT IN SEVERAL HOLES (B, D, K, M, A3). REPAIR PEROFRMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5315-106505 AND RAS/053356/009/2007 ISS A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS FOUND ON FUSELAGE CENTER SECTION, C47 SPLICE FITTING, P24-26 RT IN SEVERAL HOLES (B, D, K, M, A3). REPAIR PEROFRMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5315-106505 AND RAS/053356/009/2007 ISS A.