What was found
CRACKS ON CIRCUMFERENTIAL SPLICE STRAP BS 930, STRINGER 14R. INSTALLED FUSELAGE FRAME REPAIR AT BS 930, STRINGER 14R. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0162. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKS ON CIRCUMFERENTIAL SPLICE STRAP BS 930, STRINGER 14R. INSTALLED FUSELAGE FRAME REPAIR AT BS 930, STRINGER 14R. MATERIAL USED, 7075-T6, .125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0162. (M)