What was found
CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-2 CHECK, FOUND .5 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 400, BETWEEN STRINGER 8, STRINGER 9L. INSTALLED DOUBLER PER SRM 53-00-07. (M)