What was found
CLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 500A, BETWEEN STRINGER 87 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-2 CHECK, FOUND .125 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE AT BS 500A, BETWEEN STRINGER 87 AND STRINGER 9R. INSTALLED DOUBLER PER SRM 53-00-07 AND EA 64536. (M)