What was found
PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53-11-04. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PHX - DURING SCHEDULED C13 INSPECTION, FOUND CRACK IN FUSELAGE FRAME AT BS 360 BETWEEN STRINGER 20L AND STRINGER 21L. STOP DRILLED CRACK AND REPAIRED PER EO 53-11-04. (M)