What was found
FUSELAGE FRAME AT BS 360 INSULATION STAND OFF HOLE BETWEEN STRINGERS 19 AND 20R SHOWS CRACK INDICATION IAW T/C AD20152308-400-53-11. ACFT GROUNDED. REPAIRED THE DAMAGE IAW EA 400-53EA-17811.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT BS 360 INSULATION STAND OFF HOLE BETWEEN STRINGERS 19 AND 20R SHOWS CRACK INDICATION IAW T/C AD20152308-400-53-11. ACFT GROUNDED. REPAIRED THE DAMAGE IAW EA 400-53EA-17811.