What was found
DURING C4/A4 CHECK OF SUBJECT ACFT, FOUND CRACK DAMAGE ON FUSELAGE FRAME AT BS 800, S-7R TO S-8R AND AT BS 820, S-8L. AN INTERIM REPAIR WAS ACCOMPLISHED ON FRAME IAW SRM 53-10-04, FIGURE 54 AND NRC 506164..
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C4/A4 CHECK OF SUBJECT ACFT, FOUND CRACK DAMAGE ON FUSELAGE FRAME AT BS 800, S-7R TO S-8R AND AT BS 820, S-8L. AN INTERIM REPAIR WAS ACCOMPLISHED ON FRAME IAW SRM 53-10-04, FIGURE 54 AND NRC 506164..