What was found
HKG - DURING 'C5/D' CHECK INSPECTION, FUSELAGE BS 340-400 STRINGER GL LAP SPLICE TOP ROW FASTENER HOLES, FOUND 27 HOLES CRACKED. REPAIRED SKIN LAP IAW SRM 53-30-03 FIG 26. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
HKG - DURING 'C5/D' CHECK INSPECTION, FUSELAGE BS 340-400 STRINGER GL LAP SPLICE TOP ROW FASTENER HOLES, FOUND 27 HOLES CRACKED. REPAIRED SKIN LAP IAW SRM 53-30-03 FIG 26. (M)