What was found
DURING C-CHECK, FUSELAGE SKIN AT BS 1089 HAS AN ELONGATED FASTENER HOLE FORWARD OF THE VERTICAL STAB ATTACH FITTINGS, NRC NR073. REPAIRED PER SRM 53-31-0 FIG 19 AND ECRA. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FUSELAGE SKIN AT BS 1089 HAS AN ELONGATED FASTENER HOLE FORWARD OF THE VERTICAL STAB ATTACH FITTINGS, NRC NR073. REPAIRED PER SRM 53-31-0 FIG 19 AND ECRA. (M)