What was found
DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION III PART I PARA C. (M)