What was found
DURING INSPECTION, C-CHECK, FOUND CRACK AT FUSELAGE SKIN AT STA 1654 STRINGER 3- 4 -LT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-007, SRM 538001 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, C-CHECK, FOUND CRACK AT FUSELAGE SKIN AT STA 1654 STRINGER 3- 4 -LT. DAMAGE WILL BE REPAIRED IAW EWO 767 53-007, SRM 538001 FIG 201.