What was found
NR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03.