What was found
NR 4 EXHAUST SHROUD WORN AND CRACKED AT FORWARD FLANGE, 7 O'CLOCK POSITION. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED INTERNAL DOUBLER AND EXTERNAL WEAR PLATE IAW SRM 54-30-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 4 EXHAUST SHROUD WORN AND CRACKED AT FORWARD FLANGE, 7 O'CLOCK POSITION. BLENDED DAMAGED AREA, FABRICATED AND INSTALLED INTERNAL DOUBLER AND EXTERNAL WEAR PLATE IAW SRM 54-30-03.