What was found
NR 2 ENGINE EXHAUST CONE HAS A 2-3 INCH CRACK AT THE SIX O'CLOCK POSITION. SUPPLEMENTAL DATA UPDATE, CRACK RUNS ALONG SEAM OF WELD REPAIR AT 6 0'CLOCK POS APPROX 5 INCHES LONG. ACCOMPLISHED REPAIR BY STOP DRILLING PER MM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 2 ENGINE EXHAUST CONE HAS A 2-3 INCH CRACK AT THE SIX O'CLOCK POSITION. SUPPLEMENTAL DATA UPDATE, CRACK RUNS ALONG SEAM OF WELD REPAIR AT 6 0'CLOCK POS APPROX 5 INCHES LONG. ACCOMPLISHED REPAIR BY STOP DRILLING PER MM.