What was found
*SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLET COWL REF 767 M/M CHAP 71-11-01-404-005-H00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
*SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLET COWL REF 767 M/M CHAP 71-11-01-404-005-H00.