What was found
R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED R/H ENGINE INLET COWL ASSEMBLY IN REF TO AMM TASK 71-11-01-004-002-H00
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED R/H ENGINE INLET COWL ASSEMBLY IN REF TO AMM TASK 71-11-01-004-002-H00