What was found
INBD COWL PANEL 414AR HAS A CRACKED STIFFENER AT BS 273.5. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-05, STEP 4.E AND SRM 51-42-05, PG.204-205, PROCEDURE D, STEPS 1-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INBD COWL PANEL 414AR HAS A CRACKED STIFFENER AT BS 273.5. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-42-05, STEP 4.E AND SRM 51-42-05, PG.204-205, PROCEDURE D, STEPS 1-10.