What was found
DURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING. CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN. INSTALLED DOUBLER PER ACO 6135-54.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED QUARTER D-CHECK, FOUND NUMBER 2 ENGINE STRUT INNER SKIN CRACKED AT O/B EDGE OF PANEL 5827R OPENING. CRACK RUNS BEYOND STOP DRILL AND UNDER CROWN SKIN. INSTALLED DOUBLER PER ACO 6135-54.