What was found
DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALE D THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633308-14AD, ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 29,500 FC FROM SECTION I (21MAY26). REPEAT SECTION II INSPECTION WITHIN EVERY 8,700 FC AFTER INITIAL INSPECTION. ASSOCIATED ER/A 32-633308 ADDED FOR AC 3241. (LP: 1616599, AIRCRAFT WAS GROUNDED)