What was found
DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633637-14AD, ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 27,000 FC FROM SECTION I (21MAY26). REPEAT SECTION II INSPECTION WITHIN EVERY 4,700 FC AFTER INITIAL INSPECTION. ASSOCIATED ER/A 32-633637 ADDED FOR AC 3241. (LP: 1616702, AIRCRAFT WAS GROUNDED)