What was found
During "C" Check Inspection.-Control Cabin, Fwd Pressure Bulkhead BS178, R-H Side Chord Cracked Between WL 207 & 210.-Preventive Modification accomplished at Fwd Pressure Bulkhead BS178, R-H Chord, Between WL184 & 230 due to Crack IAW Boeing S/B 737-53A1173, REV3, Section III Part XI Paragraph I Fig 71.Note: See COOPESA Work Order No. O10863 2-37, VAM100 No. 213 & 122SDA094.