What was found
WHILE WORKING 7-5310-7-3367B PT 1, DISCOVERED A CRACK IN THE FWD PRESSURE PAN STIFFENER AT BS 740 WL 208 LT. ALSO, FOUND FWD PRESSURE PAN DAMAGED, FABRICATED NEW STIFFENER AND RIVETED TOGETHER NEW PAN. ALL WORK ACCOMPLISHED PER FEDEX SRM 51-20-1 AND BOEING DRAWING NR 65-38294.