What was found
CRACK WAS FOUND OF 0.203IN LENGTH APPROX ON THE STA 1640 FUSELAGE FRAME INNER-CHORD FWD RETURN FLANGE RADIUS, LOCATED 0.500IN BELOW THE FASTENER HOLE AT S-14L, IN REF CARD 5311-01218-01A JOB # 106-0001, STEP 7. FRAME ON STA 1640 BETWEEN STRG 9LH AND STRG 20LH WAS REPAIRED PER PRI 632412-14 REV. 0 TO 2 AND ER/A- 632412-14AD REV. ORIGINAL SECTION I : PERMANENT REPAIR. (1493045) (AIRCRAFT GROUNDED)