What was found
DURING INSPECTION, FOUND LOWER FUSELAGE SKIN TO BE CORRODED AT FRAME 22 BETWEEN STRINGERS 20 LT AND 20 RT, CUT OUT CORRODED AREA OF LOWER FUSELAGE SKIN FABRICATED AND INSTALLED A SERVICEABLE FILLER AND DOUBLER REPAIR. ALL WORK WAS DONE I/A/W EMB 120 S.B. 120-53-0065, S.R.M. 53-00-01, FIG. 202. AIRCRAFT TOTAL CYCLES, 20,085.