What was found
MAJOR: CORROSION_CENTER FUSELAGE III DRY AREA 53-23 R.HAND SIDE OF FR.84 CROSSBEAM. BLENDED CORROSION CENTER FUSELAGE FR.84 CROSSBEAM, NOMINAL THICKNESS .080" MATERIAL LOSS.040", FOUND TO BE OUT OF LIMITS REF SRM 51-10-03, 51-75-16.REMOVED AND REPLACED. R.HAND SIDE CROSS BEAM CUTOUT FR.84 REF EMB SRM 51-23-06, 51-23-04. SEE EAMS W/O H6997 SN 213 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK BNA.