What was found
FUSELAGE CENTER BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BEYOND LIMITS. PERFORMED A CUTOUT OF THE DAMAGE AREA, FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB, SRM 53-00-10 REV 34. RETURNED AIRCRAFT TO SERVICE. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE CENTER BEAM AT FRAME 25 WAS FOUND TO BE CORRODED BEYOND LIMITS. PERFORMED A CUTOUT OF THE DAMAGE AREA, FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB, SRM 53-00-10 REV 34. RETURNED AIRCRAFT TO SERVICE. (M)