What was found
CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING BS 763 BETWEEN LONG 27R-28R IN REF 663, ZONE 50. REF 334 ZONE 50. CORROSION ON FUSELAGE SKIN WAS REMOVED IAW SRM 51-10-3, PAR 26, WITH ORIGINAL THICKNESS IS 0.091" AND MINIMUM REMAINING THICKNESS 0.029" WAS FOUND OUT LIMITS, IT WAS REPAIRED IAW SRM 53-04, FIG 57 AND 51-30-5.