What was found
DURING S90M C CHECK OF DATUM A/C 1. REPAIR ON THE RT FUSELAGE SKIN AT STA Y=484,L18R-L19R (526). CORROSION ON LE WING REAR SPAR LOWER CAP AT STA XRS510 AND XRS 550(527).3.A CRACK DAMAGE ON RT FUSELAGE SKIN (P/N:5910228-259) BETWEEN CANTED STA 1520-1531 (529).4.CORROSION ON FUSELAGE FRAME LOWER T-CHORD AT STA Y=1437,BETWEEN L-29R AND L-28R (530). 5.CORROSION ON RT OUTBD FLAP INBD VANE(P/N:5930496-510) TRAILING EDGE LOWER SURFACE (533). 6.TWO AREAS DAMAGE WITH CRACK AND OIL-CANNING ON LT FUSELAGE SKIN BETWEEN CANTED STA 1520-1531(537). 7.REPAIR ON FUSELAGE SKIN AT STA Y=434(538). 8.CRACKS ON DOUBLER AND CAP OF FUSELAGE BULKHEAD AT CANTED STA 1520L-3L(539).9.REPAIR ON FUSELAGE SKIN