What was found
SURFACE HFEC INSPECTION FOUND 02EA CRACKS (FWD CRACK APPROX.0.700 INCH IN LENGTH AND AFT CRACK APPROX.0.650 INCH IN LENGTH) ON THE EXTERNAL SUR FACE OF THE FUSELAGE SKIN AROUND THE 2 HOLES COMMON TO THE LEFT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MARK AS PER W/C EO G5310-E0332629 K P5 STEP 9. C. THE 02 EA CRACKS FOUND WITHIN THE TRIM LINE BOUNDARY IN BOEING DRAWING 675W0002 SHEET 7 VIEW IC14 ,REPAIR CARRIED OUT AS PER EO : G-5310-EO332629K.P5.STEP 11. REPAIR CLASSIFIED AS MAJOR PER GMM6-2-100.