What was found
DURING PUSH BACK, FOUND DMG 10" BOTTOM AFT OF RADOME. PERFORMED PRELIMINARY HFEC SURFACE SCAN OF PUNCTURE ON LOWER NOSE FWD OF PRESSURE BULKHEAD/CENTERLINE PER AIRBUS NTM TASK 51-10-08. CRACK IS APPROX 3/4" IN LENGTH W/ PUNCTURE IN UN-PRESSURIZED AREA. REMOVED DAMAGE PER A330 SRM 51-70-20. PERFORMED HFEC OF SKIN DAMAGE TRIM OUT INTERIOR AND EXTERIOR, AS WELL AS THE INTERNAL SURFACE OF P-DOME SKIN FLANGE AND EXTERNAL P-DOME SURFACE PER A330 NTM 51-10-08. NO CRACK INDICATIONS NOTED. PERFORMED U.T. MEASUREMENT OF REMAINING SURFACE THICKNESS AT TRIM PER A330 NTM 51-10-04. RESULTS SENT TO ENGINEERING. PERFORMED STEP 2 OF PRI IAW ERA 577214-14 REV. 0 ROTO - TEST OF OPEN HOLES, NO CRACKS OR INDICATIONS NOTED FABRICATED REPAIR PARTS PER FIG 4. PRI 577214-14 REV 2 ADDED ADDITIONAL HOLES. PERFORMED STEP 2 OF PRI 577214-14 REV. 0 ROTO - TEST NO CRACKS NOTED, PERFORMED TIME LIMITED REPAIR PER ERA 577214-14 REV ORIG.