What was found
BIRD STRIKE ON T/O, LOSS OF AIRSPEED ON RT SIDE INTERMITTENT ON LT SIDE AIRSPEED. FOUND EVIDENCE OF BIRD STRIKE AT RADOME, PITOT TUBES, WING L/E. INSPECTED AND CLEANED AREAS IAW AMM 12-22-01. NO DENTS OR DEFECTS NOTED. OVERWEIGHT LANDING, OVER BY 200 LBS. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-04 PAGE 605, TABLE 601 A1 CHECK INSPECTION, NO DEFECT NOTED. REF ITEM 1 ABOVE, DURING BIRD STRIKE CONDITION CHECK FOUND EVIDENCE OF BIRD INGESTION ON RT ENG INLET. CLEANED MINIMAL BIRD FEATHERS OUT OF RT ENGINE IAW AMM 12-22-01, INSPECTED RT ENGINE IAW AMM 05-51-08 PAR 25, LT NO DEFECT NOTED. GROUND RAN RT ENGINE IAW 71-00-00 ALL PARAMETERS CHECK IN LIMITS. REF ITEM 1 ABOVE, DURING BIRD STRIKE CONDITION CHECK FOUND EVIDENCE OF BIRD INGESTION ON LT ENGINE INLET. CLEANED MINIMAL BIRD FEATHERS OUT OF LT ENGINE IAW AMM 12-22-01, INSPECTED LT ENGINE IAW AMM 05-51-08 PAR 25, LT NO DEFECT NOTED. GROUND RAN LT ENG IAW 71-00-00 ALL PARAMETERS CHECK IN LIMITS. REF TO ITEM 3, INSPECT NR 2 ENGINE INLET C1 AND CORE AREA FOR INGESTION OF BIRD. INSPECTED NR 2 ENGINE INLET AND CORE AREA FOR INGESTION OF BIRD. FOUND NO DAMAGE INLET AREA OR THE CORE AREA, NO EVIDENCE OF BIRD INGESTION C1 AND CORE AREA IAW AMM 72-00-00. REF TO ITEM 4, INSPECT NR 1 ENGINE INLET C1 AND CORE AREA FOR INGESTION OF BIRD. INSPECTED NR 1 ENGINE INLET AND CORE AREA FOR INGESTION OF BIRD. FOUND NO DAMAGE INLET AREA OR THE CORE AREA, NO EVIDENCE OF BIRD INGESTION C1 AND CORE AREA IAW AMM 72-00-00. IN REF TO ITEM NR 1, BIRD STRIKE ON T/O, CLEANED DEBRIS AT LT & RT PITOT TUBES, PURGED PITOT AND STATIC LINES WITH DRY NITROGEN. PERFORMED PITOT STATIC LEAK CHECK IAW AMM 34-11-00. LEAK CHECK FAILED. IN REF TO ITEM NR 7, LEAK CHECK FAILED, T/S SYSTEM FOUND F/O'S PIPE ASSY PITOT DRAIN PN 7912645-532 CRACKED. R & R LINE IAW AMM 20-12-04 & 20-30-02 PERFORMED PRESSURE LEAK CHECK IAW AMM 34-11-00, LEAK CHECK PASSED..