What was found
ALTITUDE UNRELIABLE F/O AIRSPEED UNRELIABLE F/O EEC ALT NO1 AND NO2 SPEED TRIM FAIL CREW INDICATED UPON TAKEOFF ROT LARGE BIRD NEAR MISS OR POSSIBLE STRIKE ON F/O SIDE. ASCENDED TO 37K, STRABILIZED AT 35K AND REPORTED DESCREPENCY IN LOG BEGAN. FOLLOWED PROCEDURE, DESCENDED TO 22K TAT1 AND SYSTEMS BEGAN OPERATING NORMAL.ERFORMED DFCS BITE CHECK, AMM 22-11-00-810-801 AUTOTEST PASS, FAULT HISTORY HAS CURRENT FAULTS. SEE ATTACHED ATTACHED ACCOMPLISHED F/O PITOT AND STATIC SYSTEM FLUSHING PER REF MM 34-11-00-170-801. F/O PITOT AND STATIC DRAINS ARE RECONNECTED. WHILE PERFORMING F/O PITOT AND STATIC SYSTEM LEAK CHECK. FOUNDED F/O AIR SPEED AND ALTITUDE LEAK CHECK READING LOWER THAN LAVERSAB TESTER READING. ADD EMP:6092 ACP. IDT INSPECTION IAW GMM 09-10-05 & AMM 34-11-00. VERIFIED RECONECTION, SAFETY & SECURITY OF QUICK DISCONNECTS. NO DEFECTS NOTED. ACPD FULL RANGE LEAK CK OF LEFT & RIGHT PITOT AND STATIC SYSTEMS GOOD, NO LEAKS. AIRSPEED AND ALTIMETRY ACCURACY GOOD USING ALTERNATE "PFD" METHOD IAW AMM 34-11-00-501, ALL READINGS STABLE AND WELL WITHIN TOLERANCE, NO STATUS MSGS, ACPD VISUAL INSP OF PITOT PROBES AND NOTED NO DEFECTS OR DEBRIS IAW AMM 34-11-01-200-804