What was found
LARGE BIRD INGESTED AT 154 KTS ON TAKEOFF NO. 2 ENGINE. 3.8 VIBS . DID NOT S/D ENGINE. RTB. PRELIMINARY INSP REF AMM 05-51-18. SEVERAL FAN BLADES DAMAGED. DEACTIVATED TE & LE FLAPS & SLATS IAW AMM 27-51-00 & 27-81-00. DEACTIVATED TE FLAP BYPASS VALVE, SAFETY PIN INSTALLED. DEACTIVATED LE CRUISE DEPRESSURIZATION VALVE & ACCOPMLISHED BIRD STRIKE INSP IAW AMM 05-51-18-210-801. ONLY DAMAGE FOUND TO BE AT #2 ENGINE. INSTALLED SAFETY PIN. BOROSCOPE SHOWED NO INTERNAL DAMAGE. REPLACED FAN BLADE SET & ACOUSTICAL PANELS. REPAIRED FAN CASE ABRAIDABLE LINER. REPLACED OIL COOLERS IAW AMM 72-22-00. INSTALL NEW BLADE & FILLER SET IAW AMM 72-22-02-400-803-G00. FOUND 4 DEEP PUNCTURES IN ENGINE TWO INBOARD TR TRANSLATING SLEEVE INBOARD & OUTBOARD ACCOUSTIC PANEL. REF SRM 54-30-01-1A-6 , COMPLIED WITH EC/RA 7831-03331 PART 1 STEPS A, B & C. STEP C, ECRA 7831-03331 STEPS C - E, SRM 54-30-01. L REPLACED #2 ENGINE REF WORK CARD 61-7100-1-4800 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1809402 SN OFF 3391 ENGINE, BASIC, OFF 42-7200-9-0001 3391 ON 0000 ENGINE, BASIC, OFF 42-7200-9-0001 3391 ON 42-7200-9-0001 0598. ORIGINAL SUBMISSION DATE: 9/13/2023.