What was found
BIRD STRIKE RIGHT SIDE OF FUSALAGE. REMOVED RT WING #4 LEADING EDGE SLAT REF AMM 27-81-21-000-801 CORRECTION RH #5 SLAT HAS BEEN REMOVED REF 27-81-21-000-801. NUMBER #4 WAS NOT REMOVED. INSTALLED NEW #5 SLAT PER AMM 27-81-21-400-801, OPS CHECK REQUIRED AFTER SLAT #6 HAS BEEN INSTALLED. COMPLETED LEADING EDGE SLAT INSTALLATION, REFERENCE: TASK 27-81-21-400-801, PERFORMED LEADING EDGE FLAPS AND SLATS ACTIVATION, REFERENCE: TASK 27-81-00-440-801, WING ANTI-ICING DUCT LEAK TEST, REF TASK 30-11-00-790-801, AND LEADING EDGE ACCESS PANEL INSTALLATION REF TASK 57-41-02-400-801. SLAT 5 INSPECTION SATISFACTORY IAW WITH REQS OF GMM 09-25-05 REFERENCING AMM 27-81-21.