As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRONG HYDRAULIC SMELL IN THE COCKPIT. *S/D* SMELL DUE TO HYDRAULIC LEAK OF HYD SYSTEM NR 1 TUBE LOCATED IN FWD PIT AT AFT SIDE OF STA 900, STRINGER 28L. PIN HOLE DEVELOPED DUE TO CHAFING UNDER CLAMP. ACCOMPLISHED TUBE RINGLOCK REPAIR. LEAK CHECK ACCOMPLISHED ON REPAIR AREA, NO LEAKS. AIRCRAFT RETURNED TO SERVICE.