As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLEED 1 LEAK DISPLAYED DURING CLIMB AT APPROX 3000 FEET. (CREW STATED THEY WERE NOT OVER WEIGHT AND F/O GREASED THE LANDING AT ABOUT 200 FT/MIN). MEL C08336 36-1-1. ENGINE BLEED SYSTEMS. PERFORMED OPERATIONAL TEST OF AIR BLEED SYSTEM PER AMM 36-00-00-700-803-A, OPS CK GOOD NO DEFECTS NOTED ON VISUAL INSPECTION OF BLEED 1 COMPONENTS. CHECKED #1 BLEED VALVE. CLEAR MEL.