As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE BLEED FAULT. RIGHT WING BLEED LEAK DISPLAYED AFTER TAKEOFF. FOUND LEAK ABOVE NR 2 ENG PYLON AT DUCT CLAMP (REF IPC 36-11-05 FIG 02 ITEM 20). REPLACED CLAMP. LEAK WAS 2 INCHES IN FRONT OF RT WING LOOP -A- ELEMENTS 43HF AND 44HF.