As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER TAKEOFF NOTICED BLEED AIR SPLIT AT CLIMB POWER. ACCOMPLISHED BLEED AIR SYSTEM HEALTH CHECK REF MM 36-11-00. HIGH STAGE VALVE FOUND TO BE INTERMITTENT DURING PRESSURE CHECK. REPLACED NR1 ENGINE HIGH STAGE VALVE REF MM 36-11-06, OPS NORMAL DURING TEST. AS PRECAUTIONARY REPLACED HIGH STAGE REGULATOR REF MM 36-11-07 OPS & LEAK CHECKED NORMAL.