What was found
DUCT PRESSURE SPLIT ON CLIMB AT 10,000 FT L14/ R34 20K, L13 R32, 30K, L13, R24, AT CRUISE 380K L16/R23. REMOVED AND REPLACED NR 1 ENG BLEED AIR REGULATOR IAW 36-11-03-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DUCT PRESSURE SPLIT ON CLIMB AT 10,000 FT L14/ R34 20K, L13 R32, 30K, L13, R24, AT CRUISE 380K L16/R23. REMOVED AND REPLACED NR 1 ENG BLEED AIR REGULATOR IAW 36-11-03-4.