What was found
ENGINE DUCT PRESSURES SPLIT DURING TAKEOFF OR CLIMB. ISOLATION VALVE CLOSED & BLEED SWITCH SELECTED ON. RECORDED DUCT PRESSURES. LEFT-42 RIGHT-36. REPLACED OVERTEMP STRUT BLEED SENSOR PER MM. OPS CHECKED GOOD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ENGINE DUCT PRESSURES SPLIT DURING TAKEOFF OR CLIMB. ISOLATION VALVE CLOSED & BLEED SWITCH SELECTED ON. RECORDED DUCT PRESSURES. LEFT-42 RIGHT-36. REPLACED OVERTEMP STRUT BLEED SENSOR PER MM. OPS CHECKED GOOD.