C25C First Officer reported multiple system failures during departure climb. Flight crew returned to departure airport uneventfully.
Synopsis
C25C First Officer reported multiple system failures during departure climb. Flight crew returned to departure airport uneventfully.
Narrative
We were climbing through 33;000 feet with FL450 as final; when we heard the voice announcement LEFT OIL PRESS LOW LEVEL. Both pilots checked the EICAS and found all these messages: BLEED AIR MONITOR FAIL L; WINDSHIELD HEAT FAIL L; PITOT/STATIC COLD STBY; PITOT/STATIC COLD L; AP PITCH TRIM FAIL; RUDDER BIAS FAIL; AC ALTERNATOR FAIL L; SPEED BRAKES FAIL; FLAPS FAIL; PRESSURIZATION CONTROL; PRIMARY ELEVATOR TRIM FIAL.Airplane was fly able and because we had visual conditions we decided to return to land to ZZZ airport; were we departed from company facilities. During descent we had pitch trim runaway; AP failure; CABIN PRESS caution message descending through 18;000 feet; we had to manually extent the landing and land with no flaps nor speed brakes.This situation was accomplished uneventfully because of the visual conditions. On IFC and/or ice formation; the outcome would have been totally different.At Company Center; after a complete evaluation; determined that the problem was a faulty CB. What a dangerous situation for just a tiny peace of metal! Nevertheless; there's a second part of this story. Next will be posted dated Day 0 when they found corrosion inside cockpit of our airplane.
Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.