Manufacturer
Bombardier
Number
Transport Canada CF-2023-78
Model(s)
Challenger 604, 605, and 650
Published Date
Effective Date
Summary
Requires revising the airplane flight manual, verifying aircraft technical records, cleaning of printed circuit boards, and modification of the left-hand direct current power center (DCPC) internal communication data bus units. Prompted by multiple in-service reports of erratic electrical system status on the push button annunciators and EICAS while on-ground and during flight. Several of these incidents resulted in the airplane experiencing a momentary loss of electrical power and loss of flight displays following crew action. During the investigation, it was found that airplanes can experience misleading electrical system status indications as a result of contamination of electrical contacts in the left-hand DCPC internal communication data bus. The erratic indications could cause the crew to turn off fully operational electrical power sources, leading to partial or complete loss of electrical power.
Company Reference
Aircraft Reference