Question 1
What is the primary function of the Generator Control Unit (GCU) in an aircraft electrical system?
Question 2
What advantage does a Constant Speed Drive (CSD) provide in an Integrated Drive Generator (IDG) system?
Question 3
What is the role of a Transformer Rectifier Unit (TRU) in an aircraft electrical power system?
Question 4
If two identical 24 V, 40 Ah batteries are connected in parallel, what is the resulting voltage and capacity?
Question 5
In aircraft electrical generation, what defines a single-point failure?
