What are possible sources of AC power on an aircraft?
A) AC generators, fuel pumps, and batteries
B) Static inverters, rotary inverters, and AC generators
C) Hydraulic pumps, AC generators, and static inverters
B) Static inverters, rotary inverters, and AC generators
In a rotating field alternator, which component is stationary?
A) Field
B) Armature
C) Rotor
B) Armature
What does CSD stand for?
A) Constant Speed Drive
B) Consistent Spindle Drive
C) Constant Spindle Distance
A) Constant Speed Drive
What device is used to convert variable engine speed into a constant output drive speed for a generator?
A) Variable Speed Drive (VSD)
B) Constant Speed Drive (CSD)
C) Auxiliary Power Unit (APU)
B) Constant Speed Drive (CSD)
What does IDG Stand for?
A) International Distance Generation
B) Instant Drive Generator
C) Integrated Drive Generators
C) Integrated Drive Generators
What is a key advantage of the Integrated Drive Generator (IDG) compared to the traditional two-unit system?
A) It uses more fuel
B) It is heavier and larger
C) It is lighter and smaller
C) It is lighter and smaller
How many Generator Control Units (GCUs) are there for each generator?
A) One
B) Two
C) Three
A) One
What are the three parts the functions can be divided into?
A) Generation, distribution, storage
B) Regulation, protection, switching
C) Conversion, transmission, grounding
B) Regulation, protection, switching
What does GCU stand for?
A) Ground Control Unit
B) Generator Control Unit
C) General Circuit Unit
B) Generator Control Unit
What is the aircraft battery generally used to supply?
A) Cabin lighting and entertainment systems
B) Emergency power and APU starter motor power
C) Hydraulic pump power and air conditioning
B) Emergency power and APU starter motor power
What is one function of the aircraft battery?
A) To power the landing gear
B) To provide electrical power capable of starting the engines
C) To operate the fuel system
B) To provide electrical power capable of starting the engines
What are the two main types of aircraft batteries fitted to aircraft?
A) Ni-Cd and Lithium-ion
B) Ni-Cd and Lead-acid
C) Lead-acid and Alkaline
B) Ni-Cd and Lead-acid
Which type of battery is most common today despite earlier problems with Thermal Runaway (TR)?
A) Lead-acid
B) Ni-Cd
C) Lithium-ion
B) Ni-Cd
Which part of the aircraft electrical system is protected by the electronic circuits of the GCU instead of fuses or circuit breakers?
A) Battery feeder lines
B) Generator feeder lines
C) Lighting circuits
B) Generator feeder lines
What devices can provide DC voltage on an aircraft?
A) Only DC generators
B) Batteries and Transformer Rectifier Units (TRU)
C) Only AC generators
B) Batteries and Transformer Rectifier Units (TRU)
What voltage levels do Transformer Rectifier Units (TRUs) typically provide?
A) 115 Vdc or 230 Vdc
B) 28 Vdc or 14 Vdc
C) 400 Vdc or 28 Vdc
B) 28 Vdc or 14 Vdc
What is the primary purpose of a Transformer Rectifier Unit (TRU)?
A) To convert DC voltage to AC voltage
B) To transform AC voltage to a lower level and rectify it to DC
C) To increase AC voltage from 28 V to 115 V
B) To transform AC voltage to a lower level and rectify it to DC
What does a parallel system consist of?
A) One generator connected to multiple buses
B) Two or more generators connected to a common power bus
C) Multiple batteries connected in series
B) Two or more generators connected to a common power bus
What happens when one generator fails in a system with a Bus Tie Breaker (BTB)?
A) The failed generator supplies both busbars
B) The BTB opens to isolate the busbars
C) The BTB closes, connecting the two busbars to be supplied by the serviceable generator
C) The BTB closes, connecting the two busbars to be supplied by the serviceable generator
What is one advantage of parallel systems in the event of a generator failure?
A) The defective generator continues to supply power
B) The buses are already connected, allowing isolation of the defective generator
C) The system shuts down completely
B) The buses are already connected, allowing isolation of the defective generator
What is the minimum duration that emergency electrical power systems on aircraft are designed to provide power?
A) 15 minutes
B) 30 minutes
C) 60 minutes
B) 30 minutes
What are typical sources of emergency electrical power on an aircraft?
A) Main Battery, Inverters, Auxiliary Power Unit (APU), Ram Air Turbine (RAT)
B) Fuel pumps, hydraulic pumps, and air conditioning units
C) Landing gear, flaps, and spoilers
A) Main Battery, Inverters, Auxiliary Power Unit (APU), Ram Air Turbine (RAT)
What is one function of the APU on an aircraft?
A) To provide hydraulic power only
B) To start the main engines and provide electrical power during flight if the main engine fails
C) To control the landing gear
B) To start the main engines and provide electrical power during flight if the main engine fails
What is a Ram Air Turbine (RAT) used for on an aircraft?
A) To provide normal electrical power during flight
B) To generate power from the airstream in emergencies
C) To increase aircraft speed
B) To generate power from the airstream in emergencies