CPL » Air Tech (A) » Electrical Systems - DC
26.30 Electrical Systems - DC
26.30.2 Describe the systems which typically require DC power in an aircraft.
26.30.4 Explain the function(s) of the following in a typical electrical system:
(a) the battery;
(b) a ground power source;
(c) the alternator or generator;
(d) bus bars;
(e) over voltage protection.
26.30.6 Given appropriate data, determine the duration of battery operation following a generator failure.
26.30.8 Describe the relative advantages and disadvantages of:
(a) a generator;
(b) an alternator.
26.30.10 Explain the functions and interpretation of:
(a) left-zero ammeters;
(b) centre-zero ammeters.
26.30.12 Explain the functions and correct operation of a:
(a) single battery master switch;
(b) split battery/alternator switch.
26.30.14 Explain the operation of:
(a) fuses;
(b) circuit breakers;
(c) overload switches.
26.30.16 Explain operational principles for the handling of the electrical DC system, including: