근거 : A321/320 FCOM GENERAL The Auxiliary Power Unit (APU) is a self-contained unit that supplies the aircraft with pneumatic and electrical power. On the ground ‐ It supplies bleed air for starting the engines and for the air conditioning system ‐ It supplies electrical power to the electrical system.
During takeoff ‐ It supplies bleed air for air conditioning (for example, when optimum aircraft performance is required). In flight ‐ It backs up the electrical system ‐ It backs up the air conditioning ‐ It can be used to start the engines.
The APU may obtain power for starting from the ..........