DASSAULT FALCON 7X — Systems Description

The document provides a summary of the systems related to the Auxiliary Power Unit (APU) of the Dassault Falcon 7X aircraft. It covers the APU's operation, controls, indications, and various systems including fuel, ignition, and electronic control.

• The Falcon 7X APU is a HONEYWELL 36-150 gas turbine engine.
• The APU provides bleed air for the Environmental Control System and electrical power.
• APU operation is electronically controlled and intended for ground use only.
• The APU is equipped with an automatic ignition and starting system.
• The APU is enclosed in a fireproof enclosure for safety.
• The APU can power the entire DC electrical system and charge batteries.
• The ECU manages APU operation and provides automatic shut down protections.
• The APU is located in the aft fuselage section of the aircraft.