DASSAULT FALCON 7X — Systems Description
1 systems description reference for the DASSAULT FALCON 7X.
Overview
DASSAULT FALCON 7X SYSTEMS SUMMARY Auxiliary Power Unit
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.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
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