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TABLE OF CONTENTS
CHAPTER 5
Page
TABLE OF CONTENTS 05.00.1
DESCRIPTION
General 05.10.1
APU Access and Component Location 05.10.2
APU Compartment 05.10.2
APU General Arrangement 05.10.3
APU System Schematic 05.10.3
Lubrication 05.10.4
Oil Pressure 05.10.4
Gravity Oil Fill 05.10.4
Oil Replenishment System 05.10.4
Oil Replenishment System Filling 05.10.6
Oil Replenishment Panel 05.10.7
Operation 05.10.7
Fuel Control and Indication 05.10.8
Airframe Fuel 05.10.8
Ignition 05.10.9
Start System 05.10.9
Speed Indication 05.10.9
Temperature Indication 05.10.9
Hourmeter/Cycle Counter 05.10.9
ECU Component Control Schematic 05.10.10
Control System 05.10.10
Pneumatic 05.10.10
APU System Operating Modes 05.10.12
ECU Power-up 05.10.12
Start Mode 05.10.12
On-speed Mode 05.10.12
Cooldown Mode 05.10.12
Shutdown Mode 05.10.12
APU System Operating Sequence 05.10.12
APU Starting 05.10.12
APU Door Positioning 05.10.12
APU Loading 05.10.13
APU Shutdown 05.10.13
APU Door Operation and Indication 05.10.14
Door Operation 05.10.14
Door Indication 05.10.14
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AUXILIARY POWER UNIT
TABLE OF CONTENTS
Page
DESCRIPTION
APU RPM and EGT Indications 05.10.14
APU Fire Protection 05.10.15
APU Control Panel 05.10.15
Start Sequence 05.10.16
Normal Shutdown 05.10.16
Emergency Shutdown 05.10.16
APU Emergency Shut-off Buttons 05.10.17
Restart After Emergency ShutDown 05.10.17
Protective Shutdowns 05.10.18
System Overview Schematic 05.10.19
Electrical Power and Distribution 05.10.20
Start Control Schematic 05.10.20
FADEC Inputs and Outputs 05.10.21
ECU Schematic 05.10.22
EICAS Messages 05.10.23
EMS CIRCUIT PROTECTION
CB . APU System 05.20.1
Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
GENERAL
An Allied-Signal RE 220 gas turbine Auxiliary Power Unit (APU) is installed in a fire proof enclosure in the tail cone of the airplane (beneath the airplane rudder and elevator control systems) and has a fire detection element system (see Fire Protection System Chapter 9). The APU is installed outside of the main engine rotor burst zone which enhances airplane high altitude operation.
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