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AIR CONDITIONING AND PRESSURIZATION Table of Contents Vol. 2 02.00.1
Oct 05/06
CHAPTER 2 - AIR CONDITIONING AND PRESSURIZATION
TABLE OF CONTENTS
Page
TABLE OF CONTENTS 02.00.1
DESCRIPTION
General 02.10.1
Air Conditioning System 02.10.1
Description 02.10.1
Components and Operation 02.10.1
Pressurization System 02.10.9
Description 02.10.9
Components and Operation 02.10.10
Controls and Indicators 02.10.20
General 02.10.20
EICAS Messages 02.10.23
SUMMARY
Power Supply and Circuit Breaker Summary 02.20.1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 02.10.1 Air Conditioning Pack . Schematic 02.10.3
Figure 02.10.2 Air Conditioning Distribution 02.10.5
Figure 02.10.3 Flight Compartment Fan Sensor 02.10.6
Figure 02.10.4 AIR CONDITIONING Panel 02.10.8
Figure 02.10.5 Cabin Pressurization Schematic 02.10.12
Figure 02.10.6 Cabin Pressurization Schedule 02.10.13
Figure 02.10.7 CABIN PRESSURIZATION Panel 02.10.14
Figure 02.10.8 Typical Flight Pressurization Profile 02.10.17
Figure 02.10.9 Takeoff at Sea Level to Land at 14,000 feet 02.10.18
Figure 02.10.10 Takeoff at 14,000 feet to Land at Sea Level 02.10.19
Figure 02.10.11 AIR CONDITIONING Panel 02.10.20
Figure 02.10.12 CABIN PRESSURIZATION Panel 02.10.21
Figure 02.10.13 Air Conditioning and Pressurization Indications 02.10.22
Figure 02.10.14 Air Conditioning and Pressurization Indications 02.10.23
AIR CONDITIONING AND PRESSURIZATION Table of Contents Vol. 2 02.00.2
Oct 05/06
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CL.605 Flight Crew Operating Manual
PSP 605.6
AIR CONDITIONING AND PRESSURIZATION Description Vol. 2 02.10.1
Oct 05/06
The air conditioning system provides temperature-regulated, conditioned air to the cockpit and passenger cabin using two air conditioning units (ACU’s), commonly referred to as “packs”.
An electric cockpit heating system and an avionics cooling system are also provided.
Aircraft pressurization is accomplished by regulating the overboard discharge of the conditioned air through two outflow valves. The automatic pressurization system maintains cabin pressure to provide passenger comfort throughout all phases of flight within the limitations of the aircraft structure.
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