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Vol. 1 09--60--2
EMERGENCY EQUIPMENT
Flight Compartment Emergency Equipment REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Flight Compartment Emergency Equipment
Figure 09---60---1
COVER
VELCRO
STRAP
ROPE
BOX
CREW
LIFE VEST
FLASHLIGHT
CRASH AX
FIRE
EXTINGUISHER
PORTABLE
BREATHING
EQUIPMENT
FLASHLIGHT
B
C
D
A
A
C D
B
Vol. 1 08--00--1
ENVIRONMENTAL CONTROL SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
CHAPTER 8 --- ENVIRONMENTAL CONTROL SYSTEM
Page
TABLE OF CONTENTS 08--00
Table of Contents 08--00--1
INTRODUCTION 08--10
Introduction 08--10--1
AIR-CONDITIONING SYSTEM 08--20
Air--Conditioning System 08--20--1
Packs 08--20--1
Temperature Control 08--20--5
Ram Air Ventilation 08--20--7
Conditioned Air Distribution 08--20--9
Low Pressure Ground Air Connection Panel <1007> 08--20--11
System Circuit Breakers 08--20--12
AVIONICS COOLING SYSTEM 08--30
Avionics Cooling System 08--30--1
System Circuit Breakers 08--30--7
AFT CARGO BAY VENTILATION SYSTEM 08--40
AFT Cargo Bay Ventilation System 08--40--1
System Circuit Breakers 08--40--4
LAVATORY AND GALLEY VENTILATION SYSTEM 08--50
Lavatory and Galley Ventilation System 08--50--1
System Circuit Breakers 08--50--1
PRESSURIZATION SYSTEM 08--60
Pressurization System 08--60--1
Cabin Pressure Controllers 08--60--8
Automatic Pressurization Modes 08--60--8
Manual Pressurization Modes 08--60--9
Safety Valves 08--60--9
Ground Valve 08--60--9
Cabin Altitude Limitation 08--60--9
Emergency Depressurization 08--60--9
Cabin Pressure Monitoring 08--60--10
System Circuit Breakers 08--60--10
Vol. 1 08--00--2
ENVIRONMENTAL CONTROL SYSTEM
Table of Contents REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
LIST OF ILLUSTRATIONS
INTRODUCTION
Figure 08--10--1 Air Conditioning System 08--10--2
AIR-CONDITIONING SYSTEM
Figure 08--20--1 Air Conditioning Unit Schematic 08--20--2
Figure 08--20--2 Packs Control 08--20--3
Figure 08--20--3 Packs EICAS Indications 08--20--4
Figure 08--20--4 Temperature Controls 08--20--5
Figure 08--20--5 Temperature Synoptic and EICAS Indications 08--20--6
Figure 08--20--6 RAM Air Control 08--20--7
Figure 08--20--7 Temperature Synoptic and EICAS Indications 08--20--8
Figure 08--20--8 Recirculation Air Control 08--20--9
Figure 08--20--9 Air Distribution Schematic 08--20--10
Figure 08--20--10 Low Pressure Ground Air Connection <1007> 08--20--11
AVIONICS COOLING SYSTEM
Figure 08--30--1 Cockpit Displays and Avionics Cooling System Schematic 08--30--2
Figure 08--30--2 Avionics Cooling System--General 08--30--3
Figure 08--30--3 Display Fan Controls 08--30--4
Figure 08--30--4 Avionics Cooling EICAS Indications 08--30--5
Figure 08--30--5 Display Overtemperature Indications 08--30--6
AFT CARGO BAY VENTILATION SYSTEM
Figure 08--40--1 Cargo Compartment Air System Schematic 08--40--2
Figure 08--40--2 AFT Cargo Bay EICAS Indication 08--40--3
PRESSURIZATION SYSTEM
Figure 08--60--1 Pressurization System -- General 08--60--2
Figure 08--60--2 Pressurization Controls 08--60--3
Figure 08--60--3 Pressurization EICAS Synoptic Page Message 08--60--4
Figure 08--60--4 Pressurization EICAS Synoptic Page Elements 08--60--5
Figure 08--60--5 Pressurization EICAS Indications -- Primary Page 08--60--6
Figure 08--60--6 Pressurization EICAS Indications -- Status Page 08--60--7
Vol. 1 08--10--1
ENVIRONMENTAL CONTROL SYSTEM
Introduction REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. INTRODUCTION
The environmental control system (ECS) provides temperature and pressure regulated air
for heating, ventilating and for pressurizing the flight and passenger compartments. Exhaust
air from each compartment is used to ventilate the avionics and cargo compartments, before
being dumped overboard through an outflow valve and a ground valve.
For ground operations, pneumatic air for operation the ECS can be obtained from any of the
following:
S A ground air supply cart connected to the aircraft
S The auxiliary power unit (APU)
S Either or both engines.
During flight, the engines normally supply bleed air for operating the air-conditioning,
pressurization, and avionics cooling systems.
ECS warnings and cautions are displayed on the engine indication and crew alerting system
(EICAS) primary page. ECS advisory and status messages are displayed on the EICAS
 
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