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FMS CDU 1 DC BUS 1 H9
PRE SB
604–24–002
FMS CDU 2 DC BUS 2 2 H9
FMS CDU 3 DC ESS 4 D9
5302 & POST SB
604–34–002
FMS DATA LOAD
DC BUS 1 1
H10
GPS
GPS 1 H11 5301–5303, 5306
& POST SB
604–34–007 or
604–34–018
GPS 2 DC BUS 2 2 H11
Inertial Reference
System
IRU 1
AC ESS 3
C1
IRU FAN 1 C2
IRU BATT 1 DC BATT 1 Q8
IRU 2
AC BUS 2 2
B14
IRU FAN 2 B15
IRU BATT 2 DC ESS 4 D8
IRU 3
AC BUS 1
1
B14
POST SB
604–24–004
IRU FAN 3 B15
IRU BATT 3 DC BATT Q9
Radio Altimeter
RAD ALT 1 DC BUS 1 H14
RAD ALT 2
DC BUS 2 2
H14
POST SB
604–24–005
Lightning Sensor
LIGHTNING
SENSOR
H6
5302 & POST SB
604–34–008
NAVIGATION SYSTEMS
Summary
Vol. 2 17−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY (CONT'D)
SYSTEM SUB-SYSTEM CB NAME BUS BAR
CB
PANEL
CB
LOCATION
NOTES
Navigation
Systems
Weather Radar
WEATHER RDR
R/T
DC BUS 1 1
K1
WEATHER RDR
CONT 1
K2
WEATHER RDR
CONT 2
K3
POST SB
604–24–006
Traffic Collision
Avoidance System
TCAS AC ESS 3 C5
5301–5303, 5306
& POST SB
604–34–001 or
604–34–017
Ground Proximity
Warning System
GPWS AC BUS 1 1 B13
5301–5303, 5306
& POST SB
604–34–003 or
604–34–016
NAVIGATION SYSTEMS
Summary
Vol. 2 17−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
DESCRIPTION
General 18−10−1
10th-Stage Bleed Air 18−10−2
Description 18−10−2
Components and Operation 18−10−2
14th-Stage Bleed Air 18−10−4
Description 18−10−4
Components and Operation 18−10−5
Bleed Air Leak Detection System 18−10−6
Description 18−10−6
Components and Operation 18−10−7
Controls and Indicators 18−10−10
BLEED AIR Panel 18−10−10
EICAS STATUS Page 18−10−11
EICAS Messages 18−10−11
SUMMARY
Power Supply and Circuit Breaker Summary 18−20−1
LIST OF ILLUSTRATIONS
DESCRIPTION
Figure 18−10−1 Pneumatic Schematic 18−10−1
Figure 18−10−2 10th-Stage Bleed Air Schematic 18−10−2
Figure 18−10−3 14th-Stage Bleed Air Schematic 18−10−5
Figure 18−10−4 Bleed Air Leak Detection Sensing Elements and Thermal
Switches 18−10−7
Figure 18−10−5 Bleed Air Leak Detection System Capabilities 18−10−9
Figure 18−10−6 BLEED AIR Panel 18−10−10
Figure 18−10−7 EICAS STATUS Page − Bleed Pressure Readouts 18−10−11
PNEUMATIC
Table of Contents
Vol. 2 18−00−1
REV 66, Feb 01/07
CHAPTER 18 - PNEUMATIC
18−00−1
CL−604 Operating Manual
PSP 604−6
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
PNEUMATIC
Table of Contents
Vol. 2 18−00−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
The pneumatic system consists of two separate bleed air systems; 10th-stage and 14th-stage bleed
air. The 10th-stage bleed air is supplied from the engines, the APU or an external air source. The
14th-stage bleed air is supplied from the engines.
The pneumatic system also includes a bleed air leak detection system that warns the flight crew of
possible duct ruptures.
Pneumatic Schematic
Figure 18−10−1
PNEUMATIC SYSTEM
Description
Vol. 2 18−10−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
10TH-STAGE BLEED AIR
Description
The 10th-stage bleed air is supplied from the left and right engine compressor’s 10th-stage, the
APU or an external air source. The bleed air is distributed to the various systems by the 10th-stage
bleed air manifold.
Bleed air from the 10th-stage manifold is used for:
• Engine starting; and
• Air conditioning and pressurization.
　
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