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TRANSPONDER
IN
DC 2
BATT
IN
VHF COM 3 DC 1 IN
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
COMMUNICATIONS
EMS CIRCUIT PROTECTION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
06−20−1
CB - COMM SYSTEM (CONT'D)
Effectivity:
· Airplanes 9002 thru 9122 not incorporating Service Bulletin:
· SB 700−24−045, AC and DC Power Distribution − Unit Change and Activation of Build 4
Electrical System.
GF0620_002
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
CB − COMM SYSTEM 1/5
CB − COMM SYSTEM 2/5
CB − COMM SYSTEM 3/5
CB − COMM SYSTEM 4/5
CB − COMM SYSTEM 5/5
COMMUNICATIONS
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
06−20−2
DESCRIPTION
General 07−10−1
EPGDS Components 07−10−2
EPGDS Architecture 07−10−3
AC System 07−10−4
AC System Distribution 07−10−6
Electrical Panel 07−10−7
Electrical Management System 07−10−8
AC System EICAS Messages 07−10−14
AC System Synoptic 07−10−18
AC BUS Feed System 07−10−19
EXT AC Power 07−10−25
DC System 07−10−26
DC System Distribution 07−10−27
Electrical Panel 07−10−28
DC System EICAS Messages 07−10−29
DC System Synoptic 07−10−33
DC BUS Feed System 07−10−34
External DC Power 07−10−39
RAT GEN Feed 07−10−40
RAT Pilot Activated Test 07−10−41
Emergency DC Power 07−10−42
DC Power Emergency Override 07−10−43
EICAS Philosophy 07−10−45
EMS CIRCUIT PROTECTION
Cockpit Circuit Breaker Panel (CCBP) 07−20−1
EMS CDU 07−20−2
System Key 07−20−2
Next Page Key 07−20−2
Previous Page Key 07−20−2
Elec System Key 07−20−3
ELECTRICAL
TABLE OF CONTENTS
CHAPTER 7
07−00−1
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
07−00−1
Page
TABLE OF CONTENTS
EMS CIRCUIT PROTECTION
Bus Key 07−20−5
AC BUS 1 07−20−5
AC BUS 2 07−20−6
AC BUS 3 07−20−7
AC BUS 4 07−20−8
AC ESS BUS 07−20−9
DC EMER BUS 07−20−10
DC BUS 1 07−20−11
DC BUS 2 07−20−22
DC ESS BUS 07−20−35
BATT BUS 07−20−41
AV BATT BUS 07−20−53
APU BATT BUS 07−20−55
CNTL Key 07−20−56
Test Key 07−20−58
FIRE TEST 07−20−60
STALL TEST 07−20−61
AURAL WARNING TEST 07−20−62
LAMP TEST 07−20−63
RAT TEST 07−20−65
EMER CONT 07−20−66
ELECTRICAL
TABLE OF CONTENTS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
07−00−2
Page
GENERAL
The airplane electrical power generation and distribution system (EPGDS) consist of four 40 KVA,
enginedriven
variable frequency generators (VFG) and one constant frequency 40/45 KVA APU
generator. Control and protection of the generators are provided by five identical generator control
units (GCU). Distribution systems furnish power to the following busses through the AC power center
(ACPC) and the cockpit circuit breaker panel (CCBP).
· AC bus 1, 2, 3 and 4
· AC essential bus (normally powered by AC bus 4)
A ram air turbine (RAT) deployable during flight, supplies 115−volt, 400−Hz, 3−phase AC power
9 KVA for emergency use (when all other AC sources have been lost) to supply AC power to the AC
essential bus. Mounted on the RAT is a hydraulic pump which powers hydraulic system #3.
　
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