|
canaetair
ctiaiientyer
OPERATING MANUAL
PSP 601A-6
SECTION 7
ELECTRICAL
TABLE OF CONTENTS
Page
1. GENERAL 1
2. AC GENERATION SYSTEMS 1
A. Primary Generating System 1
B. Auxiliary Generating System 1
C. Emergency Generating System 2
3. DC GENERATION SYSTEMS 2
A. Static Conversion System 2
B. Battery System 3
4. EXTERNAL POWER 3
5. ELECTRICAL LOAD DISTRIBUTION 4
LIST OF ILLUSTRATIONS
Figure
Number Title Page
1 AC Generation Systems - Layout 5
2 DC Generation Systems - Layout 6
3 Electrical Power Generation and Distribution System - 7/8
Basic Configuration
4 Primary AC Power Control 9
5 Auxiliary AC Power Control 10
6 Main DC Power Control 11
7 Essential AC Power and ADG Control 12
8 External Power and Battery Control 13
9 AC and DC Metering 14
7-CONTENTS
Page 1
Apr 02/87
OPERATING MANUAL
PSP 601A-6
Figure Title Page
Number
10 Main AC No. 1 and DC No. 1 Circuit Breaker Panel 15
11 Battery Bus - Left Circuit Breaker Panel 16
12 Main AC No. 2 and DC No. 2 Circuit Breaker Panel 17
13 Battery Bus - Right Circuit Breaker Panel 18
14 AC Essential Bus Circuit Breaker Panel 19
15 DC Essential Bus Circuit Breaker Panel 20
16 Aft Electrical Distribution Box Circuit Breaker Panel (2 Sheets) 21
7 - CONTENTS
Page 2
Apr 10/95
chauenaer
OPERATING KANUAL
PSP 6 0 U -6
SECTION 7
ELECTRICAL
GENERAL
The electrical power generating system consists of the AC generation systems,
the DC generation systems, the external power system and the electrical load
distribution.
AC GENERATION SYSTEMS (Figures 1 and 2)
A. Primary Generating System
The primary generating system normally supplies all i n - f l i g h t aircraft
electrical power requirements- The system consists of two engine-driven
integrated drive gpnerators (IDG), GEN 1 and GEN 2. Each generator
provides a 115/200-volt, 400-Hz output, with a maximum power rating of
30 kVA.
Each generator normally supplies power to the associated distribution
system. GEN 1 supplies power to ac main bus No. 1, the ac essential bus,
TRU 1 and ac utility bus No. 1. The ac essential bus supplies the
essential loads and ESS TRU 1. GEN 2 supplies power to ac main bus No. 2,
TRU 2 , ESS TRU 2, ac u t i l i t y bus No. 2 and the main battery charger.
If either generator f a i l s , the associated bus is transferred automatically
to the other generator and both ac u t i l i t y busses are disconnected. The
automatic transfer circuit can be inhibited using the AUTO OFF/FAIL
switch/lights. To restore the services of the ac u t i l i t y busses, the APU
generator must be brought on line (refer to paragraph B.).
Under bus tie conditions, if an overload occurs in the bus t i e , the
generator control circuit de-energizes the transfer contactors, removing
power from the failed side distribution panels. If power i s lost from ac
main bus No. 1, the essential transfer contactor automatically transfers
the ac essential bus to ac main essential bus No. 2. When both IDGs are
operating, the ac essential bus can be manually transferred to the ac main
bus No. 2 (refer to Figure 7).
The GEN 1 and GEN 2 operation can be monitored on the power management
panel (refer to Figures 4 and 9).
B. Auxiliary Generating System
The auxiliary generating system supplies aircraft electrical power on
ground in lieu of external power and can also supply power in flight if
both IDGs fail. The system consists of an APU-driven generator with the
same power capability as a single IDG. When the aircraft i s on the ground
with the flaps at zero degrees, and the APU-driven generator is on line,
SECTION 7
Page 1
Apr 02/87
OPERATING MANUAL
PSP 601A-6
all busses receive electrical power, with the exception of the ADG bus. In
flight or with the flaps greater than zero degrees, the u t i l i ty busses are
disconnected,
The APU-driven generator operation can be monitored on the power management
panel (refer to Figures 5 and 9).
Emergency Generating System (Figure 7)
The emergency generating system supplies emergency electrical power for
limited distribution to essential ac services. The system consists of an
automatically deployed, air-driven generator (ADG). The generator provides
a 115/200-volt, 400-Hz output with a maximum power rating of 15 kVA at or
above airspeeds of 160 knots.
If all ac power is lost, the ADG i s deployed automatically. If automatic
deployment fails, the ADG can be deployed manually by operating the ADG
manual deploy handle located on the centre pedestal. When the ADG comes on
line, the ADG ac emergency transfer contactor transfers the ac essential
bus to the battery bus. The ADG bus receives power only when the ADG is
operating.
The ADG operation can be monitored on the AC METERING section of the power
management panel (refer to Figure 9).
DC GENERATION SYSTEMS (Figures 2 and 3)
A. Static Conversion System
The dc static conversion system converts the output of the ac
generating system into unregulated 28-volt main dc power. The system
consists of four transformer rectifier units (TRU). TRU 1, TRU 2 and
ESS TRU 2 receive primary ac power from the main ac busses and
ESS TRU 1 receives this power from the ac essential bus.
The TRU 1 and TRU 2 supply the dc bus No. 1 and dc bus No. 2
respectively. ESS TRU 1 and ESS TRU 2 supply the dc essential bus.
If TRU 1 or TRU 2 f a i l s , the affected bus can be transferred to the
operating TRU, using the bus t i e switch/lights on the power managment
panel (refer to Figure 6). When the bus tie function is selected, the
dc utility bus No. 1 and dc u t i l i t y bus No. 2 are disconnected. The
ESS TRU 1 and ESS TRU 2 are dedicated to the dc essential bus and
cannot be used to supply either the dc bus No. 1 or dc bus No. 2. If
ESS TRU 1 or ESS TRU 2 fails, the dc essential bus can be supplied
from the operating ESS TRU, or in an emergency condition (all ac power
l o s t ) , by deploying the ADG. During ADG operation, the battery bus
and the dc essential bus are connected.
During transfer to ADG, when the aircraft is in a weight-off-wheels
condition and the battery bus i s unpowered, the dc essential bus is
supplied from the battery direct bus via the DC EMER TIE CONTROL 2
contactor.
SECTION 7
Page 2
Apr 02/87
OPERATING MANUAL
PSP 601A-6
B. Battery System
The battery system consists of the main battery and the auxiliary
battery.
The main battery system provides emergency dc power to the battery bus
and the battery direct bus when primary dc power is lost due to a
complete ac power failure (TRU 1, TRU 2, ESS TRU 1 and ESS TRU 2 are
unavailable).
The main battery provides a nominal output of 25 volts and has a capacity
of 43 ampere-hours at the 1-hour rate. A battery charger is connected
directly to the battery and operates automatically, when ac power is
available, to maintain the battery in a fully charged condition.
The main battery system supplies the battery bus via the battery
contactor which is activated when the battery bus is unpowered due to a
TRU failure, provided that the BATTERY MASTER switch on the
IGNITION/ELECT PWR panel is set to ON (refer to Figure 8)-
If an overload condition occurs on the battery bus, the battery RCCB
trips and disconnect the battery. When the battery RCCB trips, the BATT
CONT circuit breaker also trips. It is necessary to reset the BATT CONT
circuit breaker (CBP-E) before resetting the BATT RCCB CONT circuit
breaker (CBP-D).
The main battery operation can be monitored on the DC METERING section of
the power management panel (refer to Figure 9).
On aircraft 5001 thru 5134,
the auxiliary battery provides dc power to start the APU during cold
temperature conditions (refer to SECTION 5).
On aircraft 5135 and subsequent and aircraft incorporating Canadair
Service Bulletin 601-0418,
IRS 2 battery provides dc power to start the APU during cold temperature
conditions (refer to SECTION 5).
4. EXTERNAL POWER (Figures 3 and 8)
The aircraft can be supplied with electrical power from an external power
source through the ac and dc receptacles located on the lower fuselage.
External power is an alternative source to the auxiliary generating system
power.
When the APU generator is running and on line, the external power supply is
take off line. The external power supplies all the busses except the ADG
bus. When the flaps are greater than zero degrees or the aircraft is in a
weight-off-wheels condition, the utility busses are disconnected.
SECTION 7
Page 3
Apr 10/95
canadair
ctiauencfer
OPERATING MANUAL
PSP 601A-6
5. ELECTRICAL LOAD DISTRIBUTION
The electrical power is distributed through the following circuit breaker
panels:
- CBP-A i s located on forward bulkhead behind pilot's position and is divided
into two sections. One section contains the 115-volt ac main bus No. 1, the
28-volt dc main bus No- 1, the 115-volt ac u t i l i t y bus No. 1 and the 28-volt
dc u t i l i t y bus No- 1 circuit breakers. The other section contains the
battery bus circuit breakers (refer to Figures 10 and 11).
- CBP-B i s located on forward bulkhead behind copilot's position and is divided
into two sections. One section contains the 115-volt ac main bus No. 2, the
28-volt dc main bus No. 2, the 28-volt dc u t i l i ty bus No. 2 and the 115-volt
ac u t i l i t y bus No. 2 circuit breakers. The other section contains the
battery bus, the 26-volt ac bus, and the 115-volt ac main bus No. 2 circuit
breakers (refer to Figures 12 and 13).
- CBP-C i s located in the flight compartment on pilot's left console and
contains the 26-volt ac essential bus, the 115-volt ac essential bus and the
115-volt ac ADG bus circuit breakers. The other section contains the battery
bus, the 26-volt ac bus, and the 115-volt ac main bus No. 2 circuit breakers
(refer to Figure 14).
- CBP-D i s located in the flight compartment on the copilot's right console and
contains the 28-volt dc essential bus and the 28-volt dc power control
circuit breakers (refer to Figure 15).
- CBP-E i s located in the aft electrical distribution box in the battery
compartment and contains the battery direct bus and the battery bus circuit
breakers (refer to Figure 16).
SECTION 7
Page 4
Apr 02/87
canacaatr
ctiatienaer
OPERATING MANUAL
PSP 601A-6
LEGEND
- AUXILIARY SYSTEM
> MAIN AC SYSTEM
»EMERGENCY AC SYSTEM
EXTERNAL AC
CONNECTION
ADG
AOG
CONTROL
UNIT
AC ESSENTIAL
BUS CBP-C
AC Generation Systems - Layout
Figure 1
SECTION 7
Page 5
Apr 02/87
OPERATING MANUAL
PSP 601A-6
LEGEND
• BATT AND EXT PWR
•AC
STATIC CONVERSION DC
AUXILIARY BATTERY
EFFECT1V1TY:A/C5001 TO 5134
IRS 2 BATTERY
EFFECnVTTY: AJC 5135 AND SUBS AND
A/C POST SB 601-0418
BATTSIY BUSRIGHT
CBP-B
DC ESSENTIAL
BUS CBP-D
TRANSFORMER
RECTIFIER UNITS
DC Generation Systems - Layout
Figure 2
SECTION 7
Page 6
Apr 10/95
OPERATING MANUAL
PSP601A-6
C DC8UST )
Electrical Power Generation and Distribution
System - Basic Configuration
Figure 3
SECTION 7
Page 7/8
Apr 02/87
ctianentjer
OPERATING MANUAL
PSP 601A-6
GEN 1
GEN "5 AND GEN 2 KVA LOAD METERS
indexes the kVA io3fl on the associated
gervrattv
GEN OFF LIGHT
Amber GEN Qfr u$r>z comes or. when the generator
ts off line tor any of the following reasons:
- Generator treouenry out of tolerance
- Generator voJt3ge out of tolerance
- No output from the generator.
OVLD LIGHT
if tne generator output current exceeds 100 A
for m c e than 2 seconds, the overload
monrtonng circuit m The GCU operates and
the amber OVLD light comes on.
ON-OFF 'RESET - TEST SWITCH
Three-position generator control switch with the following
functions:
ON - supplies primary power to ac busses
OFF - removes primary power f r om the ac busses
RESET - respects generator after a fault
TEST - checks voltage and freouency of the generator off-load.
GlK
MAIN
BUS 1
OFF
T>
AUTO
OFF
FAIL r ^
MAIN BUS 1 OFF UGHT
Amber MAIN BUS 1 OFF light
comes on when main bus No. 1
is not connected to any generator.
AUTO OFF SWITCH LIGHTS
When pressed the automatic bus tie operation »s
disabled ano the associated amber AUTO OFF light
comes on.
FAIL LIGHTS
Associated amber FAIL light comes on if a bus tie
overcurrent or generator overcurrent condition exists.
MAIN
BUS 2
OFF
Z MAIN BUS 2 OFF LIGHT
Amber MAIN BUS 2 OFF light
comes on when main bus No. 2
is not connected to any generator.
CENTRE PEDESTAL
Primary AC Power Control SECTION7
Figure 4 Page 9
Apr 02/87
OPERATING MANUAL
PSP 601A-6
nSM TOOtCftATE
APU KVA LOAD METER
Inoicates the kVA load on the APU generator
ON-OFF/RESET - TEST SWITCH
Three-position generator control switch with the
following functions:
ON - suppfies power to ac busses.
OFF - removes auadiary power from the ac busses.
RESET - reseJeets generator after a fault.
TEST - checks voltage and frequency of the
generator off-load.
GEN OFF LIGHT
Amber GEN OFF light comes on when the generator
is off line for any of the following reasons:
- Generator frequency out of tolerance.
- Generator voltage out of tolerance.
- No output from the generator.
If the APU is shut down, the APU GEN OFF light
goes out.
BUS! BUS 2
OVLD LIGHT
If the generator output current exceeds 100 A
for more than 2 seconds, the overload
monitoring circuit in the GCU operates and
the amber OVLD light comes on.
CENTRE PEDESTAL
Auxiliary AC Power Control SECTION7
F i9"re 5 Page 10
Apr 02/87
"chaueiicrer
OPERATING MANUAL
PSP 601A-6
MAIN BUS 2 OFF LIGHT
Amber MAIN BUS 2 OFF light
comes on if the power is lost from
the main dc bus No. 2 due to failure
of TRU 2 or ac bus No. 2. Power is
supplied from main dc bus No. 1
when both BUS TIE CLOSED
switch/lights are pressed.
MAIN BUS 1 OFF LIGHT
Amber MAIN BUS 1 OFF light
comes on if power is lost from the
main dc bus No. 1 due to failure of
TRU 1 or ac bus No. 1. Power is
supplied from main dc bus No. 2
when both BUS TIE CLOSED
switch/lights are pressed.
ESS TRUS 1 OFF LIGHT
Amber essential TRUS 1 OFF light
comes on rf power is lost from ESS
TRU 1 or ac essential bus. In that
case, power is supplied to the dc
essentia] bus from the ESS TRU 2 or
in emergency condition, by
deploying the ADG.
_ _ _ DC POWER
I TRU 1 I ^ t TR U 2 1 T
BUS TIE CLOSED SWITCH/LIGHT
When both the left and right BUS
TIE CLOSED switch/lights are
pressed, the dc bus No. 1 and dc
bus No. 2 are interconnected and dc
utility bus No. 1 and dc utility bus
No. 2 are disconnected.
ESS TRUS 2 OFF LIGHT
Amber essential TRUS 2 OFF light
comes on if power is lost from ESS
TRU 2 or ac main bus 2. in that
case, power is supplied to the dc
essential bus from the ESS TRU 1 or
in emergency condition, by
deploying the ADG.
BATT BUS OFF LIGHT
Amber BATT BUS OFF light comes
on if power is lost from the battery
bus due to an ESS TRU 1 and ESS
TRU 2 failure. Power is restored to
the battery bus by deploying the
ADG or by switching on the
BATTERY MASTER switch.
ESS BUS OFF LIGHT
Amber ESS BUS OFF light comes
on if power is lost from the dc
essential bus due to the failure of
ESS TRU 1 and ESS TRU 2. In that
case, power is restored to the dc
essential bus by deploying the ADG.
CENTRE PEDESTAL
Main DC Power Control SECTION7
Figure 6 Page 11
Apr 02/87
OPERATING MANUAL
PSP 601A-6
FAIL LIGHT
Amber FAIL light comes on when the ac
essential voltage is less than 90 volts on
any phase.
ALTN SWITCH/LIGHT
When pressed, green ALTN fight comes on
and the ac essential bus transfers from ac bus
No. 1 to ac bus No. 2- The light comes on
automatically if access to ac bus No. 1 is lost.
CENTRE INSTRUMENT PANEL
AOG LAMP - UNIT TEST SWITCH
Two-position switch checks the following:
UNIT - Continuity of the uplock squib
circuit
- Continuity of the three transfer
contactors.
- Logic circuits
LAMP - TEST fight
- Weight-on-wheeis circuit.
ADG AUTO DEPLOY TEST LIGHT
Green fight comes on when the tests performed
with the LAMP-UNIT test switch in the UNIT
position are correct. On the ground, the fight
comes on immediately for 2 seconds. In the air,
the light comes on after a delay of 5 seconds
and remains on for 2 seconds.
A.D.G. MANUAL DEPLOY
HANDLE
Martuafiy deploys the ADG
and energizes the throe
transfer contactors.
^ ^ i ADG PWR TXFR OVERRIDE SWITCH
When pressed, de-energizes the ac emergency,
dc emergency and 38 hydraulic contactors if
power has been restored to the main ac bus.
CENTRE PEDESTAL
Essential AC Power and ADG Control SECTION7
^gure 7 Page 12
Apr 02/87
cfta/zenaer
OPERATING MANUAL
PSP 601A-6
ELECT PWR AVAIL LIGHT
When external power is connected to the aircraft, the
external power monitor checks for:
- Correct phase sequence.
- Voltage between 106 and 124 volts ac.
• Frequency between 370 and 430 Hz.
The green AVAIL light comes on if these parameters are met.
ELECT PWR IN USE LIGHT
When the G PWR switch is on and neither the APU nor any
generator is on line, the external contactor energizes. The
green AVAIL light goes out and the amber IN USE light
comes on. The IN USE light also comes on when external dc
power is connected.
CHARGER LIGHT
The amber CHARGER light comes on if any of
the following conditions exist:
- Battery charger fail.
- Overtemperature of battery.
- Loss of ESS TRU 1 and ESS TRU 2 feed
to battery bus.
- Charger circuit breaker tripped.
- AOG deployed.
ELECWPWR
G PWR CONTROL SWITCH
Ground power control switch energizes tne
external power contacts of the AP/EPC
f (auxiliary power/external power contactor*
and if no other generator is on line,
the ground power supplies the busses
BATTERY LIGHT
Amber BATTERY light comes on if any of the
following conditions exist:
-BATTERY MASTER switch se: to off.
— Loss of power to the battery direct bus.
— Faulty battery direct sensing relay.
— 8attery control circuit breaker tnpped.
BATTERY MASTER SWITCH
ON - Connects the battery to the battery bus
when no external power is connected.
The battery is automatically connected to the
battery bus if ESS TRU 1 and ESS TRU 2 fail.
OVERHEAD PANEL
External Power and Battery Control SECTION 7
Figure 8 page 13
Apr 02/87
OPERATING MANUAL
PSP 601A-6
DC METERING
Monitors TRU loads and bus
voltages.
AC METERING
Monitors ac voltages
and frequency.
AC SELECTOR SWITCH
Used to select power source to be
monitored.
CENTRE PEDESTAL
AC and DC Metering SECTION7
Figure 9 Page 14
Apr 02/87
cacnhsacJjiseirri Qer
OPERATING MANUAL
PSP 601A-6
EFFECTIVITY
H A/C POST SB 601 -262 AND
5135 AND SUBS
g ] A/C 5001 TO 5134
[§] A/C 5041 AND 5146
0 ] A/C POST SB 601 -0396 AND
5135 AND SUBS
g ] A/C POST SB 601-0262 REV.2 AND REV.3
A/C POST SB 601-0355 AND
5135 AND SUBS
AR
Lyi
110
S3
CONF
WARN1
©
80
H
CBP-A
2
5s|
5 3 14_
FLAP
MOTOR
- 1 1 5 V AC BU8 1 -
W
FAN
115] 1201
31 32
[3J
33 34 35
f3JJ
36 37 38 39 40 41 42 43 45
GALLEY
8UPPLY
1
115V AC UTILITY BU8 1
ADO
115VACBU8 1
I L/T LT8 1
CKPT ' L L ' LTS
FAN NOSE WING NAV
PA88
WARN
SIGNS
ENQ
VIB
MON
0©OOOOOQ
46 47 48 49 50 51 52 53 54 55
^5J
56 57 58 59 60
28V DC UTILITY BUS
FEED
28VDCBU8 1 —
UTIL BATT PWR 10 ST
BUS RCCB 8ENS B/AIR
WOW
CHAN
1
TTM
61 62 63 64
^50|
65 66
©
67
© @ © ® ® ©
70 71 72 73 74 75
FLAP LD QR NOSE
C O N -
1
QND CO~NT CONT DOOR CONF
SPIR i ion —
28VDC BU8 1
A N T I 8 K I D — | PA88 f
NT WARN INBD OUTBD SIGNS STEER
WARN NOSE NAV/C CDU DATA REAR WING
1 1 LOAD A/COLL IN8P
CKPT
FLOOR
76 77 78
yy
79 80 81
©
82 83 84 85
©©
86 87
yy
90
HYDSYST-i T/T GRAV m .
LENG IND AC PUMP TRANS ^ L '
PUMP 80V 1 CONT 2 CONT Qjy
28VDC BUS 1
- CKPT TEMP CONT , LAIR
LO ' COND
UM MAN AUTO CONT
14 8T A/ICE A/ICE AUX/TOT
B/AIR AUTO .SOL. FUEL SEL
80V L 1 VALVE QUANT CAL
HTR CONT
LEFT
WSHLD
®®©@®
100 101 102 103 104 105
AFCS
T/T BACK Y/D
IND UP PUMP RECEN l/H
y j \2) W \S) %2J
106 107 108 109 110
16 17 16
IRU
3
19
m
3
20
MFD
FAN
21
HTTR
22 23 24 25 26
INT LTS
27 28 29
LEFT 1 STATIC
WSHLD L
30
i
i_n_ru-i_r
Main AC No. 1 and DC No. 1 Circuit Breaker Panel
Figure 10
SECTION 7
Page 15
Aug 14/02
chauenqer
OPERATING MANUAL
PSP 601A-6
EFFECTIVITY
E3 A/C 5041 AND 5146
g] A/C 5067 AND 5087 AND SUBS
g] A/C POST SB 601 -0363
ffl A/C 5001 TO 5134
Ly yj iy ii
139 140 141 142 28V DC BATTERY BU8
— STALL PR0T-,, QEN CONT UNITS — , E8S AC , LIGHT8-
STICK LH XFR CTR
PUSH CHAN 1 2 3 CONT FLOOD DOME
WARN
LT TE8T
-MA8TER CAUTION-
8 CHAN 10 CHAN PILOT
ANN 1 ANN 1 LIGHTS
150 151
U71/2J H 7M
152 153
TO2J
154 155 156 157 158 159 160
f3J
161
28V DC BATTERY BU8
WOW I FUELSOV 1 L FUEL | ENQ IQN . L
CHAN ' R L ' PUMP ' FUEL
1 ENQ APU ENQ XFLOW CONT A B PUMP
-ENQ START-
_R L_
162 163 164 165 © ® ® ® © 166 167 168 169 170 171 172 173
FIRE DETECTORS
ENQ ENI APU TEST
28V DC BATTERY BUS
- 1 — FIRE EXT—2
ENILQ JEN.Q. JENLQ E±NQ BP FAULT
CONT ANN BATT
CJD C y CL) C y CEi) CE1 CE1I CE# IE#
174 175 176 177 178 179 180 181 182
xjn_jn_jn_TLj-i_n_n_r
1B3 184 185
Battery Bus - Left Circuit Breaker Panel SECTION 7
Figure.11 Page 16
Aug 14/02
cacnhaadnaeinr Qer
OPERATING MANUAL
PSP 601A-6
EFFECTIVITY
A/C POST SB 601-0262 AND
5135 AND SUBS
A/C POST SB 601-0396 AND
5135 AND SUBS
A/C 5041 AND 5146
T/0
CONF
WARN 2
113
[2]
CBP-B
15 14 13 12 10 5 2
TRU
E88
2
HYD
8YST
FAN
-116V AC BUS 2 -
116V AC
h% MOTOR
2
30 29 _28 27L 26 25 24 23 22 21 20 19 18 17 16
45 ©
44 43
|20j
42 §©0@0080080
41 40 39 38 37 36 35 34 33 32 31
115VACBU8 2
L/TLT8 1 ICE ADO
R R DET DEPLOY
WINQ NQ8E 2 SENS
115V AC UTILITY BUS 2 -
GALLEY
SUPPLY
2
60 59 58 57
I5J
56 55 54 53 52 51 50 49 48
|5J
47 46
wow
CH2
10 ST
B/AIR PWR
SOV R SENS
28VDCBUS2-
ICE UTIJL
DET BUS
2 CO)NNTT UTIL
28V DC UTILITY BU8 2
FEED JIT TRANS T/T FUEL FEED
CONT TRANS PUMP
IRU
BATT
2
HFCOMM2
CONT • TX/RX-
© © © © © © © @
75 74 73 72 71 70 69 68 _67^/i6_
; &
©
64 63 62 61
PRE88 ' CDU NAV/C ' M/C C/PLT
IND 2 2 PWRF -3 •M"A-P A/COLL
2BVDC BU8 2 -
1 CLOCK R RFUEL FLT
WINQ 1 FUEL P-;UgMN_P CONT
PUMP CONT MON OUTBD INBP
NOSE
STEER
CONT QND
90
f3j
88 87 86
© © © © © © © © © ©
85 84 83 82 81 80 79 78 77 76
HTR CONT ,
R R ADF
W8HLD WINDOW 2
AUTO
2 80V R
28VDC BUS 2
RAIR r—CABIN TEMP CONT ir
COND ' '~ "
CONT AUTO I i\S AC PUMP IND PUMP RENO FAN
CONT 1 2 CONT 3A PUMP 80V CONT
CP CP CP © © CP CP © CP CP CP CP CP © ©
105 104 103 102 101 100 99 98 97 96 95 94 93 92 91
VHF r -AFC8-
ADC NAV FQC Y/D ACT SERVO
2 2 2 2 2
CONT
2
28V DC BU8 2
I AURAL HYD SOV VHF I EFIS 2
WARN O/RIDE WXR ATT DME COMM DSPLY EHSI EADI
8 R/H REVRLY 2 2 CONT
SQ
Q Q Q © ^
120 119 118 117 116 mrtra
$J i£J ^3 <HJ i5J iSJ C5J
112 111 110 109 108 107 106
STATIC
R
HEATERS
PITOT AOA
R R
, RIGHT—
1 WSHLD
- , 26V AC 1 XFMR
— 116V AC BUS 2
CABIN
FAN CHAN1
BATT
OHQR
Main AC No. 2 and DC No. 2 Circuit Breaker Panel SECTION 7
Figure 12 page 17
Aug 14/02
canadair
chanenqer
OPERATING MANUAL
PSP 601A-6
EFFECTIVITY
E3 A/C POST SB 601-0262 AND 5135 AND SUBS
g] A/C POST SB 601-0225, 5001 AND 5027 AND SUBS
A/C 5041 AND 5146
A/C POST SB 601-0359 AND 5100 AND SUBS
A/C 5001 TO 5134
A/C POST SB 601-0394
FDR A/P A/P EFIS2
V0LTAQE SYNCH SYNC ADC RMT
CQNT Y5L
SURF
M/ASI Ail PP9B
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139 149 \ 148 147
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