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C-141C Dash 1 Section 1, Pages 401-450
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TO 1C-141C-1
DIGITAL FUEL QUANTITY INDICATOR
\ ^ > '
V ^ j
TANK IDM1 = MAIN #1M2 = MAIN #2M3 = MAIN #3M4 = MAIN #4A1 =AUX#1A2=AUX#2A3 = AUX #3A4 = AUX#4E1 = EXTENDED RANGE LHE2 = EXTENDED RANGE RH
MAIN NUMERICDISPLAY
ERROR CODE DIGIT(FOR TOTALIZER ONLY)
ERROR INDICATION
FUEL QUANTITY DATA TABLE
TANK CAPACITIES
USABLE FUEL FULLY SERVICED
GALLONS POUNDS GALLONS POUNDS
NO. 1 OR NO. 4 MAINNO. 2 OR NO. 3 MAINNO. 1 OR NO. 4 AUXNO. 2 OR NO. 3 AUXLH OR RH EXT RANGEPLUMBING (EACH SIDE)TOTAL (EACH WING)TOTAL (BOTH WINGS)
1.2332,1692.5701.6964,128
11,79623,592
8,01414,10016.70411,02226,836
76,676153,352
1,2652,1782,5721,7014,140
3211,88823.776
8,22114,15916,71611,05626,915
20877,275
154,550
THE TABLE IS BASED ON:1. JP-4 FUEL AT 6.5 LB/GAL (ICAO STANDARD DAY CONDITIONS).2. MEASURED DATA.
Figure 1-170. Fuel Quantity Data Table
1-413
TO 1C-141C-1
FUEL SUPPLY SYSTEM
TOENGINENO. 2 ■ ^ j
(TYPICALFORNO. 4 AUX)
JETTISONSWITCH
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REFUELJETTISON SWITCHMAST
REFUELSWITCH
FUEL SUPPLY
REFUELSWITCH
REFUELSWITCH
REFUEL SWITCH
BOOST PUMP
^ ^ J E T T I S O N L I N E
nmmm
\\^# CHECK VALVESINGLE POINTFUELING LINES
AERIAL REFUELINGLINES
AERIAL REFUELINGDRAIN LINE
\fWx THERMAL RELIEF VALVE
|X| REFUEL VALVE
i f1=o
PRESSURE SWITCH
FUEL QUANTITYINDICATOR PROBE
SHUTOFF VALVE
MECHANICAL ACTUATION
ELECTRICAL ACTUATION
-3<1
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MOTOR OPERATEDSHUTOFF VALVE
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AERIAL REFUELING RECEPTACLE' ■ ^ J
SINGLE POINTREFUELING RECEPTICAL
—H JET PUMP~1 I EJECTOR
141B-XCVCV023-I
Figure 1-171. (Sheet I of 2)
1-414
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AERIAL REFUELING SYSTEMSLIPWAY DOOROPEN SWITCH
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At?*-1RH AERIAL REFUELISOLATION VALVE
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aGN-FUEL DRAINPUMP & VALVES
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^ Sa/r ;OFF
o - *
J
L _sf 5.JFUEL LINEDRAIN SWITCH
TO NO. 3MAIN TANK
S J
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Figure 1-172. Aerial Refueling System (Sheet I of 2)
1-416
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T01C-141C-1
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1-420
TO 1C-141C-1
FLIGHT ENGINEER'SELECTRICAL PANEL
(CSOOVERHT
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Y
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\ \NO. 1 CSD
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M A I N D C | I M A I N O C_BUSJ£U_I 1 .fillS NO, 2.I o f f I n n l o f f I
ISOL DC BUSBATTERY
IW"-H-!d
EMER DC BUS
■ ' J ( B U S P W R D I S C O N N E C T JF f J U U N A C B U S U A J N A C B U S E S S E N S O L C
EXT POWERUAMACBUS UAMACBUS
.NORM /S& NORMAL
/ N O ! I J N O . I 4 4 B U S E S B U S E S /
Figure 1-176. Flight Engineer's Electrical Panel
1-421
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1-424
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COMPONENTCIRCUIT BREAKER
POWER SOURCEDESIGNATION LOCATIONAILERONSAILERON POWER CONTROL SWITCHES:
LEFT LH AILERON SYSTEM NO. 1LH AILERON SYSTEM NO. 2
39-R43-R
MAIN DC BUS 1MAIN DC BUS 2
RIGHT RH AILERON SYSTEM NO. 1RH AILERON SYSTEM NO. 2
39-R44-R
MAIN DC BUS 1MAIN DC BUS 2
POWER OFF LIGHTS LH AILERON INDRH AILERON IND
43-R44-R
MAIN DC BUS 1MAIN DC BUS 2
SYSTEM POWER ANNUNCIATOR LIGHTS
TAB OPERABLE:
WARN LT TEST & ANNUN CONT NO. 1WARN LT TEST & ANNUN CONT NO. 2
26-R27-R
ISOLATED DC BUSISOLATED DC BUS
LEFTRIGHT
AILERON TAB ACTRLHAILERON TAB ACTRRH
31-R31-R
ISOLATED DC BUSISOLATED DC BUS
TAB OPERABLE ANNUNCIATION WARN LT TEST & ANNUN CONT NO. 1WARN LT TEST & ANNUN CONT NO. 2
26-R27-R
ISOLATED DC BUSISOLATED DC BUS
TRIM AILERON TRIM CONT 13-R ESSENTIAL AC BUS 1
TRIM INDICATOR AILERON TRIM POS IND 38-R MAIN DC BUS 1ANTI-ICING/DE-ICING
NO. 1 SYSTEM-PILOT PLT ANGLE OF ATTACK VANE HTR PWR 17-R ESSENTIAL AC BUS 1NO. 2 SYSTEM ■ COPILOT COPLT ANGLE OF ATTACK VANE HTR
PWR22-R ESSENTIAL AC BUS 2
HTR FAULTED LIGHT PITOT EPR & ANGLE OF ATTACK (12-A) EMERGENCY DC BUS
CONTROL EMP DE-ICE CONT 42-R MAIN OC BUS 2INDICATOR LIGHTS EMP DE-ICE IND 42-R MAIN DC BUS 2POWER EMP DE-ICE PWR 4, S, 6-R MAIN AC BUS 2SYSTEM CONTROLLER EMP DE-ICE SYS
CONTROLLERMAIN AC BUS 2
ANTI-ICE ON LIGHTS ENG ANTI-ICE (NO. 1 & 4)ENG ANTI-ICE (NO. 2 & 3)
36-L41-L
MAIN DC BUS 1MAIN DC BUS 2
SWITCH & VALVES NAC ANTI-ICE & IND NO. 1 & 4NAC ANTI-ICE & IND NO. 2 & 3
3S-L40-L
MAIN DC BUS 1MAIN DC BUS 2
EPR HEAT CONTROL PITOT EPR & ANGLE OF ATTACK (12-A) EMERGENCY DC BUSEPR HEAT POWER EPR PROBE ANTI-ICE 15.16-R ESSENTIAL AC BUS 1
ICE DETECTION CONTROL SWITCH ENG AUTOMATIC ICE CONT 44-L MAIN DC BUS 2ICE DETECTION TEST SWITCH ICE DETECT 22-R ESSENTIAL AC BUS 2
ICING WARNING LIGHT ENG AUTOMATIC ICE CONT 44-L MAIN DC BUS 2
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| TOTAL TEMP PROBE DE-ICE NO. 2
16-R21-R
ESSENTIAL AC BUS 1ESSENTIAL AC BUS 2
Figure 1-182. Circuit Breaker Index (Sheet 1 of 31)
1-442
TO 1C-141C-1
COMPONENTCIRCUIT BREAKER POWER SOURCED E S I G N A T I O N | LOCATION
ANTMCING/DE-ICING (CONTINUED)
PILOT PLT PITOT STATIC HEATER HEADPLT PITOT STATIC HTR MASTPLT STATIC HTR HEADPLT STATIC HTR MAST
(3-C)15-R(3-A)22-R
EMERGENCY AC BUSESSENTIAL AC BUS 1EMERGENCY AC BUSESSENTIAL AC BUS 1
COPILOT COPLT PITOT STATIC HTR MAST & HEADCOPLT STATIC HTR HEAD & MAST
16-R21-R
ESSENTIAL AC BUS 1ESSENTIAL AC BUS 2
HEATER FAULTED LIGHTS PITOT EPR & ANGLE OF ATTACK (12-A) EMERGENCY DC BUS
PITOT HEAT ANNUNCIATOR WARN LT TEST & ANNUN CONT NO. 4 29-R ISOLATED DC BUS
INDICATIONS:LEFT ON & RIGHT ON LIGHTSL OVERHEAT & R OVERHEAT UGHTSWING ANTI-ICE OVERHEAT
ANNUNCIATOR LIGHT
WING ANTI-ICING INDWING ANTI-ICING OVHT WARN
WARN LT TEST & ANNUN CONT NO. 4
33-R33-R
29-R
ISOLATED DC BUSISOLATED DC BUS
ISOLATED DC BUSPOWER:
INNER-OUTBOARD POWERMID WING POWEROUTBOARD POWER
WING ANTI-ICE INNER OUTBD PWRWING ANTI-ICE MID PWRWING ANTI-ICING OUTBD PWR
42-R42-R36-R
MAIN DC BUS 2MAIN DC BUS 2MAIN DC BUS 1
AUTOMATIC FLIGHT CONTROLS SYSTEM (AFCS)AUTOPILOT/FLIGHT DIRECTOR
AUTOMATIC FLIGHTCONTROL PROCESSOR
AFCP NO. 1AFCP NO. 1AFCP NO. 2AFCP NO. 2AIL SERVO
(2-A)(6-A)23-D36-B11-D
EMER ACEMER DCAVIONICS AC 2MAIN DC AVIONICS 1MAIN DC AVIONICS 2
FLIGHT CONTROL PANEL/MODE SELECT PANEL
FCP/MSPNO.1FCP 2MSP NO. 2
(7-A)7-C35-B
EMER DCAC NAV EXCITATION 2MAIN DC AVIONICS 1
ELEVATOR SERVO ELEV SERVO 12-D MAIN DC AVIONICS 2
ELEVATOR SYNC ELEV POSN NO. 1ELEV POSN NO. 2
30-C8-B
AC NAV 1AC NAV 2
AUTOTHROTTLE SERVO A/T SERVOFCP 1/A/T SERVO
13-D43-D
MAIN DC AVIONICS 2ISOL 26V AC
AUTOPILOT/YAW DAMPER RUD SERVO NO. 1RUD SERVO NO. 2
10-B29-D
EMER DCMAIN DC AVIONICS 1
STALL WARNING AUDIO STALL WARNSTALL WRN NO. 1STALL WRN NO. 2
22-L37-D10-C
26V AC BUS 1ISOL AC EXCITATIONAC NAV EXCITATION 2
PILOTS STICK SHAKERCOPILOTS STICK SHAKER
STALL PREVENT NO. 1STALL WARN (OR PREVENT) NO. 2
35-R40-R
MAIN DC 1MAIN DC 2
AUXILIARY POWER UNITCONTROL CONTROL
CONTROLFUEL SHUTOFF VALVE
ACPDC930-L30-L
ISOLATED DC BUSISOLATED DC BUS
EGT APU EXHAUST GAS TEMP 20-R ESSENTIAL AC BUS 2FIRE EXTINGUISHER FIRE EXT 30-L ISOLATED DC BUSTEST AUX GENERATOR VOLT AND FREQ TEST ACPDC9WARNING LIGHTS APU FIRE DET CONT UNIT
APU GEN WARN LTDOOR WARN LTFIRE IND LT
11-L30-R30-L30-L
MAIN AC BUS 4ISOLATED DC BUSISOLATED DC BUSISOALTED DC BUS
Figure I-182. Circuit Breaker Index (Sheet 2 of 31)
1-443
T01C-141C-1
COMPONENTCIRCUIT BREAKER
POWER SOURCED E S I G N A T I O N | L O C A T I O NCARGO DOORS, RAMP & ADS
ADS ARMED SWITCHADS INDICATOR LIGHTS
DOOR OPEN LIGHT ANNUNCIATORAIR DEFLECTION DOORS CONTROL
AND INDICATIONANCHOR CABLE ACTUATOR ARMS:
LEFTRIGHT
ARMED INDICATORCHUTE RELEASE SWITCHSTATIC LINE RETRIEVER WINCH NO. 1:
CONTROLPOWER
STATIC LINE RETRIEVER WINCH NO. 2:CONTROLPOWER
PARATROOP PLATFORM UGHTSJUMP SIGNALS:
CONTROLPOWER
AIR DROP SYSTEM CONTDOOR WARN & INDWARN LT TEST & ANNUN CONT NO. 4TROOP SPOILER DOOR POS IND & CONT
STATIC LINE CABLE POS ACTR LHSTATIC LINE CABLE POS ACTR RHAIR DROP SYSTEM CONTAIR DROP SYSTEM CONT
STATIC UNE WINCH NO. 1 CONTSTATIC LINE WINCH NO. 1
STATIC LINE WINCH NO. 2 CONTSTATIC UNE WINCH NO. 2JUMP PLATFORM LTS
TROOP JUMP LTS CONTTROOP JUMP LTTROOP JUMP LT
43-R29-R29-R44-R
6-L9-L43-R43-R
35-R4,5.6-L
40-R7,8,9-L
43-R
39-RCFJBCFJB
MAIN DC BUS 2ISOLATED DC BUSISOUTEDOCBUSMAIN DC BUS 2
MAIN AC BUS 2MAIN AC BUS 3MAIN DC BUS 2MAIN DC BUS 2
MAIN DC BUS 1MAIN AC BUS 2
MAIN DC BUS 2MAIN AC BUS 3MAIN DC BUS 2
MAIN DC BUS 128V AC BUS9VACBUS
DOOR ARMING SWITCH:CONTROLPOWER
AIR DROP SYSTEM CONTCARGO DOOR CONTAIR DROP SYSTEM PWR
43-R45-R43-R
MAIN DC BUS 2MAIN DC BUS 2MAIN DC BUS 2
COMMUNICATIONS
EMERLOCRXMTR 39-B ISOLATED DC AVIONICS
HF-1
KY-75 ^L\KYV-5 A
HF1 ACS (KEEP ALIVE) /a\
HFNO. 1HF NO. 1
KY7S NO. 1
KYV-5 NO.1
HF1 ACS
21-B, C, D21-A
18-C
17-C
(14-A)
AC AVIONICS BUS 1MAIN DC AVIONICS 1
MAIN DC AVIONICS 2
MAIN DC AVIONICS 2
EMERGENCY DC BUS
_ ^J^
AA
AIRCRAFT MODIFIED BY TCTO 636
AIRCRAFT MODIFIED BY ICJD_55Q
A AIRCRAFT MODIFIED BY TCTO 769
J
Figure 1-182. Circuit Breaker Index (Sheet 3 of 31)
1-444
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TO 1C-141C-1
COMPONENTCIRCUIT BREAKER
POWER SOURCEDESIGNATION LOCATION
COMMUNICATIONS (CONTINUED)
AN/ARC-164 (V) UHF KY58 NO. 1KY-58 UHF NO. 2
19-B16-A
ISOL OC AVIONICSMAIN DC AVIONICS
VHF KY58 NO. 1KY-58 VHF NO. 2
18-B17-A
ISOL DC AVIONICSMAIN DC AVIONICS 2
DEFENSIVE SYSTEMS (DS)MISSILE WARNING SET (AN/AAR-47) AAR-47 SYS 25-R MAIN DC BUS 1COUNTERMEASURES DISPENSING
SYSTEM (AN/ALE-47):COCKPIT CONTROL UNIT ALE-47 CCU
ALE-47 IND PWRALE-47 LOGIC
24-R24-R24-R
MAIN DC BUS 1MAIN DC BUS 1MAIN DC BUS 1
FLARE SEQUENCE & DISPENSE EMIFILTERS:
FORWARD FUSELAGE FWD FSLG SQCR 25-R MAIN DC BUS 1LT GEAR POD LH MLG SQCR 25-R MAIN DC BUS 1LTWING LH WING SQCR 24-R MAIN DC BUS 1RT GEAR POD RH MLG SQCR 25-R MAIN DC BUS 1RTWING RH WING SQCR 24-R MAIN DC BUS 1 ^ )
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JFigure 1-182. Circuit Breaker Index (Sheet 5 of 31)
1-446
TO 1 C-141 C-1
CIRCUIT BREAKERCOMPONENT POWER SOURCEDESIGNATION | LOCATIONELECTRICAL SYSTEMS (AC)
AUTO PAR CONT PH C ACPDC 12
MAIN AC BUS NO. 2 LOAD MONITOR RELAY MAIN BUS 2 MONITOR CONT 31-L ISOLATED DC BUSMAIN AC BUS NO. 3 LOAD MONITOR RELAY MAIN BUS 3 MONITOR CONT 32-L ISOLATED DC BUS
EMERGENCY AC BUS LIGHTS EMER POWER CONTROL (9-A) EMERGENCY DC BUSEMERGENCY POWER ON LIGHT EMER POWER CONTROL (9-A) EMERGENCY DC BUSESSENTIAL AC NO. 1 BUS LIGHTS
(CONTROL):OFF BUS OFF WARN 13.14,15-R ESSENTIAL AC BUS 1GEN 1 & GEN 2 ESS BUS POWER SOURCE IND LTS 37-L MAIN DC BUS 1
ESSENTIAL AC NO. 2 BUS LIGHTS(CONTROL):OFF BUS OFF WARN 18.19.20-R ESSENTIAL AC BUS 2GEN 3 & GEN 4 ESS BUS POWER SOURCE IND LTS 37-L MAIN DC BUS 1
ESSENTIAL AC BUS OFF LIGHTS (POWER) BUS WARN LTS 32-L ISOLATED DC BUSISOLATED AC BUS LIGHTS:
EMER PWR - ISOL AC BUS (CONTROL) EMERG POWER CONTROL (9-A) EMERGENCY DC BUSEMER PWR/ISOL AC BUS (POWER) ISOL DC BUS IND 31-L ISOLATED DC BUSISOL AC OFF (CONTROL) BUS OFF WARN 24-L&25-R ISOLATED AC BUSISOL AC OFF (POWER) ISO BUS OFF (8-A) EMERGENCY DC BUS
MAIN AC BUS OFF LIGHTS:NO. 1 CONTROL BUS OFF WARN 1,2,3-R MAIN AC BUS 1NO. 2 CONTROL BUS OFF WARN 4,5,6-R MAIN AC BUS 2NO. 3 CONTROL BUS OFF WARN 7.8, 9-R MAIN AC BUS 3NO. 4 CONTROL BUS OFF WARN 10,11,12-R MAIN AC BUS 4POWER BUS WARN LTS 32-L ISOLATED DC BUS
BUS TIE CONTACTORS:NO.1 GEN BUS TIE CONT NO. 1 26-R ISOLATED DC BUSNO. 2 GEN BUS TIE CONT NO. 2 27-R ISOLATED DC BUSNO. 3 GEN BUS TIE CONT NO. 3 28-R ISOLATED DC BUSNO. 4 GEN BUS TIE CONT NO. 4 29-R ISOLATED DC BUS
BUS TIE OPEN LIGHTS:NO. 1 & 4 GEN WARN LTS NO. 1&4 38-L MAIN DC BUS 1N0.2&3 GEN WARN LTS NO. 2 &3 44-L MAIN DC BUS 2
BUS TIE SWITCHES:NO.1 GEN BUS TIE CONT NO. 1 26-R ISOLATED DC BUSNO. 2 GEN BUS TIE CONT NO. 2 27-R ISOLATED DC BUSNO. 3 GEN BUS TIE CONT NO. 3 28-R ISOLATED DC BUSNO. 4 GEN BUS TIE CONT NO. 4 29-R ISOLATED DC BUS
BUS TIE SYNCHRONIZATION CONTROL SYNC BUS RELAY PWR 32-L ISOLATED DC BUS
CSD DISCONNECT SWITCHES:NO.1 CSD DISC & CSD OVHT IND NO. 1 36-L MAIN DC BUS 1NO. 2 CSD DISC & CSD OVHT IND NO. 2 41-L MAIN DC BUS 2NO. 3 CSD DISC & CSD OVHT IND NO. 3 41-L MAIN DC BUS 2NO. 4 CSD DISC & CSD OVHT IND NO. 4 36-L MAIN DC BUS 1
CSD OIL TEMPERATURE GAUGE:NO.1 CSD ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1NO. 2 CSD & ENG OIL TEMP IND NO. 2 40-L MAIN DC BUS 2NO. 3 CSD & ENG OIL TEMP IND NO. 3 40-L MAIN DC BUS 2NO. 4 CSD ENG OIL TEMP IND NO. 4 | 35-L MAIN DC BUS 1
Figure 1-182. Circuit Breaker Index (Sheet 6 of 31)
1-447
T01 C-141 C-1
CIRCUIT BREAKERCOMPONENT POWER SOURCE" « # " * j *■w * " n ^ # > ^ * » i ^ ■ D E S I G N A T I O N | LOCATION
ELECTRICAL SYSTEMS (AC) (CONTINUED)
CSD OVERHEAT LIGHT:NO.1 CSD DISC & CSD OVHT IND NO. 1 36-L MAIN DC BUS 1NO. 2 CSD DISC & CSD OVHT IND NO. 2 41-L MAIN DC BUS 2NO. 3 CSD DISC & CSD OVHT IND NO. 3 41-L MAIN DC BUS 2NO. 4 CSD DISC & CSD OVHT IND NO. 4 36-L MAIN DC BUS 1
DIFFERENTIAL FAULT RESET GEN DIFF PROT RESET 43-L MAIN DC BUS 2GENERATOR CONTROL:
NO.1 GEN NO. 1 CONT (PH A, B, C [3 C/Bs]) ACPDC12NO. 2 GEN NO. 2 CONT (PH A, B, C [3 C/Bs]) ACPDC11NO. 3 GEN NO. 3 CONT (PH A, B, C [3 C/Bs]) ACPDC 10NO. 4 GEN NO. 4 CONT (PH A. B, C [3 C/Bs]) ACPDC9APU GENERATOR AUX GENERATOR CONTROL (PH A, B. C
(3 C/Bs])ACPDC9
GENERATOR FAIL & GENERATOR OUTLIGHTS:NO.1 GEN WARN LTS NO.1 38-L MAIN DC BUS 1NO. 2 GEN WARN LTS NO. 2 44-L MAIN DC BUS 2NO. 3 GEN WARN LTS NO. 3 44-L MAIN DC BUS 2NO. 4 GEN WARN LTS NO. 4 38-L MAIN DC BUS 1APU APU GEN WARN LT 30-R ISOLATED DC BUS
GENERATOR LINE CONTACTORS:NO.1 GEN LINE CONTACTOR NO. 1 ACPDC4NO. 2 GEN LINE CONTACTOR NO. 2 ACPDC3NO. 3 GEN UNE CONTACTOR NO. 3 ACPDC2NO. 4 GEN LINE CONTACTOR NO. 4 ACPDC 1
GENERATOR SEQUENCING & LOADCONTROL:NO.1 GEN NO. 1 SEQ & LOAD CONT ACPDC4 ISOLATED AC BUSNO. 2 GEN NO. 2 SEQ & LOAD CONT ACPDC3 ISOLATED AC BUSNO. 3 GEN NO. 3 SEQ & LOAD CONT ACPDC2 ISOLATED AC BUSNO. 4 TIE BUS SEQ & NO. 4 LOAD CONT ACPOC12 ISOLATED AC BUS
AVIONICS AC BUS:POWER FEEDER NO. 1 AVIONICS BUS NO.1 ACPDC12POWER FEEDER NO. 2 AVIONICS BUS NO. 2 ACPDC 9TEST RECEPTACLE AVIONICS TEST RECP MISC 10-L MAIN AC BUS 4
EMERGENCY AC BUS POWER FEEDER EMER AC BUS PWR FEEO 13.14,15-R ESSENTIAL AC BUS 1ESSENTIAL AC BUS NO. 1:
POWER DELIVERY POWER FEEO PHASE POWER DELIVERYNO. 1(3 C/Bs)
ACPDC7
POWER FEEO MULTI-FEED ESS BUS NO. 1 (PH A, B. C)(9C/BS)
ACPDC12
POWER FEED POWER FEED (A, B. C) ESS BUS NO. 1(3 C/Bs)
ACPDC7
STANDBY POWER FEED NO. 1 ESS BUS NO. 1 STANDBY PWR FEEDNO. 1(PHA,B,C)(3C/Bs)
ACPDC 4
STANDBY POWER FEED NO. 2 ESS BUS NO. 1 STANDBY PWR FEEDN0.2(PHA.B,C)(3C/BS)
ACPDC 3
ESSENTIAL AC BUS NO. 2:POWER FEEDERS (PH A, B, C) MULTI-FEED ESS BUS
NO. 2 (9 C/Bs)ACPDC 9
POWER FEEDERS POWER FEED (PHASE A, B, C) ESS BUSNO. 2 (3 C/BS)
ACPDC 6
STANDBY POWER FEEDERS NO. 1 ESS BUS NO. 2 STANDBY PWR FEEDN0.1.(PHA.B,C[3C/Bs])
ACPDC1
STANDBY POWER FEEDERS NO. 2 ESS BUS NO. 2 STANDBY PWR FEEDN0.2(PHA,B,C[3C/Bsl)
ACPDC2
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S J
Figure 1-182. Circuit Breaker Index (Sheet 7 of 31)
1-448
TO 1 C-141 C-1
I C I R C U I T B R E A K E RCOMPONENT POWER SOURCE| D E S I G N A T I O N LOCATION
ELECTRICAL SYSTEMS (AC) (CONTINUED)
ESSENTIAL AC POWER FEEDERS NO. 1 ESS PWR FEED NO. 1 (PHASE A, B, C [9C/Bs])
ESS PWR FEED NO. 2 (PHASE A. B. C 19C/Bs])
EXTERNAL POWER CONTROL (PHASE A.
13,14,15-R ESSENTIAL AC BUS 1
ESSENTIAL AC POWER FEEDERS NO. 2 18,19, 20-R ESSENTIAL AC BUS 2
EXTERNAL AC POWER CONTROL ACPDC 9 EXTERNAL ACB,C[3C/Bs]) POWER
EXTERNAL DC POWER CONTROL EXTERNAL POWER CONTROL DC ACPDC 9 EXT (EXT AC PWR CONEXTERNAL POWER EXT POWER CONTROL PWR RECPT. VERTED BY PHASESEQUENCE RELAY)
ISOLATED AC BUS POWER FEEDERS ISOLATED BUS (PH A. B, C (3 C/Bs]) ACPDC 12MAIN AC BUS NO. 1 POWER FEEDERS MAIN AC BUS NO. 1 POWER FEED (PHASE
A, B. C (3 C/Bs])ACPDC 8
MAIN AC BUS NO. 2 POWER FEEDERS MAIN AC BUS NO. 2 POWER FEED (PHASEA,B,C[3C/Bs])
ACPDC3
MAIN AC BUS NO. 3 POWER FEEDERS MAIN AC BUS NO. 3 POWER FEED (PHASEA.B,C[3C/Bs])
ACPDC 2
MAIN AC BUS NO. 4 POWER FEEDERS MAIN AC BUS NO. 4 POWER FEED (PHASEA,B,C[3C/Bs])
ACPDC 5
NAVIGATION AC BUS NO. 1 BUS POWER NAV 1 27-D AC AVIONICS BUS 1NAVIGATION AC BUS NO. 2 BUS POWER NAV 2 26-D AC AVIONICS BUS 1NAVIGATION AC BUS NO. 2 STANDBY NAVBUS2STDBYPWR 17-B AC AVIONICS BUS 2
POWER26V AC NAVIGATION BUS 1 INST TRANS NO. 1 25-D AC AVIONICS BUS 126V AC NAVIGATION BUS 2 INST TRANS NO. 2 1-B AC AVIONICS BUS 228V AC & 9V AC LIGHTING BUS 1 LGT XMFR & CAR COMPT WHT LTS 1-R MAIN AC BUS 128V AC & 9V AC LIGHTING BUS 2 CARGO COMPT DOME LT 12-R MAIN AC BUS 4
COPILOTS FRONT WINDSHIELD (52V AC) COPLT WSHLD HTR PWR 12-R MAIN AC BUS 4COPILOT SIDE WINDSHIELD HEATER (52V
AC)DC POWER SUPPLY NO. 1, TRANSFORMER
COPLT SIDE WSHLD HTR PWR 5-L MAIN AC BUS 2
POWER FEED NO. 1 TRANS-RECTIFIER ACPDC 12 ESSENTIAL AC BUS 1RECTIFIER NO. 1
DC POWER SUPPLY NO. 2, TRANSFORMER POWER FEED NO. 2 TRANS-RECT ACPOC 9 ESSENTIAL AC BUS 2RECTIFIER NO. 2
26V AC EMERGENCY INSTRUMENTS 26 VAC EMERG INST TRANS (6-B) EMERGENCY AC BUSP H BEMERGENCY AC BUSP H AMAIN AC BUS 2
26V AC T24 (26V AC) AHRS ATT/2 RSP 1 & 2 EXC (4-A)
FLIGHT STATION LIGHTING 28V AC XMFR FLT STA LTG TRANS 4-LFORMATION LIGHTS 6V AC XMFR FORMATION LT 2-L MAIN AC BUS 1INSTRUMENT INDEX 26V AC XMFR INST INDEX TRANS 34-D NAVIGATION AC 1MISCELLANEOUS LTG 9 & 28V AC XMFR NO.
1LTG TRANS & CAR COMPT WHT LTS 1-R MAIN AC BUS 1
MISCELLANEOUS LTG 9 & 28V AC XMFR NO.2
CARGO COMPT DOME LT 12-R MAIN AC BUS 4
NAV INSTRUMENT 26V AC XMFR NO. 1 INST TRANS NO. 1 25-D AC AVIONICS BUS 1NAV INSTRUMENT 26V AC XMFR NO. 2 INST TRANS NO. 2 1-B AC AVIONICS BUS 2NAV INSTRUMENT 26V AC XMFR NO. 3 INSTRTRANSNO.3 39-C ISOLATED AC AVION
ICSMAIN AC BUS 1PILOTS FRONT WINDSHIELD HEAT (52V AC) PLT WSHLD HTR PWR 1-L
PILOTS SIDE WINDSHIELD HEAT (52V AC) PLT SIDE WSHLD HTR PWR 4-L MAIN AC BUS 2PILOTS CENTER WINDSHIELD HEAT (52V
AC)26V AC BUS NO. 1 ENGINE INST TRANS
CENTER WSHLD HTR PWR 11-L MAIN AC BUS 4
26V BUS NO. 1 TRANS 16-L ESSENTIAL AC BUS 126V AC BUS NO. 2 ENGINE INST TRANS 26V BUS NO. 2 TRANS 21-L ESSENTIAL AC BUS 2
Figure 1-182. Circuit Breaker Index (Sheet 8 of 31)
1-449
T01C-141C-1CIRCUIT BREAKER
COMPONENT POWER SOURCED E S I G N A T I O N | LOCATIONEL-ECTRICAL SYSTEMS (AC) (CONTINUED
GENERATOR NO. 1 GEN NO. 1 VOLT AND FREQ TEST (3 C/B) ACPDC 12NO. 2 GEN NO. 2 VOLT & FREQ TEST (PH A, B, C
[3 C/Bs])ACPDC 11
NO. 3 GEN NO. 3 VOLT & FREQ TEST (PH A. B, C[3 C/Bs))
ACPDC10
NO. 4 GEN NO.4 VOLT AND FREQTEST (PH A. B,C [3 C/Bs])
ACPDC9
APU GENERATOR AUX GEN VOLT AND FREQ TEST (3 C/Bs) ACPDC 9EXTERNAL POWER EXTERNAL POWER VOLT AND FREQ
TEST(PHA.B.C[3C/BS])ACPDC 9
EMERGENCY POWER AC VOLTAGE TEST EMERGENCYGEN. CONTROL
BOXELECTRICAL SYSTEMS (DC)
FEEDER BAT FEED 34-R MAIN DC BUS 1POWER BATTERY POWER BATTERY BOX BATTERY
BATTERY BUS WARN LTS 32-L ISOLATED DC BUSEMER DC BUS LIGHTS:
EMER PWR LIGHT DC EMER GENCONT
EMERGENCY GEN
EMER DC BUS LIGHT DC EMERGENCONT
EMERGENCY GEN
ISOL DC BUS LIGHTS:EMER PWR LIGHT (CONTROL) ISO DC BUS IND 31-L ISOLATED DC BUSEMER PWR UGHT (POWER) ISO DC BUS IND 31-L ISOLATED DC BUSISOL DC BUS LIGHT (CONTROL) BUS WARN LTS 32-L ISOLATED DC BUSISOL DC BUS LIGHT (POWER) BUS WARN LTS 32-L ISOLATED DC BUSISOLATED DC OFF LIGHT (POWER) ISO BUS OFF (8-A) EMERGENCY DC BUS
MAIN DC BUS LIGHTS:MAIN BUS NO. 1 OFF LIGHT (CONTROL) BUS OFF WARN 34-R MAIN DC BUS 1MAIN BUS NO. 2 OFF LIGHT (CONTROL) BUS OFF WARN 34-L MAIN DC BUS 2MAIN DC NO. 1 & NO. 2 OFF LIGHT POWER BUS WARN LTS 32-L ISOLATED DC BUS
DC POWER SUPPLY NO. 1. TRANSFORMER POWER FEED NO. 1 TRANS-RECTIFIER ACPDC12 ESSENTIAL AC BUS 1RECTIFIER NO. 1
DC POWER SUPPLY NO. 2, TRANSFORMER POWER FEED NO. 2 TRANS-RECT ACPDC9 ESSENTIAL AC BUS 2RECTIFIER NO. 2
EXTERNAL POWER CONTROL EXTERNAL POWER CONTROL DC ACPDC 9 (EXT AC PWR CONEXTERNAL POWER EXT POWER CONTROL EXT PWR VERTED BY PHASE
RECPT. SEQUENCE RELAY)
AEROMEDICAL EQUIPMENTFORWARD ^ AEROMED EQUIP FWD 34-L MAIN DC NO. 2 FEED
ER BUSAFT ,A AEROMED EQUIP AFT 34-R MAIN DC NO. 1 FEED
ER BUSEMERGENCY DC BUS POWER FEEDER EMERG DC PWR FEEDER 30-L MAIN DC NO. 1 FEED
ER BUS/BATTERYISOLATED DC BUS:
POWER FEEDER NO. 1 ISOL DC PWR FEEDER NO. 1 26-L MAIN DC NO. 1 FEEDER BUS/BATTERY
POWER FEEDER NO. 2 ISOL DC PWR FEEDER NO. 2 27-L MAIN DC NO. 1 FEEDER BUS/BATTERY
A LABELED 'IRON LUNG FWD" ON AIRCRAFT 12778•—* THRU 38090. A LABELED 'IRON LUNG AFT ON AIRCRAFT 12778
•^ THRU 38090.
Figure 1-182. Circuit Breaker Index (Sheet 9 of 31)
1-450