C-141C Dash 1 011 1- 451-500

TO 1C-141C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCEDESIGNATION LOCATION

ELECTRICAL SYSTEMS (DC) (CONTINUED)

POWER FEEDER NO. 3 ISOL DC PWR FEEDER NO. 3 28-L """ MAIN DC NO. 1 FEEDER BUS/BATTERY

POWER FEEDER NO. 4 ISOL DC PWR FEEDER NO. 4 29-L MAIN DC NO. 1 FEEDER BUS/BATTERY

ISOLATED DC AVIONICS BUS ISO NAV BUS DC PWR 34-L MAIN DC NO. 1 FEEDER BUS/BATTERY

MAIN DC NO. 1 FEEDER BUS TRANSFORMERRECEIVER NO. 1

MAIN DC BUS NO. 1POWER FEEDER NO. 1 FEEDER NO. 1 34-R MAIN DC NO. 1 FEED

ER BUSPOWER FEEDER NO. 2 FEEDER NO. 2 34-R MAIN DC NO. 1 FEED

ER BUSMAIN DC NO. 2 FEEDER BUS TRANSFORMER

RECEIVER NO. 2MAIN DC BUS NO. 2

POWER FEEDER NO. 1 FEEDER NO. 1 34-L MAIN DC NO. 2 FEEDER BUS

POWER FEEDER NO. 2 FEEDER NO. 2 34-L MAIN DC NO. 2 FEEDER BUS

MAIN DC AVIONICS BUS NO. 1 POWER FEED FEEDER AVIONICS BUS 34-R MAIN DC NO. 1 FEEDER BUS

MAIN DC AVIONICS BUS NO. 2 POWER FEED FEEDER AVIONICS BUS 34-L MAIN DC NO. 2 FEEDER BUS

TEST RECEPTACLE AVIONICS TEST RECP MISC 34-L MAIN DC NO. 2 FEEDOR

USTS POWER 6ÊR BUS

USTS POWER OC BUS 34-L MAIN DC NO. 2 FEEDER BUS

EMERGENCY DC BUS BUS WARN LTS 32-L ISOLATED DC BUSISOLATED DC BUS ISOL DC BUS IND 31-L ISOLATED DC BUSMAIN DC BUS NO. 1 BUS VOLT TEST 34-R MAIN DC BUS 1MAIN DC BUS NO. 2 BUS VOLT TEST 34-L MAIN DC BUS 2

ELECTRICAL SYSTEM - EMERGENCY GENERATORAC ACPHA.B.CPOWER CFJB EMERGENCY GENDC DC POWER CFJB EMERGENCY GENEMERGENCY GENERATOR CONTROL EMERG POWER CONTROL (9-A) EMERGENCY GENEMERGENCY POWER ON LIGHT EMERG POWER CONTROL (9-A) EMERGENCY GEN

ELEVATORARTIFICIAL FEEL: ELEV & ART FEEL PWR 16-R ESSENTIAL AC BUS 1

ELEV ART FEEL & CADC NO. 1 EXCIT 30-R ISOLATED DC BUSELEV ART FEEL SERVO EXC 22-L 26V AC BUS 1ELEV FEEL CADC EXC NO. 2 22-L 26V AC BUS 1ELEVATOR COMPARATOR PWR 22-L 26V AC BUS 1

ARTIFICIAL FEEL MALFUNCTION LIGHT WARN LT TEST & ANNUN CONT NO. 1 26-R ISOLATED DC BUSELEVATOR POWER CONTROL SWITCHES:

HYDRAULIC SYSTEM NO. 1 ELEV HYD POWER SYS NO. 1 26-R ISOUTEDOCBUSHYDRAUUC SYSTEM NO. 2 ELEV HYD POWER SYS NO. 2 27-R ISOUTEDOCBUS

ELEVATOR EMERGENCY POWER ELEV EMERG HYD SYS 30-R ISOUTED DC BUSPOWER OFF U6HTS ELEV HYD PWR IND 28-R ISOUTED DC BUSELEVATOR EMERGENCY POWER WARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUS

ANNUNCIATOR UGHT

^ A AIRCRAFT MODIFIED BY TCTO 530

Figure 1-182. Circuit Breaker Index (Sheet 10 of 31)

1-451

TO 1C-141C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCED E S I G N A T I O N | LOCATIONELEVATOR (CONTINUED)

ELEVATOR EMERGENCY POWER ON LIGHT ELEV HYD PWR IND 28-R ISOUTED DC BUSELEVATOR EMERGENCY POWER OFF LIGHT ELEV HYD PWR IND 28-R ISOUTED DC BUSELEVATOR SYSTEM POWER OFF WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUS

ANNUNCIATOR UGHTS WARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUSPITCH RATE ADAPTER PITCH RATE ADPT EXC (S-C) 26V EMERGENCY AC

ENGINE

ENGINE NO. 1 ENG NO. 1 EMERG SHUTDOWN REUY 26-R ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 EMERG SHUTDOWN REUY 27-R ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 EMERG SHUTDOWN REUY 28-R ISOUTED DC BUSENGINE NO. 4 ENG NO. 4 EMERG SHUTDOWN REUY 29-R ISOUTEDOCBUS

FUEL ENRICHMENT ENG FUEL ENRICH VALVES 31-L ISOUTEDOCBUSFUEL HEATERS AND FUEL HEAT LIGHTS:

ENGINE NO. 1 FUEL HEAT & IND LTS NO. 1 35-L MAIN DC BUS 1ENGINE NO. 2 FUEL HEAT & IND LTS NO. 2 40-L MAIN DC BUS 2ENGINE NO. 3 FUEL HEAT & IND LTS NO. 3 40-L MAIN DC BUS 2ENGINE NO. 4 FUEL HEAT & IND LTS NO. 4 35-L MAIN DC BUS 1

FUEL INDICATOR UGHTS:ENGINE NO. 1 ENG FUEL & LOW BOOST PRESS.

WARN LT NO.136-L MAIN DC BUS 1

ENGINE NO. 2 ENG FUEL & LOW BOOST PRESS.WARN LT NO. 2

44-L MAIN DC BUS 2


44-L MAIN DC BUS 2


36-L MAIN DC BUS 1

FUEL INLET TEMPERATURE INDICATOR CSD. ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1FUEL SHUTOFF VALVES:

POWER:ENGINE NO. 1 ENG NO. 1 FUEL SHUTOFF VALVE 26-L ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 FUEL SHUTOFF VALVE 27-L ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 FUEL SHUTOFF VALVE 28-L ISOUTED DC BUSENGINE NO. 4 ENG NO. 4 FUEL SHUTOFF VALVE 29-L ISOUTEDOCBUS

CONTROL - FUEL AND STARTIGNITION SWITCH:

ENGINE NO. 1 ENG NO. 1 START & START IGNITION 26-L ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 START & START IGNITION 27-L ISOUTEDOCBUSENGINE NO. 3 ENG NO. 3 START & START IGNITION 28-L ISOUTEDOCBUSENGINE NO. 4 ENG NO. 4 START & START IGNITION 29-L ISOUTED DC BUS

CONTROL • FIRE CONTROL HANDLE:ENGINE NO. 1 ENG NO. 1 EMERG SHUTDOWN REUY 26-R ISOUTEDOCBUSENGINE NO. 2 ENG NO. 2 EMERG SHUTDOWN REUY 27-R ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 EMERG SHUTDOWN REUY 28-R ISOUTED DC BUSENGINE NO. 4 ENG NO. 4 EMERG SHUTDOWN REUY 29-R ISOUTED DC BUS

CONTINUOUS IGNITION SWITCH:ENGINE NO. 1 ENG CONTINUOUS IGNITION NO. 1 14-R ESSENTIAL AC BUS 1ENGINE NO. 2 ENG CONTINUOUS IGNITION NO. 2 19-R ESSENTIAL AC BUS 2ENGINE NO. 3 ENG CONTINUOUS IGNITION NO. 3 19-R ESSENTIAL AC BUS 3ENGINE NO. 4 ENG CONTINUOUS IGNITION NO. 4 14-R ESSENTIAL AC BUS 1

FUEL AND START IGNITION SWITCH:ENGINE NO.1 ENG NO. 1 START & START IGNITION 26-L ISOUTEDOCBUSENGINE NO. 2 ENG NO. 2 START & START IGNITION 27-L ISOUTEDOCBUSENGINE NO. 3 ENG NO. 3 START & START IGNITION 28-L ISOUTEDOCBUSENGINE NO. 4 ENG NO. 4 START & START IGNITION 29-L ISOUTED DC BUS


1-452

TO 1C-141C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCEDESIGNATION LOCATIONE N G I N E ( C O N T I N U E D ) >

STARTER BUTTONA/ALVE:ENGINE NO. 1 ENG NO.1 START & START IGNITION 26-L ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 START & START IGNITION 27-L ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 START & START IGNITION 28-L ISOUTEDOCBUSENGINE NO. 4 ENG NO. 4 START & START IGNITION 29-L ISOUTEDOCBUS

STARTER VALVE OPEN LIGHTS:ENGINE NO. 1 LOW OIL PRESS. & START VALVE

POSITION IND NO. 137-L MAIN DC BUS 1

ENGINE NO. 2 LOW OIL PRESS. & START VALVEPOSITION IND NO. 2

37-L MAIN DC BUS 1


37-L MAIN DC BUS 1


37-L MAIN DC BUS 1

ENGINE PRESSURE RATIO (EPR):ENGINE NO. 1 ENG PRESSURE RATIO NO. 1 25-L ISOUTED AC BUSENGINE NO. 2 ENG PRESSURE RATIO NO. 2 24-L ISOUTED AC BUSENGINE NO. 3 ENG PRESSURE RATIO NO. 3 24-L ISOUTED AC BUSENGINE NO. 4 ENG PRESSURE RATIO NO. 4 25-L ISOUTED AC BUS

ENGINE VIBRATION INDICATOR (EVI): ENG VIB IND 25-R ISOUTED DC BUSN1 RPM. N2 RPM. EGT & FUEL FLOW:

ENGINE NO. 1 EGT-RPM FUEL FLOW NO. 1 20-R ESSENTIAL AC BUS 2ENGINE NO. 2 ENG EGT-RPM FUEL FLOW NO. 2 18-R ESSENTIAL AC BUS 2ENGINE NO. 3 ENG EGT-RPM FUEL FLOW NO. 3 18-R ESSENTIAL AC BUS 2ENGINE NO. 4 ENG EGT-RPM FUEL FLOW NO. 4 20-R ESSENTIAL AC BUS 2

LOW OIL QUANTITY LIGHT ENG LOW OIL QTY IND 35-R MAIN DC BUS 1LOW OIL PRESSURE WARNING LIGHT


37-L MAIN DC BUS 1


37-L MAIN DC BUS 1


37-L MAIN DC BUS 1


37-L MAIN DC BUS 1

OIL PRESSURE INDICATORENGINE NO. 1 ENG OIL PRESS. IND NO. 1 23-L 26V AC BUS 1ENGINE NO. 2 ENG OIL PRESS. IND NO. 2 23-R 26V AC BUS 2ENGINE NO. 3 ENG OIL PRESS. IND NO. 3 23-R 26V AC BUS 2ENGINE NO. 4 ENG OIL PRESS. IND NO. 4 23-L 26V AC BUS 1

OIL TEMPERATURE INDICATORENGINE NO. 1 CSD ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1ENGINE NO. 2 CSD & ENG OIL TEMP IND NO. 2 40-L MAIN DC BUS 2ENGINE NO. 3 CSD & ENG OIL TEMP IND NO. 3 40-L MAIN DC BUS 2ENGINE NO. 4 CSD ENG OIL TEMP IND NO. 4 35-L MAIN DC BUS 1

POSITION & PRESS. INDICATOR POWER:ENGINE NO. 1 ENG NO. 1 THRUST REV POS IND PWR 26-R ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 THRUST REV POS IND PWR 27-R ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 THRUST REV POS IND PWR 28-R ISOUTED DC BUSENGINE NO. 4 ENG NO. 4 THRUST REV POS IND PWR 29-R ISOUTEDOCBUSPRESSURE VALVE POWER:ENGINE NO.1 ENG NO. 1 THRUST REV PRESS. VALVE

POWER26-R ISOUTEDOCBUS

ENGINE NO. 2 ENG NO. 2 THRUST REV PRESS. VALVEPOWER

27-R ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 THRUST REV PRESS. VALVE

POWER 28-R ISOUTEDOCBUSENGINE NO. 4 ENG NO. 4 THRUST REV PRESS. VALVE

P O W E R | 29-R ISOUTED DC BUS

Figure 1-182. Circuit Breaker Index (Sheet 12 of 31

1-453

T01C-141C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCEDESIGNATION LOCATIONFLAPS

ASYMMETRY:CONTROL WING FLAPS BRAKES ACT CONT 43-R MAIN DC BUS 2

WING FUPS HYD SHUT OFF VALVE 43-R MAIN DC BUS 2DETECTION AND WARNING LIGHTS FUP ASYMN CONT WARN LT 30-R ISOUTED DC BUS

POWER WING FLAP ASYMM DET PWR 23-R 26V AC BUS 2FUP POSITION INDICATOR WING FUP POS IND 38-R MAIN DC BUS 1STOP POSITION INDICATOR (HIGH-FORCE SPOILER AUTO GND OPERATION NO. 2 44-R MAIN DC BUS 2

DETENT)FUGHT CONTROL SYSTEMSA H C B A U . — I

AILERON POWER CONTROL SWITCHESLEFT LH AILERON SYSTEM NO. 1 39-R MAIN DC BUS 1

LH AILERON SYSTEM NO. 2 43-R MAIN DC BUS 2RIGHT RH AILERON SYSTEM NO. 1 39-R MAIN DC BUS 1RH AILERON SYSTEM NO. 2 44-R MAIN OC BUS 2

POWER OFF LIGHTS LH AILERON IND 43-R MAIN DC BUS 2RH AILERON IND 44-R MAIN DC BUS 2SYSTEM POWER ANNUNCIATOR LIGHTS WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUSWARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUSTAB OPERABLE:

LEFT AILERON TAB ACTR LH 31-R ISOUTED DC BUSRIGHT AILERON TAB ACTR RH 31-R ISOUTED DC BUS

TAB OPERABLE ANNUNCIATION WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUSWARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUSTRIM AILERON TRIM CONT 13-R ESSENTIAL AC BUS 1TRIM INDICATOR AILERON TRIM POS IND 38-R MAIN DC BUS 1

ARTIFICIAL FEEL:ELEV & ART FEEL PWR 16-R ESSENTIAL AC BUS 1ELEV ART FEEL & CADC NO. 1 EXCIT 30-R ISOUTED DC BUSELEV ART FEEL SERVO EXC 22-L 26V AC BUS 1ELEV FEEL CADC EXC NO. 2 22-L 26V AC BUS 1ELEVATOR COMPARATOR PWR 22-L 26V AC BUS 1

ARTIFICIAL FEEL MALFUNCTION LIGHT WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUSELEVATOR POWER CONTROL SWITCHES:

HYDRAULIC SYSTEM NO. 1 ELEV HYD POWER SYS NO. 1 26-R ISOUTED DC BUSHYDRAULIC SYSTEM NO. 2 ELEV HYD POWER SYS NO. 2 27-R ISOUTED DC BUS

ELEVATOR EMERGENCY POWER ELEV EMERG HYD SYS 30-R ISOUTED DC BUSPOWER OFF LIGHTS ELEV HYD PWR IND 28-R ISOUTED DC BUSELEVATOR EMERGENCY POWER WARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUS

ANNUNCIATOR LIGHTELEVATOR EMERGENCY POWER ON ELEV HYD PWR IND 28-R ISOUTED DC BUS

UGHTELEVATOR EMERGENCY POWER OFF ELEV HYD PWR IND 28-R ISOUTED DC BUS

LIGHTELEVATOR SYSTEM POWER OFF WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUS

ANNUNCIATOR LIGHTS WARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUSPITCH RATE ADAPTER PITCH RATE AOPT EXC (5-C) 26V EMERGENCY AC

ASYMMETRY SYSTEM:CONTROL: WING FUPS BRAKES ACT CONT 43-R MAIN DC BUS 2

WING FUPS HYD SHUT OFF VALVE 43-R MAIN DC BUS 2DETECTION AND WARNING LIGHTS FUP ASYMN CONT WARN LT 30-R ISOUTED DC BUSPOWER WING FLAP ASYMM DET PWR 23-R 26V AC BUS 2

FUP POSITION INDICATOR WING FUP POS IND 38-R MAIN DC BUS 1STOP POSITION INDICATOR (HIGH-FORCE SPOILER AUTO GND OPERATION NO. 2 44-R MAIN DC BUS 2

DETENT)


1-454

SSfr-t

(I£f° PI &*HS) ^P"! J9)f09jg imaitj Z81-1 *>n8}J

'0608C nUHl 8UZV idVdOdlV NO OIT1NI91W b31IOdS. 0313aVl

N0I1V1I0X3 0V10SIa-scnvadiiNn Nomsinoov viva iHOiidSOINOIAV

ovaaivtosi0-Zt>03b lidbaauooaa iHOiid

SOINOIAVov aaiviosiQ-€frbAO

suaauooau iHondnuvmiiwuv(1N3130 30bOd

z sna oa nivwU-St>1N3JL30 310NVH AOS lid Nl U31IOdSM01/H9IH) bOlVOIONI NOIUSOd dOlSZ SOS OV TVI1N3SS3b*Ot>Z "ON (lN3A3bd bO) NbVM TWISONINbVMisnaoviviiN3ss3b-seI'ONlNSASbdllVlSaiaianv ■» iH9ii assds B3QNn aaiiods

2 sna oa nivwU-St>aos baiiods e on sas oah3A1VA 0Ab3S 31BV0 H31IOdSv sna oa nivwU-9EONI SOd V7 AOS U31IOdSovid aMiNn/aaxooiisneovA9zi-ezoni sod uaiiods

NbVAAllWbV

Sb31NI0d:y01VOIONI NOIUSOd

s sna oa nivwU-Sfr1N3130 310NVH AOS ITd Nl b31IOdS^7 dOlSHWIl IHOiidz sna oa nivwa-sfaos aaiiods e on sas oahz sna oa nivwu-t>t>Z 'ON NOUVbBdO 0N9 oinv bSHOdSi sna oa nivwU-9Si on NonvuadO abo oinv bsnodslObiNOOi sna ov A9ZT6Zissi ono oinv su3iiOds1S31

z sna oa nivwH-Lt>e ON SAS OAH WWASV SU31IOdSW31SAS onnvuaAH E "ONi. sna oa nivwU-96Z ON SAS OAH WWASV usuodsW31SAS OlinVbOAH Z 'ON

:W31SASAbl3WWASV

l sna oa nivwu-eeaNisodWibiaaaanubOJWOIONI Wlbl

lSna0V1VIJLN3SS3sna oa aaiviosi

b-etH-oe

lNoowibibaaanboni b3M0d inoo aaaana

WlbliHon 3bnssaud U3A0 usaanb

sna oa aaiviosia-oeoni B3M0d inoo b3aanuS1H9I13bnSS3bd H9IH W31SASsna oa aaiviosi sna oa aaiviosi

ti-LZy-9z

Z "ON INOO NnNNV 3 1S31 11 NbVMV ON INOO NnNNV 91S3111 NbVMS1H9I1 UOlVIONnNNV U3MOd W31SAS

sna oa aaiviosiu-oeoni bSMOd inoo U3aanuS1H9I1 ddO b3M0dl sna oa nivwa-eeS3A1VA nwn avoi bsaanuS3A1VA iiwn avoiz sna oa nivwh-evz 'on waisAS UMd inoo uaaanbz on W31SAS onnvuaAH

v sna oa nivwb-esv on sas b3/v\od lObiNOO uaaanbI. ON W31SAS OlinVbOAH=S3H01IMS 10U1N00 U3AA0d bSOOnb

l sns oa nivwb-zeoni sod wiui avis zibohbOlVOIONI Wlbl HOlIdv sna oa nivwa-eeiNOOidoaia/aAH10U1N00 Wlbl HOlId OlinVbOAH\ sna oa nivwU-8ClNO01dO313/aAHOnnVbOAHObl0313z sna oa nivwb-*T>INOO Wlbl HOlId 0313TV0IU10313

U.3S3U WIUIi sna oa nivwy-6e39V0N3SI0 Wlbl HOlIdloaNNOosia wibi

zsnaovrviiNassaz sna oa nivw

U-0Z'6L'8lu-tf

bMd uoiow wibi avisIjNOO HOiniO Wlbl HOlId 0313

U3MOd Wlbl TV0IU1D313lObiNOO HOiniO WIUI 1V0IU10313

z sna oa nivwU-t>1>INOO Wlbl HOlId 031310U1N00 WIUI 1V0IU10313:WlblHOJJd

onnvuaAHOuio3i3 * ivoiuioai3

i(aanNiiNOo) swbisas iobinoo mom

aoanos d3M0dNOIIVOOINOI1VNOIS301 M~~N0«i*"J03uaxvaua unouio

t-Otfrt-OtOJL

TO 1C-141C-1

COMPONENT CIRCUIT BREAKER - POWER SOURCEDESIGNATION LOCATIONFUEL SUPPLY SYSTEMSAIQ DCC1ICI l l l l f * .

A/R ISOUTION VALVES:LEFT LH AERIAL REFUEL ISOL VALVE 39-L MAIN OC BUS 1RIGHT RH AERIAL REFUEL ISOL VALVE 45-L MAIN DC BUS 2

DISCONNECT SWITCHES AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1FUEL LINE DRAIN SWITCH FUEL DRAIN PUMP & VALVES 44-L MAIN OC BUS 2INDICATOR LIGHTS:

DISCONNECT AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1DOOR UNLOCKED AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1UTCHED AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1OVERRIDE AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1READY AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1

MASTER POWER SWITCH AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1MODE SELECT SWITCH AERIAL REFUELING CONTROL 39-L MAIN DC BUS 1

AUX TANK BOOST PUMP CONTROL:NO. 1 & NO. 4 PRIMARY PUMPS FUEL BOOST AUX PRI NO. 1 & 4 37-L MAIN DC BUS 1NO. 2 & NO. 3 PRIMARY PUMPS FUEL BOOST AUX PRI NO. 2 & 3 42-L MAIN DC BUS 2NO. 1 & NO. 4 SECONDARY PUMPS FUEL BOOST AUX SEC NO. 1 & 4 42-L MAIN DC BUS 2NO. 2 & NO. 3 SECONDARY PUMPS FUEL BOOST AUX SEC NO. 2 & 3 37-L MAIN DC BUS 1AUX TANK BOOST PUMP POWER:NO. 1 PRIMARY PUMP FUEL BOOST NO. 1 AUX PRI 1,2,3-R MAIN DC BUS 1SECONDARY PUMP FUEL BOOST NO. 1 AUX SEC 4, 5.6-R MAIN DC BUS 2NO. 2 PRIMARY PUMP FUEL BOOST NO. 2 AUX PRI 10,11.12-R MAIN DC BUS 4SECONDARY PUMP FUEL BOOST NO. 2 AUX SEC 7. 8,9-R MAIN DC BUS 3NO. 3 PRIMARY PUMP FUEL BOOST NO. 3 AUX PRI 10. 11,12-R MAIN DC BUS 4SECONDARY PUMP FUEL BOOST NO. 3 AUX SEC 7, 8, 9-R MAIN DC BUS 3NO. 4 PRIMARY PUMP FUEL BOOST NO. 4 AUX PRI 1,2,3-R MAIN DC BUS 1SECONDARY PUMP FUEL BOOST NO. 4 AUX SEC 4, 5.6-R MAIN DC BUS 2

EXTENDED RANGE TANK PUMP CONTROL:LEFT: INBOARD FUEL BOOST EXTENDED RANGE INBD 37-L MAIN DC BUS 1OUTBOARD FUEL BOOST EXTENDED RANGE OUTBD 42-L MAIN DC BUS 2RIGHT: INBOARD FUEL BOOST EXTENDED RANGE INBD 37-L MAIN DC BUS 1

OUTBOARD FUEL BOOST EXTENDED RANGE OUTBD 42-L MAIN DC BUS 2EXTENDED RANGE TANK PUMP POWER:

LEFT: INBOARD FUEL BOOST LH EXT RANGE INBD 1.2,3-R MAIN DC BUS 1OUTBOARD FUEL BOOST LH EXT RANGE OUTBD 10.11,12-R MAIN DC BUS 4

RIGHT: INBOARD FUEL BOOST RH EXT RANGE INBD 1.2, 3-R MAIN DC BUS 1OUTBOARD FUEL BOOST RH EXT RANGE OUTBD 10,11.12-R MAIN DC BUS 4

MAIN TANKS:NO. 1 PRIMARY PUMP FUEL BOOST PUMP NO. 1 MAIN PRI 13,14.15-L ESSENTIAL AC BUS 1

SECONDARY PUMP FUEL BOOST PUMP NO. 1 MAIN SEC 18,19.20-L ESSENTIAL AC BUS 2NO. 2 PRIMARY PUMP FUEL BOOST PUMP NO. 2 MAIN PRI 18.19.20-L ESSENTIAL AC BUS 2

SECONDARY PUMP FUEL BOOST PUMP NO. 2 MAIN SEC 13.14.15-L ESSENTIAL AC BUS 1NO. 3 PRIMARY PUMP FUEL BOOST PUMP NO. 3 MAIN PRI 18,19,20-L ESSENTIAL AC BUS 2

SECONDARY PUMP FUEL BOOST PUMP NO. 3 MAIN SEC 13,14.15-L ESSENTIAL AC BUS 1NO. 4 PRIMARY PUMP FUEL BOOST PUMP NO. 4 MAIN PRI 13,14,15-L ESSENTIAL AC BUS 1

SECONDARY PUMP FUEL BOOST PUMP NO. 4 MAIN SEC 18.19.20-L ESSENTIAL AC BUS 2

FUEL INLET TEMPERATURE INDICATOR CSD ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1FUEL PRESSURE INDICATOR FUEL PRESS. IND 23-R 26V AC BUS 2

^ f

■ ^ J

s-#

\ ^ f


1-456

TO 1C-141C-1

l||H^

k i i ^ j

CIRCUIT BREAKERCOMPONENT POWER SOURCE

DESIGNATION LOCATIONFUEL SUPPLY SYSTEM (CONTINUED)FUEL SYSTEM INDICATORS (CONTINUED): - -

FUEL QUANTITY SYSTEM:AUX TANK NO.1 FUEL QTY IND AUX TANK NO. 1 35-L MAIN DC BUS 1

NO. 2 FUEL QTY IND AUX TANK NO. 2 35-L MAIN DC BUS 1NO. 3 FUEL QTY IND AUX TANK NO. 3 43-L MAIN DC BUS 2NO. 4 FUEL QTY IND AUX TANK NO. 4 43-L MAIN DC BUS 2

EXTENDED RANGE TANKS: LEFT FUEL QTY IND EXT RGLH 36-L MAIN DC BUS 1RIGHT FUEL QTY IND EXT RG TANK RH 43-L MAIN DC BUS 2

MAIN TANK MAIN TANKS NO.1 FUEL QTY IND MAIN NO. 1 TANK 26-L ISOUTED DC BUSNO. 2 FUEL QTY IND MAIN NO. 2 TANK 27-L ISOUTED DC BUSNO. 3 FUEL QTY IND MAIN NO. 3 TANK 28-L ISOUTED DC BUSNO. 4 FUEL QTY IND MAIN NO. 4 TANK 29-L ISOUTED DC BUS

TOTALIZER FUEL QTY IND TOTALIZER 32-L ISOUTED DC BUS

A/R ISOUTION VALVES:LEFT LH AERIAL REFUEL ISOL VALVE 39-L MAIN DC BUS 1RIGHT RH AERIAL REFUEL ISOL VALVE 45-L MAIN DC BUS 2

CROSSFEED VALVES:NO.1 ENG NO. 1 FUEL CROSSFEED VALVE 26-L ISOUTED DC BUSNO. 2 ENG NO. 2 FUEL CROSSFEED VALVE 27-L ISOUTED DC BUSNO. 3 ENG NO. 3 FUEL CROSSFEED VALVE 28-L ISOUTEDOCBUSNO. 4 ENG NO. 4 FUEL CROSSFEED VALVE 29-L ISOUTED DC BUS

FUEL HEAT VALVES:ENGINE NO. 1 FUEL HEAT & IND LTS NO. 1 35-L MAIN DC BUS 1ENGINE NO. 2 FUEL HEAT & IND LTS NO. 2 40-L MAIN DC BUS 2ENGINE NO. 3 FUEL HEAT & IND LTS NO. 3 40-L MAIN DC BUS 2ENGINE NO. 4 FUEL HEAT & IND LTS NO. 4 35-L MAIN DC BUS 1

GROUND ISOUTION VALVE GROUND ISOL VALVE 42-L MAIN DC BUS 1JETTISON VALVES:

LEFT FUEL JETTISON VALVE LH 38-L MAIN DC BUS 1RIGHT FUEL JETTISON VALVE RH 44-L MAIN DC BUS 2

SEPARATION VALVES:CENTER FUEL SEP VALVE CTR 30-L ISOUTED DC BUSLEFT FUEL SEP VALVE LH 31-L ISOUTED DC BUSRIGHT

BCCI ICI tUfi MAI UCCJDt tMDQ.FUEL SEP VALVE RH 32-L ISOUTED DC BUS

ncrUcLINU VALvtS/rUMroiAUX TANK: NO.1 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN &

AUX NO. 1 & 442-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC MAIN & AUX NO.1&4

39-L MAIN DC BUS 1

NO. 2 PRIMARY FUEL LEVEL CONTROL VALVE-PRI AUXN0.2&3

42-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC AUX NO. 2 & 3 39-L MAIN DC BUS 1NO. 3 PRIMARY FUEL LEVEL CONTROL VALVE-PRI AUX

N0.2&342-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC AUX NO. 2 & 3 39-L MAIN DC BUS 1NO. 4 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN &

AUXN0.1&442-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC MAIN & AUX NO.1&4

39-L MAIN DC BUS 1


1-457

TO 1C-141C-1

^hh^^ m. mi mm ^Blk km a m^mt CIRCUIT BREAKERCOMPONENT POWER SOURCEDESIGNATION LOCATIONFUEL SUPPLY SYSTEM (CONTINUED)REFUEUNG VALVES/PUMPS (CONTINUED): - -

EXTENDED RANGE TANKSL E F T P R I M A R Y FUEL LEVEL CONTROL VALVE-PRI

EXTENDED RANGE42-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC EXTENDEDRANGE

FUEL LEVEL CONTROL VALVE-PRI

39-L MAIN DC BUS 1

R I G H T P R I M A RY 42-L MAIN DC BUS 2EXTENDED RANGE

SECONDARY FUEL LEVEL CONT-SEC EXTENDEDRANGE

39-L MAIN DC BUS 1GROUND ISOUTION VALVE GROUND ISOL VALVE 42-L MAIN DC BUS 1MAIN TANKS: NO. 1 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN &

AUX NO. 1 & 442-L MAIN DC BUS 2

SECONDARY FUEL LEVEL CONT-SEC MAIN & AUX NO.1 &4

39-L MAIN DC BUS 1NO. 2 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN


SECONDARY FUEL LEVEL CONT-SEC MAIN NO. 2 & 3 39-L MAIN DC BUS 1NO. 3 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN


SECONDARY FUEL LEVEL CONT-SEC MAIN NO. 2 & 3 39-L MAIN DC BUS 1NO. 4 PRIMARY FUEL LEVEL CONTROL VALVE-PRI MAIN &

AUX NO. 18,4 42-L MAIN DC BUS 2SECONDARY FUEL LEVEL CONT-SEC MAIN & AUX NO.

1 & 4 39-L MAIN DC BUS 1SPR DRAIN PUMP AND VALVES FUEL DRAIN PUMP & VALVES 44-L MAIN DC BUS 2

BOOST PUMP PRESSURE LOW UGHTS:NO. 1 MAIN. NO. 1 AUX AND LH EXT RNG ENG FUEL & LOW BOOST PRESS. WARN 36-L MAIN DC BUS 1OUTBD LTNO. 1NO. 2 MAIN. NO. 2 AUX AND LH EXT RNG ENG FUEL & LOW BOOST PRESS. WARN 44-L MAIN DC BUS 2INBD LT NO. 2NO. 3 MAIN. NO. 3 AUX AND RH EXT RNG ENG FUEL & LOW BOOST PRESS. WARN 44-L MAIN DC BUS 2

INBD LT NO. 3NO. 4 MAIN, NO. 4 AUX AND RH EXT RNG ENG FUEL & LOW BOOST PRESS. WARN 36-L MAIN DC BUS 1OUTBD LT NO. 4

FUEL JETTISON STOP PUMP UGHTS:PRIMARY PUMPS FUEL BOOST AUX PRI NO. 1 & 4 37-L MAIN DC BUS 1SECONDARY PUMPS FUEL BOOST AUX SEC NO. 1 & 4 42-L MAIN DC BUS 2

SUMP LOW UGHTS:CONTROL UNITS: NO. 1 & 4 MAIN TANKS FUEL SUMP & LOW WARN CONT UNIT NO.

1&4MAINTANK38-L MAIN DC BUS 1

NO. 2 &3 MAIN TANKS FUEL SUMP LOW WARN CONT UNIT NO. 2& 3 MAIN TANK

43-L MAIN DC BUS 2

UGHTS: NO. 1 MAIN TANK FUEL SUMP & LOW WARN LT NO. 1 MAINTANK

38-L MAIN DC BUS 1

NO. 2 MAIN TANK FUEL SUMP LOW WARN LT NO. 2 MAINTANK

43-L MAIN DC BUS 2

NO. 3 MAIN TANK FUEL SUMP LOW WARN LT NO. 3 MAINTANK

43-L MAIN DC BUS 2

NO. 4 MAIN TANK FUEL SUMP & LOW WARN LT NO. 4 MAINTANK

36-L MAIN DC BUS 1

HYDRAULIC SYSTEMS

EMERGENCY BRAKE PRESSURE HYD PRESS. IND EMER BK PRESS. 23-R 26V AC BUS 1NORMAL BRAKE PRESSURE HYD PRESS. INDICATORS NORM BRAKE

PRESS.23-L 26V AC BUS 2

HYD SYSTEM NO.1 HYD PRESS. INDICATORS NO. 1 SYS 23-L 26V AC BUS 1PRESS.


1-458

TO 1C-141C-1

COMPONENT CIRCUIT BREAKERPOWER SOURCEDESIGNATION LOCATION

HYDRAULIC SYSTEMS (CONTINUED)HYD SYSTEM NO. 2 HYD PRESS. IND NO. 2 SYS PRESS. 23-R 26V AC BUS 2HYD SYSTEM NO. 3 HYD PRESS. INDICATORS NO. 3 SYS


HYDRAULIC SYSTEM UGHTS:PRESSURE LOW LIGHTS:

NO. 1 & 4 ENGINE-DRIVEN PUMPS HYD PUMPS LOW PRESS LTS ENGN0.1&4

33-L ISOUTED DC BUS

NO. 2 & 3 ENGINE-DRIVEN PUMPS HYD PUMPS LOW PRESS LTS ENGN0.2&3

33-L ISOUTEDOCBUS

NO. 1 SYSTEM SUCTION BOOST PUMP HYDRAULIC SYSTEM NO. 1 SUCTIONBOOST PUMP WARN

37-R MAIN DC BUS 1

NO. 2 SYSTEM SUCTION BOOST PUMP HYDRAUUC SYSTEM NO. 2 SUCTIONBOOST PUMP WARN

42-R MAIN DC BUS 2

NO. 3 HYD SYS PRESSURE ON LIGHT HYDRAULIC SYSTEM NO. 3 PRESSUREON LIGHT

37-R MAIN DC BUS 1

HYDRAULIC SYSTEMS NO. 1 AND NO. 2:ENGINE-DRIVEN PUMP VALVES:

ENGINE NO. 1 ENG NO. 1 HYD PUMP VALVES CONTROL 26-L ISOUTED DC BUSENGINE NO. 2 ENG NO. 2 HYD PUMP VALVES CONTROL 27-L ISOUTED DC BUSENGINE NO. 3 ENG NO. 3 HYD PUMP VALVES CONTROL 28-L ISOUTED DC BUSENGINE NO. 4 ENG NO. 4 HYD PUMP VALVES CONTROL 29-L ISOUTED DC BUS

SUCTION BOOST PUMPS:CONTROL: NO. 1 SYSTEM HYDRAULIC SYSTEM NO. 1 SUCTION

BOOST PUMP CONT42-R MAIN DC BUS 2

NO. 2 SYSTEM HYDRAUUC SYSTEM NO. 2 SUCTIONBOOST PUMP CONT

37-R MAIN DC BUS 1

P O W E R : N O . 1 S Y S T E M NO. 1 HYD SYS SUCT BOOST PUMP PWR 18.19.20-L ESSENTIAL AC BUS 2NO. 2 SYSTEM NO. 2 HYD SYS SUCT BOOST PUMP PWR 13.14,15-L ESSENTIAL AC BUS 1

HYDRAULIC SYSTEM NO. 3:ELECTRIC-DRIVEN HYDRAUUC PUMPS

CONTROL: NO. 1 PUMP HYDRAULIC SYSTEM NO. 3 NO. 1 PUMPCONT

37-R MAIN DC BUS 1

NO. 2 PUMP HYDRAULIC SYSTEM NO. 3 NO. 2 PUMPCONT

42-R MAIN DC BUS 2

P O W E R : N O . 1 P U M P HYD SYS NO. 3 PUMP NO. 1 PWR 1,2, 3-R MAIN AC BUS 1NO. 2 PUMP HYD SYS NO. 3 PUMP NO. 2 PWR 8,9,10-R MAIN AC BUS 3

ACCUMUUTOR CONTROL VALVE HYD SYS NO. 3 SPOILER SOV 45-R MAIN DC BUS 2SPOILER CABLE SERVO VALVE HYD SYS NO. 3 SPOILER SOV 45-R MAIN DC BUS 2

INSTRUMENTS/AVIONICSAILERON TRIM INDICATOR AILERON TRIM POS IND 38-R MAIN DC BUS 1BOGEY POSITION INDICATOR BOGEY POS IND 32-R ISOUTED DC BUS

SCADC NO. 1 (PILOT'S) CADC NO.1CADC AIRSPEED GROUP NO. 1 EXC (5-B)

(7-B)EMERGENCY AC BUS26V EMER AC BUS B

CADC NO. 1CADC ALT GROUP NO. 1 EXCCADCA/SFI TEST (PILOT)

(5-B)(7-C)8-A

EMERGENCY AC26V EMER AC BUS BMAIN DC AVIONICS 2

SCADC NO. 2 (COPILOTS)PWR CADC NO. 2AIRSPEED GROUPALT GROUP

2-B4-C3-D

NAVIGATION AC 226 VAC EXCITATION26 VAC EXCITATION

TAS NAV

CADCA/SFI TEST (COPILOT) |

4-D 26V AC NAVEXCITATION 2MAIN DC AVIONICS 2


1-459

T01C-141C-1

COMPONENTCIRCUIT BREAKER

POWER SOURCEDESIGNATION | LOCATIONINSTRUMENTS /AVIONICS (CONTINUED)

DU1 DU NO. 1DU NO. 1 HTR

3-A32-D

MAIN DC AVIONICS 1MAIN DC AVIONICS 1

DU2 DUNO. 2DU NO. 2 HTR (12-C)

13-AEMERGENCY DCMAIN DC AVIONICS 2

DU3 DUNO. 3DUNO. 3 HTR

2-A31 -D

MAIN DC AVIONICS 1MAIN DC AVIONICS 1

DU4 DU NO. 4DUNO. 4 HTR

(11-C)12-A

EMERGENCY DCMAIN DC AVIONICS 2

CDS OIL TEMPERATURE GAGE

NO.1NO. 2NO. 3NO. 4

CDS ENG OIL & FUEL TEMP IND NO. 1CDS & ENG OIL TEMP IND NO. 2CDS & ENG OIL TEMP IND NO. 3CDS ENG OIL TEMP INO NO. 4

35-L40-L40-L35-L

MAIN DC BUS 1MAIN DC BUS 1MAIN DC BUS 1MAIN DC BUS 1

AC VOLTMETER/FREQUENCY METER:

GENERATOR NO. 1GENERATOR NO. 2

GENERATOR NO. 3

GENERATOR NO. 4

APU GENERATOR

GEN NO. 1 VOLT AND FREQ TEST (3C/B)GEN NO. 2 VOLT & FREQ TEST (PH A, B,

C) (3C/B)GEN NO. 3 VOLT & FREQ TEST (PH A, B,

C) (3C/B)GEN NO. 4 VOLT AND FREQ TEST (PH A.

B. C) (3C/B)AUX GEN VOLT AND FREQ TEST (3C/B)

ACPDC 12ACPDC 11

ACPDC 10

ACPDC 9

ACPDC 9EXTERNAL POWER

EMERGENCY POWER

EXTERNAL POWER VOLT AND FREQTEST(PHA.B.C)(3C/B)

AC VOLTAGE TEST (PH. A. B. C) (3C/B)ACPDC 9

EMERGENCYGEN. CONTROL

DC VOLTMETER BOX

EMERGENCY DC BUSISOUTED DC BUSMAIN DC BUS NO. 1MAIN DC BUS NO. 2

BUS WARN LTSISOL DC BUS INDBUS VOLT TESTBUS VOLT TEST

32-L31-L34-R344.

ENGINE PRESSURE RATIO (EPR)

NO.1 ENGINENO. 2 ENGINENO. 3 ENGINENO. 4 ENGINE

ENG PRESSURE RATIO NO. 1ENG PRESSURE RATIO NO. 2ENG PRESSURE RATIO NO. 3ENG PRESSURE RATIO NO. 4

25-L244.24-L25-L

ISOUTED AC BUSISOUTED AC BUSISOUTED AC BUSISOUTED AC BUS

ENGINE VIBRATION INDICATOR (EVI) ENGVIBINDENGVIB-IND

25-R31-L

ISOUTED AC BUSISOUTED DC BUS

N], RPM. N2, RPM EGT & FUEL FLOW:


ENG EGT-RPM FUEL FLOW NO. 1ENG EGT-RPM FUEL FLOW NO. 2ENG EGT-RPM FUEL FLOW NO. 3ENG EGT-RPM FUEL FLOW NO. 4

20-R18-R18-R20-R

ESSENTIAL AC BUS 2ESSENTIAL AC BUS 2ESSENTIAL AC BUS 2ESSENTIAL AC BUS 2

OIL PRESSURE INDICATOR


ENG OIL PRESS IND NO. 1ENG OIL PRESS. IND NO. 2ENG OIL PRESS. IND NO. 3ENG OIL PRESS IND NO. 4

23-L23-R23-R23-L

26V AC BUS 126V AC BUS 226V AC BUS 226V AC BUS 1

Figure 1-182. Circuit Breaker Index (Sheet 19 of 3i

■ ^ J

1-460

TO 1 C-141 C-1

y^v

% ^

\ j ^

CIRCUIT BREAKER POWER SOURCECOMPONENT DESIGNATION LOCATIONINSTRUMENTS/AVIONICS (CONTINUED

OIL TEMPERATURE INDICATORNO. 1 ENGINE CSD ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1

NO. 2 ENGINE CSD & ENG OIL TEMP IND NO. 2 40-L MAIN DC BUS 2

NO. 3 ENGINE CSD & ENG OIL TEMP IND NO. 3 40-L MAIN DC BUS 2

NO. 4 ENGINE CSD ENG OIL TEMP IND NO. 4 35-L MAIN DC BUS 1

FLAP POSITION INDICATOR WING FUP POS IND 38-R MAIN DC BUS 1

FUEL INLET TEMPERATURE INDICATOR CSD ENG OIL & FUEL TEMP IND NO. 1 35-L MAIN DC BUS 1

FUEL PRESSURE INDICATOR FUEL PRESS. IND 23-R 26V AC BUS 2

FUEL QUANTITY SYSTEM:A U X TA N K : N O . 1 FUEL QTY IND AUX TANK NO. 1 35-L MAIN DC BUS 1

NO. 2 FUEL QTY IND AUX TANK NO. 2 35-L MAIN DC BUS 1



EXTENDED RANGE TANKS:LEFT FUEL QTY IND EXT RG LH 36-L MAIN DC BUS 1

RIGHT FUEL QTY IND EXT RG TANK RH 43-L MAIN DC BUS 2

MAIN TANK: NO. 1 FUEL QTY IND MAIN NO. 1 TANK 26-L ISOUTED DC BUS

NO. 2 FUEL QTY IND MAIN NO. 2 TANK 27-L ISOUTED DC BUS

NO. 3 FUEL QTY IND MAIN NO. 3 TANK 28-L ISOUTED DC BUS

NO. 4 FUEL QTY IND MAIN NO. 4 TANK 294. ISOUTED DC BUS

TOTALIZER FUEL QTY IND TOTAUZER 32-L ISOUTED DC BUS

EMERGENCY BRAKE PRESSURE HYD PRESS. IND EMER BK PRESS. 23-R 26V AC BUS 2HYD PRESS. INDICATORS NORM BRAKE 23-L 26V AC BUS 1

PRESS.HYD SYSTEM NO. 1 HYD PRESS. INDICATORS NO. 1 SYS


HYD SYSTEM NO. 2 HYD PRESS. IND NO. 2 SYS PRESS. 23-R 26V AC BUS 2

HYD SYSTEM NO. 3 HYD PRESS. INDICATORS NO. 3 SYSPRESS.

234. 26V AC BUS 1

BOGEY POSITION INDICATOR BOGEY POS IND 32-R ISOUTED DC BUS

LANDING GEAR POSITION INDICATOR LANDING GEAR POS IND 31-R ISOUTED DC BUS

MULTIFUNCTION STANDBY MFSI SYS 9-B EMERGENCY DC

INSTRUMENT SYSTEM (MFSI) MFSI-2 33L BATTERY BUS

NAVIGATOR'S TRUE AIRSPEED INDICATOR TAS NAV 4-D 26 VAC NAVEXCITATION 2

FLIGHT CONTROL PANEL/MODE SELECT FCP/MSP NO. 1 (7-A) EMER DC

PANEL: FCP 2 741 26V AC NAVEXCITATION 2

MSP NO. 2 35-B MAIN DC AVIONICS 1

REFERENCE SET PANEL:PILOTS AND COPILOTS RSP AHRS ATT2/RSP 1 & 2 EXC (4-A) 26V EMER AC BUS A


1-461

TO 1C-141C-1


F*0^%m\Wrm&% Jj*Ji*^ i ••J"%JJ*»j j i»POWER SOURCEDESIGNATION LOCATIONINSTRUMENTS /AVIONICS (CONTINUED)IWSCEUANEOUS INDICATORS (CONTINUED):RADAR ALTIMETER RADAR ALT 28B MAIN DC AVIONICS 1

RADAR (AN/APS-133):

POWER RADAR 28-D AC AVIONICS BUS 1RADAR OATA PROCESSOR(RDP)

RDP 14-A MAIN DC AVIONICS 2

PILOTS MFD DC MFD 12-C MAIN DC AVIONICS 2SKE RADAR (AN/APN169B):/t\AUXILIARY INTERFACE UNIT AIU 30-B MAIN DC AVIONICS 1NAVIGATOR'S MFD NAV MFD 32-C AC AVIONICS BUS 1POWER SKE 13.14,15-L ESSENTIAL AC 1

SKE 39-R (2 C/Bs) MAIN DC 1PITCH TRIM INDICATOR HORIZ STAB TRIM POS IND 37-R MAIN DC BUS 1RUDDER TRIM INDICATOR RUDDER TRIM POS IND 38-R MAIN DC BUS 1SPOILER POSITION INDICATOR

POINTERS SPOILER POS IND. 23-L 26V AC BUS 1LOCK/UNLKD FUG SPOILER SOV & POS IND 36-R MAIN DC BUS 1

TOTAL TEMPERATURE INDICATOR TOTAL TEMP IND 2-R MAIN AC BUS 1LANDING GEAR AND BRAKESB R A K E S : - — -

ANTI-SKID ANTI-SKID FAIL SAFE ISOL 39-R MAIN DC BUS 1ANTI-SKID POWER 39-R MAIN DC BUS 1

BRAKE SELECTOR SWITCH:EMERGENCY BRAKES EMERG BRAKES 30-R ISOUTED DC BUSNORMAL BRAKES ANTI-SKID PWR 39-R MAIN DC BUS 1

PRESSURE. INDICATORSEMERGENCY BRAKE PRESSURE HYD PRESS. IND EMER BK PRESS. 2<R 26V AC BUS 2NORMAL BRAKE PRESSURE HYD PRESS. INDICATORS NORM BRAKE

PRESS. 23-L 26V AC BUS 1BRAKE SYSTEM LIGHTS:

ANTI-SKID DET OUT LIGHT ANTI-SKID IND LT 32-R ISOUTED DC BUSANTI-SKID OFF LIGHT ANTI-SKID IND LT 32-R ISOUTED DC BUSBRAKES RELEASED LIGHT ANTI-SKID POWER 39-R MAIN DC BUS 1

CONTROL LANDING GEAR CONT 30-R ISOUTEDOCBUSBOGEY POSITION INDICATOR BOGEY POS IND 32-R ISOUTEDOCBUSLANDING GEAR POSITION INDICATOR UNDING GEAR POS IND 31-R ISOUTED DC BUSUNDING GEAR WARNING HORN UNDING GEAR WARN 32-R ISOUTED DC BUSRUDDER PEDAL STEERING RUDDER PEDAL STEERING 384% MAIN DC 1TOUCHDOWN REUYS UNDING GEAR TOUCH DOWN REUYS 31-R ISOUTED DC BUS

A AIRCRAFT MODIFIED BY TCTO 520


1-462 Change 1

C9fr-t

(l£f° ZZ &*HS) x9puj J9i[D9ug tmoufj Z8l'l 9jn3fd

its 0101 as aaidiaow ldvuourv

t> sna ov nivwTZlsnixviHai sna ov nivwTZsnixviHiB3M0dz sna oa nivwa-st>INOO SH IXVl V 311OB1NO0

:SlH9n IXVlt> sna ov nivwi-u1IV1 Sll N0I1V9IAVNt> sna ov nivwi-vvHB ONIM Sll N0LLV9IAVNt> sna ov nivwTUHI 9NIM Sll N0I1V9IAVN:SlH9n N0I1V9IAVN* sna ov nivw1-ZlSll 31B3M0dz sna oa nivwa-sv>INOO Sll IXVl 931iobinoo

:S1H9I1 3903 9NI0V31t> sna ov nivwTZlUMd Sll 901 Hav sna ov nww1-tUMd Sll 901 HIB3M0dt> sna ov nivwi-zvaoiow sn oai Hav sna ov nivwl-laoiow sn oai maoiowv sna oa nivwa-zeONI 11 9NI0NVIBOlVOIONIz sna oa nivwi-t>t>Sll 9NI0NVI Hai sna oa nivwa-zeINOO 9NI0NV1 HIiobinoo

:S1H9I19NI0NV1snaovA9ardo11 NOUVMBOd

i sna ov nivwl-zii Nouvwaoda3M0dv sna oo nivwa-9eINOO 11 NOUVMBOdIOBINOO

:S1H9I1 NOIlVWBOdz sna oa nivwTOt>aaddn n iioo-iinvaaddnv sna oa nivw1-96B3M01111100I1NVB3M01

^7:S1H9I1 380U1S N0ISI1100 I1NVZSnaOVTVIlN3SS3T12aaddn sn noisihoo-iinvB3ddnlSnaOVTVUN3SS3TZlB3M0111 NOISniOO-llNVB3M01

:S1H9I1 NOISIllOO I1NVi sna oa nivwT6Csii AVMdiis isaavnS1H9I1 AVMdllS

l Sna OV TVI1N3SS3H-LVsiHon oNiarvd isaavnS1H9I1 ONIBlVd 9NH3nd3B BIV:9NI1H9I1 DNI13nd3B BIV

9NI1H9IT

N0I1V0O1NOI1VNOIS3QHounosuajviodINBNOdl/VOO

U3»v3ug unouio«JJk>W^Hi ^^0<wmm w^^^r

t-Otfrt-Ot 01

TO 1C-141C-1


POWER SOURCEDESIGNATION LOCATION

LIGHTING (CONTINUED)INTERIOR LIGHTING 'FLIGHT STATION)' - -■■» i * » r » < * # < » * » i » ^ t > ■ ■ i i » * ^ ^ * * >■ *■ *■ • i w M n t i w n j , — ~

COPILOTS:INSTRUMENT FLOOD COPLT INSTR FLOOD LTS 17-L ESSENTIAL AC BUS 1INSTRUMENT PANEL COPLT PNL INST LTS 22-L ESSENTIAL AC BUS 2LETDOWN HOLDER COPLT INSTR FLOOD LTS 17-L ESSENTIAL AC BUS 1SCROLL CHECKLIST COPLT INSTR FLOOD LTS 17-L ESSENTIAL AC BUS 1SIDE CONSOLE COPLT SIDE CONSOLE LTS 17-L ESSENTIAL AC BUS 1UTILITY - GURE SHIELD COPLT INSTR FLOOD LTS 17-L ESSENTIAL AC BUS 1

FLIGHT ENGINEER'S:FLOOD FLT ENGR PNL FLOOD LTS 17-L ESSENTIAL AC BUS 1INSTRUMENT FLT ENGR INST LTS 22-L ESSENTIAL AC BUS 2PANEL FLT ENGR PNL LTS 22-L ESSENTIAL AC BUS 2MAIN CIRCUIT BREAKER PANELS MAIN CKT BKR PNL LTS 16-L ESSENTIAL AC BUS 1SCROLL CHECKLIST FLT ENGR PNL FLOOD LTS 17-L ESSENTIAL AC BUS 1

FLIGHT STATION OOME FLT STA DOME LT 1-L MAIN AC BUS 1NAVIGATOR'S:

FLOOD, UTILITY NAV PANEL FLOOD LTS 16-L ESSENTIAL AC BUS 1INSTRUMENT NAV INSTR LTS 21-L ESSENTIAL AC BUS 2PANEL NAV PANEL LTS 22-L ESSENTIAL AC BUS 2

PILOTS:INSTRUMENT FLOOD PLT INST FLOOD LTS (11-A) EMERGENCY DC BUSINSTRUMENT PANEL PLT PNL INSTR LTS 17-L ESSENTIAL AC BUS 1LETDOWN HOLDER PLT INST FLOOD LTS (11-A) EMERGENCY DC BUSSIDE CONSOLE PLT SIDE CONSOLE LTS 17-L ESSENTIAL AC BUS 1

CENTER CONSOLEMFCDU. MSP. RSP. FCP. IFF.AND CADC/YAW DAMPER PANEL

PLT CTR CSL LTS(5VAC)

29-C ESSENTIAL AC BUS 1

UTILITY - OVERHEAD PLT INST FLOOD LTS (11-A) ESSENTIAL DC BUSPILOTS' OVERHEAD:

OVERHEAD FLOOD OVERHEAD PNL FLOOD LTS 21-L ESSENTIAL AC BUS 2OVERHEAD PANEL OVERHEAD PNL LTS 16-L ESSENTIAL AC BUS 1UTIUTY- OVERHEAD PLT & COPLT UTILLT 6-L 28V AC BUS 2

PILOTS' CENTER:CONSOLE PEDESTAL LTS 17-L ESSENTIAL AC BUS 1INSTRUMENT PANEL CTR INSTR PNL LTS 16-L ESSENTIAL AC BUS 1

READING LIGHTS:POWER FLT STA LTG TRANS 4-L MAIN AC BUS 2PROTECTION FLT STA READING LT 54. 28V AC BUS 2

THUNDERSTORM CAUTION LTS DIM REUY CONT 45-R MAIN DC BUS 2


1-464 Change 1

S9fr-t

(I£Jo PZ tHS) x»P**IJt9V>9jg tmiutj Z8lml «»*»*

isnaovAszerdonavisivoiib3ANOI1031Obdi sna ov nivwu-iSll 1HM ldWCO BVO 9 SNVbl 911b3M0d

:AVM 1MVU0 IdV 9 U3ZI1I8V1S1V0I1U3AzsnaovA8zTZii V3UV asaavi 9 sn »03au3aNnNOI1031Obd

z sna ov nivwl-t>SNvuionvisiidb3MOd:V3bVX03aU30Nn

zsnaovA9z1-8Sll AVI * 113M133HM 3S0NNOIlOSlObdz sna ov nivwl-t>SNVUlOllVlSlldbSMOd

H13M133HM3SONi sna ov A8Zardo11113M133HMNIVWNOUOaiObd

i sna ov nivwb-iSll 1HM IdWOO UVO 9 SNVbl 911B3M0d:S113M133HMNIVW

z sna ov asz1-8Sll AVI 9113M133HM 3S0NNOIlOSlOUdz sna ov nivwi-t>SNVbl 911 VIS lidUBMOd

:AU01VAV1zsnaovA8zl-Zn V3BV bsaavi 9 sn xoaab3aNnNouoaioud

z sna ov nivwi-t>SNVbl 911 VIS lidUSMOd:SS300V N0I1V1S IHOiid

isnaovAszardoS119NiaV01dWVbNOI10310bdi sna ov nivwb-iSll 1HM IdWOO bVO 9 SNVbl 911b3M0d

:9NiaV01 dWVb

z sna oa nivwb-Efsii wbOdivid dwnrWbOdlVld dOOblVbVdsna oa aaiviosiTieHSinONIlXS Sll 11X3 B3W3ONiHSinoNiixa

i sna oa nivwu-zeWUV 9 39UVH011UX3 U3W39NIWbV/9NI9bVH0

11X3 A0N39b3W3LsnaovA8zardo113W00 IdWOO OObVO

t> sna ov nivwu-zin 3woa ldwoo oobvov sna ov nivwb-iSll JLHM IdWOO UVO 9 SNVbl 911U3M0d

z sna oo nivwb"St>Z ON INOO Sll 3W00 OObVOv sna oa nivwb-96I 'ON INOO 113WO0 09bVOlObiNOO

:3W0a

:(ldWOO 09UV0) 9NI1H9H B0IU31NI

(aanNiiNoo) oniihoii

3oanosu3/wodN0I1V001NOiiVNOisaalN3NOdWOOU3MV3U9 linOUlO

t-Otfrt-Ol OI

T01 C-141 C-1

COMPONENT CIRCUIT BREAKER POWER SOURCEDESIGNATION LOCATIONMISCELLANEOUS

AEROMEDICAL EVACUATION AE Q U I P M E N T ^

AEROMED EQUIP FWDAEROMED EQUIP AFT

34-L34-R

MAIN DC BUS 2MAIN DC BUS 1

ALOIS LAMP SIGNAL LT 31-L ISOUTED DC BUSCARGO WINCH CARGO WINCH 8.9,10-R MAIN AC BUS 3COMFORT PALLET POWER COMFORT PALLET 8.9.10-R MAIN AC BUS 3CREW GALLEY FLT STA GALLEY 4,5,6-R MAIN AC BUS 2

UVATORYELECTRIC SHAVER OUTLETTOILET FLUSH

FLUSH UV & ELEC SHAVER OUTLETFLUSH UV

5-R4.5,6-R

MAIN AC BUS 2MAIN AC BUS 2

PERSONNEL WARNING SIGNS PERSONNEL SIGNS 9-L 28V AC BUS 2SERVICE OUTLETS LHSERVICE OUTLETS RH

LH SERVICE OUTLETSRH SERVICE OUTLETS

7,8,9-R4,5,6-R

MAIN AC BUS 3MAIN AC BUS 2

NAVIGATION

ADF NO. 1 ADF NO. 1ADF NO. 1

24-C24-B

AC NAV EXCITATION 1MAIN DC AVIONICS 1

ADF NO. 2 ADF NO. 2ADF NO. 2

8-C8-D

AC NAV EXCITATION 2MAIN DC AVIONICS 2

AHRS ATTD NO.1AHRS ATT 2 /RSP 1 & 2 EXCMAG HDG AHRS HDG NO. 3 & 4MAG HDG AHRS HDG NO. 1,2 & 5AHRS PRIME PWRIJB NO. 1 AHRS CONT

25-C(4-A)38-039-D

(1-A, 1-B, 1-C)(16-A)

AC NAV EXCITATION 126V EMER AC BUS AISOL AC EXCITATIONISOL AC EXCITATIONEMERGENCY AC BUSEMERGENCY DC BUS

INST INDEX TRANS 34-D NAVIGATION AC 1

BDHI PILOTBDHI PILOT

11-A11-B

MAIN DC AVIONICS 2AC NAV 2

BDHI COPILOTBDHI COPILOT

34-B34-C


BDHI NO. 2 NAVBDHI NO. 2 NAV

10-A10-B


AHRS ATT 2/RSP 1 & 2 EXC (4-A) 26V EMER AC BUS A

FAN CONTROL CDS FAN CONT (5-A)EMERGENCY DCEMERGENCY AC

FAN NO. 1 CDS FAN NO. 1 (4-C) (3 PHASEC/B) AVIONICS AC 1

FAN NO. 2PILOTS DAMU

COPILOT'S DAMU

CDS FAN NO. 2DAMU NO. 1DAMU NO. 1 HTRDAMU NO. 2DAMU NO. 2 HTR

13-C(12-C)6-D4-A

30-D

EMERGENCY OCMAIN DC AVIONICS 2MAIN DC AVIONICS 1MAIN DC AVIONICS 1

7E AIRCRAFT MODIFIED BY TCTO 595 ^J


1-466

\ ! ^

% ^ /

TO 1 C-141 C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCED E S I G N A T I O N | LOCATION

NAVIGATION (CONTINUED)

DPU NO. 1 DPU NO. 1/CBC (14-C) EMERGENCY DCDPU NO. 2 DPU NO. 2 5-A MAIN DC AVIONICS 1DU NO. 1 DU NO. 1 3-A MAIN DC AVIONICS 1

DU NO. 1 HTR 32-D MAIN DC AVIONICS 1DU NO. 2 DU NO. 2 (12-C) EMERGENCY DC

DU NO. 2 HTR 13-A MAIN DC AVIONICS 2DU NO. 3 DU NO. 3 2-A MAIN DC AVIONICS 1

DU NO. 3 HTR 31-D MAIN DC AVIONICS 1DU NO. 4 DU NO. 4 (1143) EMERGENCY DC

DU NO. 4 HTR 12-A MAIN DC AVIONICS 2

DATA LOADER 40-B MAIN DC AVIONICS 1DIU 29-B MAIN DC AVIONICS 1FMS REUYS 32-B MAIN DC AVIONICS 1FMS REF 40-C ISOL AC AVIONICS

PILOT'S MFCDU MFCDU NO. 1 41-B MAIN DC AVIONICS 1COPILOTS MFCDU MFCDU NO. 2 36-C MAIN DC AVIONICS 2NAVIGATOR'S MFCDU MFCDU NO. 3 35-C MAIN OC AVIONICS 2

NP NO. 1 42-B MAIN DC AVIONICS 1NP NO. 2 3745 MAIN DC AVIONICS 2

CONTROL PLGR GPS PNL ISOUTED DC BUSPOWER SIGNAL LT 31-L ISOUTED DC BUS

IJB NO. 1 6-A MAIN DC AVIONICS 1IJB NO. 1 14-B AVIONICS AC 2IJB NO. 1 22-A MAIN DC AVIONICS 2

INS-1 /INS-2 36-D ISOL AC EXCITATION

INS-1/CADC-1 23-C 26V AC NAVEXCITATION 1

INS-1 HDG AMP PWR 41-C ISOUTEDAVIONICS AC

MAG HDG INS-1 HDG NO. 3 & 5 40-D ISOL ACEXCITATION 1

MAG HDG INS-1 HDG NO. 2 & 4 41-D ISOL AC EXCITATIONINS NO. 1 PRIME 2243 AVIONICS AC 1INS NO. 1 HTR 22-D AVIONICS AC 1

INS-2/CADC-2 1143 AC NAV EXCITATION 2INS-2 HDG AMPL PWR 6-B NAV AC 2INS-2 MAG HDG NO. 2 &4 643 AC NAV EXCITATION 2INS-2 MAG HDG NO. 3 5-D AC NAV EXCITATION 2INS-2 MAG HDG NO. 5 5-C AC NAV EXCITATION 2INS NO. 2 HTR 14-D AVIONICS AC 2INS NO. 2 PRIME 14-C AVIONICS AC 2

TACAN NO. 1 31-C AC NAV 1TACAN NO. 1 31-B MAIN DC AVIONICS 1TACAN NO. 2 9-B AC NAV 2TACAN NO. 2 9-A MAIN DC AVIONICS 2

VHF NAV NO. 1 38-B ISOUTED DCVHF NAV NO. 1 42-D AVIONICSVHF NAV NO. 2 9-D ISOL AC EXCITATIONVHF NAV NO. 2 943 MAIN DC AVIONICS 2

AC NAV EXCITATION 2/l\ AIRCRAFT MODIFIED BY ICJD_5ZQ


1-467

T01 C-141 C-1

CIRCUIT BREAKERCOMPONENT POWER SOURCE^ "* IVI"P H"hal« ■DESIGNATION LOCATION

OXYGEN

LOX QUANTITY INDICATOR CREW LOX QTY IND 22-R ESSENTIAL AC BUS 2OXYGEN QUANTITY WARNING CREW LOX QTY IND 22-R ESSENTIAL AC BUS 2

ANNUNCIATOR

LOX QUANTITY INDICATORS:CONVERTER NO. 1 TROOP LOX QTY IND NO. 1 CONV 17-R ESSENTIAL AC BUS 1CONVERTER NO. 2 TROOP LOX QTY IND NO. 2 CONV 22-R ESSENTIAL AC BUS 2

LOX QUANTITY WARNING UGHTS:CONVERTER NO. 1 TROOP LOX QTY IND NO. 1 CONV 17-R ESSENTIAL AC BUS 2CONVERTER NO. 2 TROOP LOX QTY IND NO. 2 CONV 22-R ESSENTIAL AC BUS 2

OXYGEN LIGHTS AND HORN TEST TROOP OXYGEN WARN 30-R ISOUTED DC BUSOXYGEN ON INDICATOR TROOP OXYGEN WARN 30-R ISOUTED DC BUS

PITCH TRIM

ELECTRIC & ELECTROHYDRAULICPITCH TRIM:ELECTRICAL TRIM CONTROL ELEC PITCH TRIM CONT 44-R MAIN DC BUS 2ELECTRICAL TRIM CLUTCH ELEC PITCH TRIM CLUTCH CONT 44-R MAIN DC BUS 2CONTROLELECTRICAL TRIM POWER STAB TRIM MOTOR PWR 18,19,20-R ESSENTIAL AC BUS 2TRIM DISCONNECT PITCH TRIM DISENGAGE 39-R MAIN DC BUS 1TRIM RESET:

ELECTRICAL ELEC PITCH TRIM CONT 44-R MAIN DC BUS 2ELECTROHYDRAULIC HYD/ELECPTCONT 38-R MAIN DC BUS 1

HYDRAULIC PITCH TRIM CONTROL HYD/ELEC PT CONT 38-R MAIN OC BUS 1PITCH TRIM INDICATOR HORIZ STAB TRIM POS IND 37-R MAIN OC BUS 1

PNEUMATIC SYSTEMS

AIR CONDITIONING MASTER SWITCH RAM AIR VALVE 32-R ISOUTED DC BUSLH A/C FLOW CONT VALVE 35-R MAIN DC BUS 1RH A/C FLOW CONT VALVE 40-R MAIN DC BUS 2

AIR PRESSURE REGUUTING & S/OVALVES:EMERGENCY PRESSURIZATIONSWITCHES:

LEFT AIR PRESS REG VALVES LH (12-B) EMERGENCY DC BUSRIGHT AIR PRESS REG VALVES RH (11-B) EMERGENCY DC BUS

LEFT SYSTEM SHUTOFF SWITCH LH SYS AIR PRESS. REG & REL VALVES 33-L ISOUTED DC BUSRIGHT SYSTEM SHUTOFF RH SYS AIR PRESS. REG & SHUTOFF 42-R MAIN DC BUS 2

SWITCH VALVES

CARGO COMPARTMENT CARGO COMPT RECIRC FAN 1.2.3-L MAIN AC BUS 1RECIRCUUTION FAN

J

J

^ 0


1-468

TO 1C-141C-1


POWER SOURCEDESIGNATION LOCATIONPNEUMATIC SYSTEMS (CONTINUED)air r*nNnrrinMtMft fCANTiNiiFnv .. . . .

CARGO COMPARTMENT TEMPINDICATOR

CARGO COMPT TEMP IND 41-R MAIN DC BUS 2

EJECTOR ON LIGHTS LH ENVIRON SYS IND LTRH ENVIRON SYS IND LTS

35-R40-R


EJECTOR VALVES LH PRI HEAT EXCH EJECTOR VALVERH PRI HEAT EXCHANGER EJECTOR

VALVE

35-R40-R


FLIGHT STATION AIR FLOW SWITCH AC DIVERTER VALVE 32-R ISOUTED DC BUS

FLIGHT STATION ALTERNATE AIR S/OVALVE

FLT STA ALT AIR SHUT OFF VALVE 41-R MAIN DC BUS 2

LOW LIMIT TEMP CONTROL LH LOW LIMIT TEMP CONTRH LOW LIMIT TEMP CONT

24-R21-R

ISOUTED AC BUSESSENTIAL AC BUS 2

PRIMARY HEAT EXCHANGERCONTROL:LEFTRIGHT

LH PRIM HEAT EXCH CONTRH PRIMARY HEAT EXCHANGER CONT

24-R21-R


PRIMARY HEAT EXCHANGER TEMPIND:EMERGENCY PRESSURIZATION

SWITCHES:LEFTRIGHT

LH SYS TEMP & PRESS. INDRH PRI HEAT EXCH TEMP IND

(14-B)(13-B)

EMERGENCY DC BUSEMERGENCY DC BUS

LEFTRIGHT

LH SYS TEMP & PRESS. INDRH PRI HEAT EXCHANGER TEMP IND

33-L40-R

ISOUTED DC BUSMAIN DC BUS 2

REGUUTED AIR PRESSUREINDICATORS

LH REGUUTED BLEED AIR PRESS IND.RH REGULATED BLEED AIR PRESS. IND

23-L23-R

26V AC BUS 126V AC BUS 2

TEMPERATURE CONTROL SWITCHES:FLT STA CONTROLCARGO COMPT CONTROL

FLT STA & LH LOW LIMIT TEMP CONTCARGO COMPT CARGO & RH LOW LIMIT

TEMP CONT

33-L41-R

ISOUTED DC BUSMAIN DC BUS 2

TEMPERATURE SELECTORS:FLT STACARGO COMPT

FLT STA TEMP CONTCARGO COMPT TEMP CONT

24-R21-R


BLEEO AIR SHUTOFF VALVES:NO. 1 ENGINENO. 2 ENGINENO. 3 ENGINENO. 4 ENGINE

ENG NO. 1 BLEED AIR VALVESENG NO. 2 BLEED AIR VALVESENG NO. 3 BLEED AIR VALVESENG NO. 4 BLEED AIR VALVES

26-R27-R28-R29-R

ISOUTED DC BUSISOUTEDOCBUSISOUTED DC BUSISOUTEDOCBUS

BLEED AIR SHUTOFF VALVE LIGHTS:NO. 1 & NO. 2 ENGINESNO. 3 & NO. 4 ENGINES

MANIFOLD PRESSURE INDICATOR

LH ENVIRON SYS IND LTRH ENVIRON SYS IND LTSMANIFOLD BLEED AIR PRESS. IND

35-R40-R23-R

MAIN DC BUS 1MAIN DC BUS 226V AC BUS 2

LEFT SYSTEM SHUTOFF SWITCHRIGHT SYSTEM SHUTOFF SWITCH

LH SYS AIR PRESS. REG & REL VALVESRH SYS AIR PRESS. REG & SHUTOFF

VALVES334.42-R

ISOUTEDOCBUSMAIN DC BUS 2

LEFT SYS PRESS RELIEF VALVEOPEN LIGHT:

NORMALLH EMERGENCY PRESS SWITCH

LH ENVIRON SYS IND LTLH SYS TEMP & PRESS. IND 35-R

(14-B)MAIN DC BUS 1EMERGENCY DC BUS


1-469

OZfr-t

(1£P 6Z &HS) xtpui ■«*"*<? nn!D Z8I-1 «»*?J

sna oa aaiviosi

sna oa A0N39b3ws

b-ie

(a-ei)

11 ONI MOl SS3Ud NIBVO

ONI dW31 HDX31V3H Ibd Hb

:S1H9I13B0SS3bd MOl NIBVOBOlVOIONI

3BniVU3dW31 U39NVH0X3IVSHAUVWIHdlHOIb

Sna 00 A0N39b3W3(a-u)Hb S3A1VA 93b SS3bd BIV

3A1VAddoinHS 9 oNiivmoaa

3bnSS3bdblVlH9lb:H0UMS1H9IB

sna oa A0N39U3W3(0-8)(a-n)ONI SS3bd 9 dW31 SAS HI

!H9llN3d03AlVAd3H3bSS3bdSASld31

SnaOOAON39U3W3(a-n)ONI SS3bd 9 dW31 SAS HI

bOlVOIONI3bniVb3dW31 U39NVH0X3

1V3H AbVWIbd ld31

sna oa A0N39b3W3(a-zi)HI S3A1VA 93b SS3bd blV

3A1VAddOlOHS 9NllVin93b

3UnSS3bdblVld31:H01IMSld31

:S3H01IMSNOiivziunssaud aonsobsws

sna oa aaiviosia-ieINOO SS3bd NIBVOS3H01IMS

NOiivziunssaudaa aon39U3W3

i sna ov nivwi-zNVd INOO SS3bd NiavoluniN3A9NVd

lObiNOO NOiivziunsssbd Niavo

sna oa asiviosia-ieINOO SSSbd NiavoHOUMS

3aibU3AO uwii aanuiiv Niavo

sna oa asiviosii sna ov iviiNassa

a-zeB-Zl

UMd 1HA0 UOOld O9UV0UMd 1HA0 UOOld 09UV0

U3MOd ONV 1H9I1 !V3Hb3AOb3M0d ONV lObiNOO

sna oa aaiviosii. sna oa nivw

a-zeB-9E

3A1VA ddOJilHS 1V3H UOOld 09UV03A1VA OOW1H UOOld 09UV0

:W31SAS 1V3HU3AO UOOld

HOUMS IVSHHOOld

z sna oa nivwzsnaoviviiN3ss3

i sna ov nivwb-frfr

l-OZ '61 '91i-e'z'i

INOO Z ON NVd 9NI10001V0IU10313Z ON NVd 9NI1000 0313

V ON NVd 9NI1000 lV0lb!0313

lObiNOO Z 'ON NVd 11VWSZ'ONNVdTTVWSV ON NVd TTVWS

ZSnaOVTVIlN3SS3v sna ov nivw

l-0Z'6l'8ll-e'z't

Z ON NVd 9NI1OO0 0INObl0313V ON NVd 9NH0001V0lbl0313

:SNVd TV0lbl0313Z ON NVd 39bVIV 'ON NVd 39bVI

:SNVd OINObl0313

z sna oa nivwz sna oa nivw

b-l>t>b-ot>

INOO 3A1VA MOTd IdWOO 0INObl0313Sll ONI SAS N0UIAN3 Hb

3AlVA10blNOOMOld !N3WlbVdWO0 OINOU10313

S1H9I13bnilVd NVd 9NI1000

sna oa osiviosisna oa aaiviosisna oa aaiviosisnaovasiviosisna oa aaiviosisna ov aaiviosi

b-seb-eeb-eeb-sza-eeb-sz

Hbb3MOdlHA09NIMHI bSMOd 1HA0 ONIMHb b3M0d 1HA0 ONIM

Hb bSMOd !V3Hb3AO 9NIMHI U3M0d 1HA0 ONIM

HI U3M0d 1V3HH3AO ONIM

3QIS1H9IB30ISld31 :S1H9I1

30IS1H9IB

aaisuai :s3hoiims

sna oa aaiviosia-ze3A1VA N0I1VI0SI 9NIM

:W31SAS1V3HB3A0!N3WlbVdWO0 ONINOIliaNOO

BIV ONV 'NOlAd 'ONIM3A1VA N0I1V10SI ONIM

z sna oa nivwb-ot>Sll ONI SAS N0UIAN3 Hb1H9I1 N3dO

3A1VA d3H3U SSSUd SAS 1H9IU

(aanNiiNOO) svoisas ouvwn3Nd

SOUnOS USMOdNOI1V0O1N0I1VN9IS3Q!N3N0dW00 U3*4V3USlinOUIO

t-Otfrl-OtOl

TO 1 C-141 C-1

% ^

^ ^ ^ ^ m ^ w ^ M ^ & ■ j j u b m , S ^ t V

CIRCUIT BREAKERPOWER SOURCECOMPONENT

DESIGNATION LOCATIONPNEUMATIC SYSTEMS (CONTINUED)

OVERHEAT LIGHT RAIN REMOVAL OVERHEAT LT 33-R ISOUTED DC BUS

SWITCH RAIN REMOVAL LH REG VALVE 33-R ISOUTED DC BUSRH RAIN REMOVAL REG VALVE 40-R MAIN DC BUS 2

SWITCH AND OVERHEAT SENSING RAIN REMOVAL SHUTOFF VALVES PLT 33-R ISOUTED DC BUSCIRCUIT RAIN REMOVAL SHUTOFF VALVES COPLT 33-R

RUDDERRUDDER POWER CONTROL

SWITCHES:HYDRAUUC SYSTEM NO. 1 RUDDER CONTROL POWER SYS NO. 1 38-R MAIN DC BUS 1HYDRAULIC SYSTEM NO. 2 RUDDER CONT PWR SYSTEM NO. 2 43-R MAIN DC BUS 2

LOAD LIMIT VALVES RUDDER LOAD LIMIT VALVES 38-R MAIN DC BUS 1

POWER OFF LIGHTS RUDDER CONT POWER IND 30-R ISOUTED DC BUS

SYSTEM POWER ANNUNCIATOR WARN LT TEST & ANNUN CONT NO. 1 26-R ISOUTED DC BUSUGHTS WARN LT TEST & ANNUN CONT NO. 2 27-R ISOUTED DC BUS

SYSTEM HIGH PRESSURE LIGHTS RUDDER CONT POWER IND 30-R ISOLATED DC BUS

RUDDER OVER PRESSURE UGHT RUDDER CONT POWER IND 30-R ISOUTED DC BUS

TRIM RUDDER TRIM CONT 13-R ESSENTIAL AC BUS 1

TRIM INDICATOR RUDDER TRIM POS IND 38-R MAIN OC BUS 1

SPOILERSASYMMETRY SYSTEM:

NO. 2 HYDRAULIC SYSTEM SPOILER ASYMM HYD SYS NO. 2 36-R MAIN DC BUS 1NO. 3 HYDRAULIC SYSTEM SPOILERS ASYMM HYD SYS NO. 3 41-R MAIN DC BUS 2TEST SPOILER AUTO GND TEST 23-L 26V AC BUS 1

CONTROL SPOILER AUTO GRD OPERATION NO. 1 36-R MAIN DC BUS 1SPOILER AUTO GND OPERATION NO. 2 44-R MAIN DC BUS 2HYD SYS NO. 3 SPOILER SOV 45-R MAIN DC BUS 2

FLIGHT LIMIT STOP £± SPOILER IN FLT SOV HANDLE DETENT 45-R MAIN DC BUS 2ARM LT WARN

POSITION INDICATOR:POINTERS SPOILER POS IND. 23-L 26V AC BUS 1LOCKED/UNLKD FUG SPOILER SOV & POS IND 36-R MAIN DC BUS 1

SPOILER CABLE SERVO VALVE HYD SYS NO. 3 SPOILER SOV 45-R MAIN DC BUS 2SPOILER UNDER SPEED LIGHT & STALL PREVENT NO. 1 35-R ESSENTIAL AC BUS 1

AUDIBLE WARNING STALL WARN (OR PREVENT) NO. 2 40-R ESSENTIAL AC BUS 2STOP POSITION INDICATOR SPOILER IN FLT SOV HANDLE DETENT 45-R MAIN DC BUS 2

(HIGH/LOW-FORCE DETENT) ARM LT WARN

WARNING & EMERGENCY SYSTEMSALTITUDE ALERT AUDIBLE TONE FMS REUYS 32-B MAIN DC AVIONICS 1APU FIRE WARNING APU FIRE IND LT 30-L ISOUTED DC BUS

APU FIRE DET CONT UNIT 11-L MAIN AC BUS 4APU FIRE EXTINGUISHING APU FIRE EXT 30-L ISOUTED DC BUSBAILOUT HORN CARGO COMPT WARN HORN (13-A) EMERGENCY DC BUS

MANUAL BAIL OUT HORN 34-R MAIN DC BUS 1

A LABELED "SPOILER MLG INTLK' ON AIRCRAFT 12778 THRU 38090


1-471

TO 1C-141C-1


POWER SOURCEDESIGNATION LOCATION

WARNING & EMERGENCY SYSTEM (CONTINUED)ENGINE FIRE & PYLON FIRE ANDOVERHEAT:

NO. 1 ENGINE

NO. 2 ENGINE

NO. 3 ENGINE

NO. 4 ENGINE

TEST SWITCHES

ENGINE FIRE & OVERHEAT DETCONTROL UNIT NO. 1




AUDIBLE ALARM SILENCE & TEST

254.

25-L

25-L

25-L

31-R

ISOUTED DC BUS

ISOUTED DC BUS

ISOUTED DC BUS

ISOUTED DC BUS

ISOUTED DC BUSENGINE FIRE EXTINGUISHERS:

NO. 1 ENGINE

NO. 2 ENGINE

NO. 3 ENGINE

NO. 4 ENGINE

ENG NO. 1 FIRE EXTENG FIRE EXTINGUISHER NO. 1ENG NO. 2 FIRE EXTENG FIRE EXTINGUISHER NO. 2ENG NO. 3 FIRE EXTENG FIRE EXTINGUISHER NO. 3ENG NO. 4 FIRE EXTENG FIRE EXTINGUISHER NO. 4

26-L41-L27-L41-L284.41-L29-L41-L

ISOUTED DC BUSMAIN DC BUS 2ISOUTED DC BUSMAIN DC BUS 2ISOUTED DC BUSMAIN DC BUS 2ISOUTED DC BUSMAIN DC BUS 2

TCAS/TAWS:

TAWS COMPUTER

TCASTCAPTAWS CMPTR

28-C7-D

22-B

AC AVIONICS BUS 1MAIN DC AVIONICS 2AC AVIONICS BUS 2

LANDING GEAR WARNING HORN & LIGHT LANDING GEAR WARN 32-R ISOUTED DC BUSMASTER CAUTION

ANNUNCIATOR LIGHT WRN LT TEST & ANNUN CONT NO. 1WRN LT TEST & ANNUN CONT NO. 2WRN LT TEST & ANNUN CONT NO. 3WRN LT TEST & ANNUN CONT NO. 4

26-R27-R26-R29-R

ISOUTED DC BUSISOUTED DC BUSISOUTED DC BUSISOUTED DC BUS

RESET MASTER CAUTION RESET 31-R ISOUTED DC BUSMAX SPEED WARNING MAX SPEED WARN 41-R MAIN DC 2TAKE-OFF WARNING TAKE OFF WARNING 38-C ISOL AC AVIONICSTAKE-OFF ANNUNCIATOR TAKE OFF WARN HORN 45-R MAIN DC 2WIND SHEAR WARN AUDIBLE TONE FMS REUYS 32-B MAIN DC AVIONICS 1WINDSHIELD HEAT

CONTROLPILOT'S FRONT WINDSHIELDPILOTS SIDE WINDSHIELDS

PLT WSHLD HEAT CONTPLT SIDE WSHLD HEAT CONT

35-R41-R


PILOTS CENTER WINDSHIELD CTR WSHLD HEAT CONT 41-R MAIN DC BUS 2COPILOTS FRONT WINDSHIELDCOPILOTS SIDE WINDSHIELDS

COPLT WSHLD HEAT CONTCOPLT SIDE WSHLD HEAT CONT

40-R35-R

MAIN DC BUS 2MAIN OC BUS 1

POWER:PILOT'S FRONT WINDSHIELD XMFR PLT WSHLD HTR PWR 1-L MAIN AC BUS 1PILOTS SIDE WINDSHIELDS XMFR PLT SIDE WSHLD HTR PWR 4-L MAIN AC BUS 2PILOTS FWD SIDE WINDSHIELD XMFR

TO WINDOW PWRPILOT SIDE WSHLD TRANS SEC HTR PWR 11-L 52V AC

PILOT'S CENTER WINDSHIELD XMFR CENTER WSHLD HTR PWR 114. MAIN AC BUS 4COPILOTS FRONT WINDSHIELD XMFR COPLT WSHLD HTR PWR 12-R MAIN AC BUS 4COPILOTS SIDE WINDSHIELDS XMFR COPLT SIDE WSHLD HTR PWR 54. MAIN AC BUS 2COPILOTS FWD SIDE WINDSHIELD

XMFR TO WINDOW PWRCOPLT SIDE WSHLD TRANS SEC HTR PWR 124. 52V AC

> ^

S - ^ F

^ j j /

^J

' s ^ /


1-472 Change 1

e_»i

J9MJ jojiuoj piuaiuuojiAuj '£8l~l 9Jn8ij

8E0-CVEX-I-VIH

13NVd nOdlNOO "W±N3l/\JNOUIAN3

t-Otfrt-Ot 01

fri.fr-1

j^N

/S~*>

(pfo i wis) P8I-1 *-<«8tj

NoavzianssgudTvasionaNVdaNvs-Oi--r_

HOIIMS SNIIOOOU31UV1S II3N0Z01

301-UNV 3N9N3r ~ ^ ^~ i

f^/?***•

/^^.UIV 30I-I1NV

HIV 033183UHSS3Ud HOIH

INUONNOUVTOSI

ONIMONI

UIV 03319aiOdlNVIN

SUOIOSPS 1V3Haooidoi

NOI103NN03ONflOBO

W31SAS10U1N00SS3Ud NI9V0

U3_NVHOX31V3HAHVWIUd U OI

W31SASHIV<j_3TgSNIM1HSIU nouj

W3XSASUIV 033TS SNIAA ld31 3H1 ddO SI HOIHM

1V3H UOOTd UOd ld30X31V0llN3ai 3HVSH31SAS dIV Q3319 ONIM 1H0IU ONV JJ3T

/f"j"^_^

SIAI31SAS ONI0I-I1NV QNV UIV 03319 3NI0N3 'lVlN3IAINOaiAN3

t-Otfrt-OtOl

SZfr-t

(pfo z mils) P81-1 ojnSijl-S£0-_tX-l-Vl»t

V_y U0SN3SONI dW31 dW31

IdWOOOObVO

IdWOO09UV0 .

nllli_____-Mtt

3A1VA ddOinHS1VAOW3U

NIVb lOlld

| lHAOJ,0Tld

(0.*9 ddO)OoU NO

(13NVd HOlVIDNriNNV)

| JWOTVAOW5M NWtJ >T_^

iHAOJ.Cn WOO

I I III I IIllllllI I■■■■■»

bOSN3SdW31 iomJt(

/"" wic n

HOUMS 13S1VAOW3U NIVU

J,OTIdO0^v_O

a -r-^ IlOTId

3A1VAddOlOHSlVAOWSb

NIVb lOlldOO

VIS lidVIS lid

WdONMOldblV

VIS lid

oinv1OU1NO0

VIS lid

NOISIAObd lVnNVW H1IM3A1VA ddOinHS 031VU3dO bOlOW<*

39VXNI11V0INVH03W

NOI1O3NNOO1V0IU1O313

U0SN3S 3bniVb3dW31 dOOl SnonNllNOO ■»■__>

NVd 9NllVin0bl03b

NVd ONIlVinOblO

XOfl lObiNOO 0IU10313

U0SN3S1V3HU3AO1V1S0WU3H1lOUlNOO

ro^

H01IAAS 3UnSS3bd MOl ot£y

3A1VA>I03H0 )t^

3A1VA ddOinHS 031Vb3dO AllvnNVW ^^

3A1VA 031VU3dO ATTVOIlVWnSNd ^^f)

3A1VA U010313S 031VU3dO bOlOW C*

3A1VA ddOinHS 031Vb3dO 0I0N310S3A1VA ddOinHS

Q31VU3dO AllVOIlVWnSNdasnouiNoo oionsios

3A1VA ddOinHS031Vb3d0 bOlOW<▶

t-Olfrl-Ot 01

(pfo £ j99ifS) P81-1 sjnSij

9Zfr-t

ONI dW31HOX31V3H AHVIflldd

/^

{?^

f^

l.l--'WW#lU01VUVd3SU31VM

3A1VA103P3HOX31V3HIbd __,...

-S3H01IMSSS3bd30U3IM3 OI

ddO® ®lHSIb ®

JJ31®^'«'1UV1SH109 9N3

U31SVW ONOO HIVONiiona yiv wvu bOd idsoxs awvs 3H1 SI W31SAS ONINOI1IONOO UIV IHOId

3ATVA 9Nll\nn00W 1V3H UOOld

HOUMSH31SVIN NOO blV 3H1AS 03T10U1NOO

3A1VA ddOinHS dIV 31VNd311V NOI1V1SIHOiid (N3dO %8C dO 03SO10) NOIUSOdomi 'aaivuado aoiow v si 3aiva sihi

biv 131NI 3Niaum m||aunixiw dividwoo oodvo-uiv aasia £%_%)

UIV aSNOUIONOO 3dniVb3dW31 [I

V

uiv i3iino 3Niadni _*i_^_HIV 131inO d30NVHOX3 1V3H AdVWIHd

HIVIWdbiv aaais 3bnss3Ud i

HOIH '3aniVH3dlAI31HOIH jNOI103NNOOHIV ONnOHOSS3Hd MOl

l-Otfrt-Ot 01

ZZfr-t

(p to p testis) P8I.-1 aJnBur^

t-Otfrt-Ot OI

TO 1C-141C-1

AIR CONDITIONING MASTER SWITCH POSITION CHARTCOMPONENTS

AFFECTEDAIR CONDITIONING MASTER SWITCH POSITION

APU ENG START BOTH LEFT RIGHT OFF RAMSYS AIR PRESS.

REG VALVES AS SELECTED CLOSED AS SELECTED AS SELECTED AS SELECTEDCLOSED

A A AS SELECTED

PRIM HT EXCHEJECT

S/O VALVESCLOSED POS BY CADC POS BY CADC POS BY CADC POS BY CADC POS BY CADC POS BY CADC

LH AIR CONDFLOW CONT AND

S/O VALVESOPEN POWER OFF OPEN OPEN CLOSED CLOSED CLOSED

RH AIR CONDFLOW CONT AND

S/O VALVEOPEN POWER OFF OPEN CLOSED OPEN CLOSED CLOSED

LH TURBINEBYPASS VALVE

CONTROL-LING POWER OFF CONTROL-

UNGCONTROL

LING POWER OFF POWER OFF POWER OFF

RH TURBINEBYPASS VALVE

CONTROLLING POWER OFF CONTROL

LING POWER OFF CONTROLLING POWER OFF POWER OFF

LH TEMP CONTROL VALVE


LINGCONTROL-

LING POWER OFF POWER OFF POWER OFF

RH TEMP CONTROL VALVE


LING POWER OFF CONTROLLING POWER OFF POWER OFF

FLT STA ALT AIRSHUTOFF VALVE CLOSED CLOSED CLOSED CLOSED 38% FLT STA CLOSED CLOSED

PRIM HT EXCHCOOL AIR .

CONT VALVECONTROL

LINGCONTROL

LINGCONTROL

LINGCONTROL

LINGCONTROL

LINGCONTROL

LINGCONTROL

LING

FLOOR HEATSHUTOFF VALVE OPEN OPEN AS SELECTED AS SELECTED AS SELECTED AS SELECTED AS SELECTED

FLOOR HEATMOO AND

SHUTOFF VALVEAS SELECTED CLOSED AS SELECTED AS SELECTED AS SELECTED AS SELECTED AS SELECTED

BLEED AIR WINGISOUTION

VALVEOPEN OPEN AS SELECTED AS SELECTED AS SELECTED AS SELECTED AS SELECTED

BLEED AIR SHUT-OFF VALVES CLOSED AS SELECTED AS SELECTED AS SELECTED AS SELECTED AS SELECTED AS SELECTED

RAM AIR VENTVALVE CLOSED CLOSED CLOSED CLOSED CLOSED CLOSED OPEN

FLT STA TEMPSENSOR AND

FANPOWER ON POWER OFF POWER ON POWER ON POWER OFF POWER OFF POWER OFF

CARGO COMPTTEMP SENSOR

AND FANPOWER ON POWER OFF POWER ON POWER OFF POWER ON POWER OFF POWER OFF

CARGOCOMPTRECIRCULATION

FANPOWER ON POWER OFF POWER ON POWER ON POWER ON POWER OFF POWER OFF

CABIN PRESS.CONT FAN AND

VENTURI

POWER ON(GROUND

ONLY)POWER ON

POWER ON(GROUND

ONLY)

POWER ON(GROUND

ONLY)

POWER ON(GROUND

ONLY)POWER ON POWER ON

CABIN ALT LIMTSOLENOID VALVE

CLOSED CLOSED CLOSED CLOSED CLOSED CLOSED OPEN

A ON 38075 AND UP. IF RAIN REMOVAL SWITCH IS OFF, SYSTEM AIR PRESSUREREGUUTOR VALVES WILL BE CLOSED, OR AS SELECTED WITH RAIN REMOVAL ON.

A ON 12778 AND 12779 FOR RAIN REMOVAL TO BE OPERATIONAL, THE AIR CONDITIONINGMASTER SWITCH MUST BE IN THE BOTH, LEFT OR RIGHT POSITION.

Figure 1-185. Air Conditioning Master Switch Position Chart

1-478

6Zfr-l

981 I 9-inSij

iai31sas loaiNOO 3anss3dd Niavot-Otfrt-OtOl

f*

08fr-l

umfj apmmv 9jnss9Jj wqoj 'isi'l «"'??_'

^

//^

ao-c/Ex-i-vm

os of se oe(133d dO SONVSnOHl)

3aniu.iv_dVb0biv92 OZ SL01IS i-

^^^^^p.S^^^^S'^^î^^P

NOIUSOdassoio 3Hi ni asuvd satva Moidino

3no hum aisd 98 do wnwixvw V OI3SV3U0NIAVW 3bHSS3bd lVllN3b3ddia ^7

(9ISd S'S) 3A1VA MOldinO 9NIN3dOSNI93S lObiNOO 3UnSS3Ud lVUN3U3ddia W

iouinoo iiwn 3aminv nibvo *""7

#^.

idVHO 3annnv 3anss3dd Niavol-Otfrt-Ot 01

t8fr-l

881-1 9jn8ijOMj-0/CX-l-VlH

ddO S0NO03S Ol-NO SON003S S3toao Aina luvis otoo

J.UVJ.S OTOOiUViS OTOO1UV1SOTOO

loiidoo ~*a?vaimo ioiidTVWUON y--^ TVWUON

ddO (JUW ddOHSIH HOIH

-1V3H 013IHSQNIM •NO

ddO

lOTIdOOiOTId

|g3j.Tnvdtij""" |03iTrwdtjj"""30130 M0V11V dO 310NV

•ddO

lOTIdOO•lOTId

HIOS

[iHAOlTd-QO." |XHAOJJd.|

"1VAOW3H NIVb

13NVd 10U1NOO SI/\I31SAS ONIOhllNV

1-0 tfr 1-0101

(£fo i wus) '681-1 «»*.»_■

Z8fr-l

f^

^

dnndonnvuoAHN3AIU0 3NION3

dwndisooaNOIlOnS N3AIUO

-01OW3IU10313

U311IIAISNVU13anSS3dd hum]

3A1VA Nivaa031VU3dO ATWINVW

■OB

T—10W

30V)INn-|V0INVH03nNOUVniOV TV0IU10313

SSVdAS HUM U311ld JJ5*

_cceo 30V0 0Niav3U-103Uia Q

3A1VA ddOlHHS031Vd3dO aoiow

3A1VA dJOlflHS031Vd3dOQION3TOS

U311U

U010ldlS3d AVM OMI ^j""""^

3AlVAd3ll3U ////▶;

3ATVA X03HO |\\\tj>]

ussanNS *%T,

3TONVH10U1NOOAON30d3N3 3dld

HOUMS 3UnSS3dd O

HOUMSS3A1VAf ON 9N3

UO1V0I0NI3dnSS3Ud

U01VA3T3U3aanuN0-31IV

asnddns.SN31SAS.

WOHd

I. ON iVM31SAS

si/\i3isAsonnvaaAH

uaiiid uiv

3UHSS3-ddwid isooa nouohs

033d A1IAVH0

Nuruauiaqisas HI!

3UDSS3Ud W31SAS

NOI103NNO0lS31QNnOUO

^h-bHj;ion

1N3A 03U311ld HUMMNVlMO!dU3AO

UI0AU3S3UI ON W31SAS

¥t-Otfrl-0101

£8fr-t

(£fo z i99us) 681-1 »-"*8ld

39V3H1IMuoivrnwnoov

iJO10IUiS3U AVAA OMidnrtd

OnnVUOAHNSAIUOUOIOW 0IU1O3T3uassnNS

dtww isooaNOIiOnS N3AIUQATwonnvuaAH

U311IHSNVH1 3UnSS3Ud

SATVANWUCm iwu3 jn jn-iwnwvw ><§)< «-.

dwrtd onnvuaAH nTN3AIU03NISN3 "11 3ATVAddOinHS

«-—1031VU3dO UOIOWdwrtdisooeffih Notions NSAitjo

UOION OIH103T3J.V.3ATVAddOJJTHS

O31VH3dO0ION3TOS

EST"1ri& i

SSVdA9HJJMU3nid

H311ld

UOlVTCOSHMOTd |)S-|NOIlVni0VTV0ldlO3T3

3SV9 SNIOV3U1331110

H3UAAS3UnSS3tJd

3T0NVH TOUINOOA0N3OU3W3 3U1J

3SVXNIT1V0INVH03W

■©

©

U31Tld UIV

asrtd onnvuaAH

3ATVAd3IT3U

3ATVA3I33H3

3UnS53Ud A0N39U3N3

C ON W31SAS'3UnSS3Ud dnndONVH

Z ONH31SAS-unsssud

dnnd isooa Notions

AT3All33dS3UG ON 'Z ON W31SAS

033d>aiAVH3

AT3All03dS3UG ON 'Z ON H31SAS

NUniSU W31SAS

AT3AU03dS3U'C'ON'ZONWSISAS

3UnSS3Udn31SAS

<3>

m

ID

t-Otfrt-Ot 01

T0 1C-141C-1

SYSTEM NO. 3

TWO-SECONDTIME DELAY

REUY

TO NO. 1 PUMP SWITCHRAMPwOFF ON RAMP CONTROL PANELCONTROLNO. 2 PUMP SWITCH

°^- TO NO. 2 PUMP SWITCHOFFRAMP

CONTROLON RAMP CONTROL PANEL

rjLT\ PRESSUREINDICATOR

PRESSURE DOORPETAL DOORSLOADING RAMPELEVATOR

FUPSWING SPOILERSAILERON TABCONTROL LOCKOUT

^ )

^ J

A VALVE IS DE-ENERGIZED OPEN.

A VALVE OPENS WHEN PUMPS ARE TURNED ON. CLOSED*—^WHEN PUMPS ARE SHUTOFF.

A CASE DRAIN RELIEF VALVE SET TO RELIEVE AT APPROXI-Z—iMATELY20 PSI.

^SET TO RELIEVE AT APPROXIMATELY 3,560 PSI.A ALSO FILTER RETURN FLUID FROM LANDING GEAR, PITCH-"^TRIM, EMERGENCY GENERATOR, WHEEL BRAKES AND

WING FLAPS.

A ALSO FILTERS RETURN FLUID FROM PETAL DOOR MOTOR-—ÂND WING FLAPS.

A OVERFLOW VENT TANK IS SHARED BY NO. 2 AND NO. 3"—^HYDRAULIC SYSTEMS.

Figure 1-189. (Sheet 3 of 3)

1-484

S8fr-t

j9uoj joivoipuj puv jojjuoj stu9is<s oijntupKff '061-1 *"*8tj

r\

-&

dnru\ » iSOOB'oie ions

. S3ATVA\i c

OW3

IWOT SS3Ud|MOT SS3tJd|AAOT SS3Ud|

y/TX ^SinvA dnrtd jf^siATvA/ o....' T (tS 8 1S0C4 K 31 » L. *-1J ^g>eia ions 'Sg' eraXj^v' |MOT SS3Md|MOT SS3Md|MOT SS3tfd)

ore 0NO39SOHinit3M>43t

nov^^' NOiinvs dHftdlON /g§.

tonsnaisASonnvMOAH

^1

13NVd HOIVOIQNI QNV 10U1NOO SIA131SAS OlinVdQAH

t-otfrt-oi Ol

TO 1C-141C-1

FLIGHT CONTROLS SYSTEMS

PILOTSCONTROL WHEEL'QsxS) qj\S)

TENSION REGULATORS

AILERONSYSTEM

A

COPILOTSCONTROL WHEEL

«-TENSION REGULATORS

SHEAR PIN

/ ARTIFICIALFEEL SPRING

J050H-AILERON POWER■ |_J O LU' CONTROL ASSEMBLY' - r - - 5 * — | - J

AILERON POWERCONTROL ASSEMBLY

r - a r - - 7 - i

PRESSUREAILERON AILERON

AILERON TRIMINDICATOR

RIGHT AILERONSYS NO. 1 POWERCONTROL SWITCH

NORMAL

AILERONTRIM

SWITCHES

RIGHT AILERONSYS NO. 2 POWERCONTROLjjWITCH

TAB OPERABLEOFF

NORMAL

Figure 1-191. (Sheet I of 4)

1-486

Z8fr-l

(Pfo Z w/S) 161-1 9jn8ij

(use)dsxvsuaimouo

S3ATVAlllAjnovoiusaanu

(hop)u3xv3uaiinoaio

ONI U3MOdinoo Hsoana

3UnSS3bdJI '

|SS3HdH3AOIusoona

sunsssad

HOUMStoaiNOoU3AAOd

Z ON SASU3aanu

Aasaanu

x i

mZSEtEtnaHOUMS

1OU1NO0 U3MOdI ON SASasoanu

OAU3Susdiwa aava

ONIUdST33dlVIOIdllUV

Nld HV3HS

AiawassvioaiNoo [j"""| 171u3MOd usaana , L-i l—JOAU3S

U3dlW0 MVA

IAI31SASusaana

sivasdi usaana s.ioiidoop STV03d 'u3canasj.oiid

l-0tfrt-0tOl

88fr-l

/^•fc

x^-S

/*"*

,>/o £ t99us) 161-1 9Jn8ij

^\

f^

^** ^jaSj^g^S^T

uoivniov, U01VA3T3.fA0N30d3H3

I I1 l:« 'j? . , j jh

Et mr "'''Uwuw'w m ^lEJûoivniov; I" , * J/f "r **1 " fl , >*) ,-jWif U01VA313/]

3UnSS3Ud W31SASA0N30U31N3

K'-j, f'lii'-miSiti-^

iaoivniov'luoivAjraferni n

§mfvrr.*" ^3."

3 ONoavo

H31dV0V31VU HOlId

.at'ONOOVO

NwmooTOUINOO SJ-OlldOO

[7t=f7l [b"*7| ATBH3SSV TOUINOO■WITILJ.Lr^-L U3MOd aO!VA313

- S.XNVU0T13S

IAI31SASU01VA313oaubs

loiidOinv

^=*& SHOivrnosu N01SN31

(?v5)Nld

UV3HSSH3MVHS-

ONINaVMTTVlS(PWNwmoo

10U1NOO SJ.OHd

l-Olfrl-Ol 01

HYD PITCHTRIM LEVER

AUTOPILOT

MODULATINGVALVE

PITCH TRIMSYSTEM

ELECTRICMOTOR

CLUTCHES

B KHYDRAULICV M O T O R

DRAIN

ELECTRIC ANDELECTROHYDRAULICPITCH TRIMRESET SWITCH

T0 1C-141C-1

HORIZ STAB. TRIMPOSITION INDICATOR

SCREWDRIVE

NUTDRIVE

ELEC PITCHTRIM SWITCHES POSITION

ITRANSMITTER

<z

PITCH TRIM ACTUATOR ASSEMBLY

HORIZONTALSTABILIZER

PITCH TRIMDISCONNECT BUTTON

ELECTROHYDRAULICPITCH TRIMSWITCHES

m

HYDRAULIC SYSTEM NO. 1 PRESSURE

HYDRAULIC SYSTEM NO. 1 RETURN

HYDRAULIC SYSTEM NO. 2 PRESSURE

HYDRAULIC SYSTEM NO. 2 RETURN

HYDRAULIC SYSTEM NO. 3 (EMERGENCYSYSTEM)PRESSUREHYDRAULIC SYSTEM NO. 3 RETURN

MOTOR OPERATED SHUTOFF VALVEAND BYPASS VALVE

SOLENOID OPERATED SHUTOFF VALVE(DE-ENERGIZED)SOLENOID OPERATED TAB LOCK VALVE(SHOWN DE-ENERGIZED)

& &PRESSURE SWITCH

SERVO. FLOW CONTROL VALVE

:^~P" RELIEF VALVE IF TO PRESSURE

j^ ANTI-CAVITATION VALVE IF TO RETURN

T - i

^ CHECK VALVE

C RLTERfWWEi LOAD LIMITING RELIEF VALVE

SOLENOID OPERATED PILOT VALVE(SHOWN ENERGIZED)

MECHANICAL ACTUATION

ELECTRICAL ACTUATION

ELECTRICAL POWER INPUT

/A,HH AILERON SYSTEM SHOWN. LH TYPICAL

^COPILOTS CONTROL WHEEL, PILOTS SIMILAR

ÂjHE INDICATOR REFERENCES NOSE-UPAND NOSE-DOWN OF THE AIRCRAFT

/MÔNE ADDITIONAL SHEAR PIN IS LOCATED INTHE ARTIFICIAL FEEL MECHANISM ONAIRCRAFT NOT MODIFIED BY TCTO 716/805


1-489

j99UA\!OJtuoj WIwSlJ

oefr-t1

a io*6szcaH01IMS SNOHdOdOIN SNOiina aNnoMv-oo/NOULViOb >

NOiina i03NN00Sia niHi HOiid cNOiina io3NNOosia loiuoinv z

S3H01IMS MidiHOlId 0nnVU0AH-0>J10313 i

^

$^^

misoddo s.ioiidoo NMOHS 133HW TOdlNOO SJ.01ld t

133HM10U1NOO

l-Olfrt-Ot 01

TO 1C-141C-1

i SOLENOID! OPERATED; TORQUE TUBE1 BRAKES A

RWOUTBD

% ^

%»/HYDRAULIC SYSTEM NO. 2 PRESSURE

"TUI HYDRAULIC SYSTEM NO. 2 RETURN

SI HYDRAULIC SYSTEM NO. 3 PRESSURE

LLUJ HYDRAULIC SYSTEM NO. 3 RETURN

MECHANICAL ACTUATION

ELECTRICAL ACTUATION

A SYSTEM SHOWN WITH FUPS BEING RETRACTED.A. INFLIGHT MOVEMENT OF THE WING SPOILERS FROM

THE RETRACTED POSITION. OR LOSS OF ELECTRICALPOWER AT ANYTIME. DE-ENERGIZES THE SOLENOID.ENGAGING THE STOP.

A. LOSS OF ELECTRICAL POWER IN THE ABSENCE OF ANASYMMETRIC CONDITION LEAVES THESE NORMALLYDE-ENERGIZED SOLENOIDS DE-ENERGIZED. AND THEFLAP SYSTEM REMAINS OPERATIONAL. BUT THEASYMMETRY PROTECTION SYSTEM IS RENDERED IN-OPERATIVE.

A SWITCH ACTUATES IF FLAP CONTROL CABLEBREAKS.

A 10 6PM NOMINAL TO PREVENT FLAP MOTOR OVERSPEED.

Figure 1-193.1-491

Z6fr-l

/$""*>

f*

j^^

^

^*>

(£fo i }99U$) P61-I 9jn8;j

W31SAS OAH Z ON dO SSOlbatyaW

UEU07I3S =—

AVISOTOUINOO

AtuannAsv

ONHVU3dO-lM31SAS OAH 6 ON ONV Z ON3ATVA V

Aran 30U1N03soisidatnobj

Oil

3XSWHUY30

ONtONVI

SASOAM

uaiLinsfwuiKOUISOdUJliOdS

L?o

IAI31SAS U31IOdS ONIM

1-Otfrl-OtOl

86fr-t

(£fo z wtIS) P61-I 9jn8tj

W31SAS OAH E ON JO SSOI3AT*aW

UOi33T3S -—OAU3S ,

ONIlVbSdO'HSlSAS OAH e ON ONV Z ON

AV13UTOUINOD

AtU3nWASV30151:131 nOUJ

SASOAH

C ON

T3NVdU3W>1

32 Z/12

to13NVdUBddn

• mmMOlSId

UBdSNVtU

3TCNYWav30

ONIONVT

■ , ; NOisidj»°l O U3JSNVU1

SASOAH

JON

l-0tfrl-01 01

fr6fr-t

(£fo £ i99us) P61-1 9Jn8lJ

f-^

3«niV3d 10VU13Ud31IOdS .t>S 3H11V3330 HIM MS

!V3d3Q ICVdlBd Oinv dSHOdS :3!ON

°xJNQe# ?Z#10VH13H

oinv usiiods ot> s

c<|dne# ?z#iiinin

IHOiid USVd .S

3WI1ANVe#(HOUMS 03H3)

ddO H3W3

3WI1ANVe« 9Z#(HOUMS 03U3)10VH13U U3IM3

3WI1ANVe# t?2*.WE 'SA .2/1 Z•B

:QNO0SAS OAH:|AJ3XSAS AdlSWWASV d31IOdS 3HX

NOIlVniOV 1V0INVH03 w

NOUVniOVlVOIH10313

Ndni3d C ON IAJ31SAS onnvuaAH |TB

sunsssdd e on wsisas onnvuaAH |

NdfUSd Z ON IAJ31SAS OlinVdOAH |

3UnSS3dd Z ON IAJ31SAS OlinVdOAH H(NOIUSOd N3dO 0103ZI0H3N3 NMOHS) ,#-*.

3A1VA UO10313S 0AU3S 031VH3dO 0ION31OS |U

3A1VA ddOinHS Q31Vb3dO AllvnNVIM A

JJIMI1 ONOOdO

10VU13U USIIOdS .5

uwniid

V

1N313030UOd HOIH

Q3S010

13S3H

S3H01IMS 1IWI1 H3A31 dSHOdS 01^7■310NVH U31IOdS 3H1 OI 30VMNI11V0INVH0__,•3W A8 031VU3dO SI 0AH3S 31BV0 H31IOdS N^

Nouisod do inoSI dOlS 1IWI1 IHOiid 1V0INVH03W 3H11N3A3

3H± Nl 310NVH 3H1 dO NOHOW OldVd OIOAVIHOiid ONiuna saNnod (i*) s si SNomsod

31VI03Wd31.NI 11V1V SOtlOd 'SONnOd U*)9fr SI 03Uin03U 30U0d 3H1 '30Vld Nl 1N3130

30UOd HOIH 3H1 HUM SONnOd (2*) 21 SINOIUSOd 03S010 3H1 WOUd U3A31 3H1 3AOW

OI 03din03d 30U0d 3H1 '03A0W3U 1N3130,30H0d HOIH 3H1 QNV 031dll 31QNVH 3H1 HUM \^

OSldll SI 310NVH HSIIOdS 3H1 ONV'SHnOOO NMOOHOnOl N3HM aiON310S dSllOdS

aNnouo 3Hi as Aiivouvwoinv 03aow__,-3d SI dOlS 1IWI1 IHOiid 1V0INVH03W 3H1 \y

doivniov dsnods advos•ino 3H1 dOd 3ndl SI 3Sd3A3d 3H1 W31SAS

onnvdaAH e on wodd 3dnss3Hd A8aNvis__-S3AI303d dOXVniOV d31IOdS OUVOBNI ^

NOIUSOd dn 3H1 Nl SI d3A31 HV39,0NI0NV1 N3HM a3ZI0d3N3 S0ION31OS IHOIldNI >^

lVOIdAl W31SAS d31IOdS HI-—,NMOHS IAJ31SAS d31IOdS HdNy

l-01frl-0t01

S6fr-l

(£ fo i i99ifs) S6I-1 ««»U

c-6»o*o/ox-t-at»i

Nomsod nmoo und3H1 03H0V3d 3AVH S30Vd9

OVdO 3H1 dSldV 03ZIOH3N33W003B S3A1VA 0ION31OSuoivniov jiooi nmoo shi v

S3H01IMS 1IWI1 0311OdlNO0oiw as asivniov

'asivdSdo onnvdaAH/aioNsios Vxoa lOdiNoo

aixs-iiNV 3Hi do sunodio0NISN3S NOIlVlOd NON ONV9NISN3S NOIlVd313030 3H1

aq asnodiNoo si saiva vlVOIdAl W31SAS

3HVd8 133HM Hd 'NMOHSW31SAS 3>iVda 133HM HI V

NOIUSOd NMOO 3H1Nl NMOHS dV30 ONIQNV1 V

govMNmvoiNVHoamNOIlVniOV-|VOIH103*13

U013IU183U

aaonaau 3unss3Ud

3A1VA SSVdA8 aNOOUOQ31Vd3dO ATTVnNVW

3A1VA UO10313SasivdSdO AiivnNvm

NOISIAOUd IVflNVIfl HUM3A1VA U010313S

a31VU3dO 0ION31OS(NMOHS SV 03ZI0U3N3

-30) 3A1VA 0I0N310S^ ONidwna 3unss3dd

(NMOHS SV 03ZIOU3N3-3a)3AlVAOION310S

^ ONiivinaow sunsssydU311IIMSNVU13UnSS3bld fejW]

HOUMSAi3dvs asivniov inuis

U311ld

3A1VA 311inHSuoi\nno3u moij

3A1VAM03H0useanNS

3snd3UnSS3bld A0N39U31AI3 01N3unss3Ud loyiNOo 3»vya

3unss3Ud 3>ivya(0310313SW31SAS

NO ONION3d3a) 3dnSS3dd3MVU8 A0N30y3IM3 yO TVWUON

Nunisy z on wsisas oah3dnSS3Ud Z ON W31SAS OAH

033d A1IAVU0 Z ON W31SAS OAH3UnSS3yd 3NI1

dn avso onionviNunisy e on itoisas oah

3dnss3yd 3MvygA0N30y3W3/E ON IN31SAS QAH

//*

mm

□inn

1

QN3031IAI31SAS HV30 ONIQNVl

1-0 tfr 1-01 01

T0 1C-141C-1

LANDING GEAR SYSTEMSRUDDERPEDALS

STEERINGWHEEL

RIGHTSTEERINGCYLINDER

TO NLG EMEREXT SYS

HAND PUMP

\ ^

MLG DOORLOCK SELECTOR"

VA LV E ^

RIGHT MAIN GEARDOWNLOCKACTUATING1 CYLINDER

RIGHT MLGDOOR LOCKACTUATINGCYLINDER

^ j


1-496

Z6fr-1

(i'fo C W''»'/S) V6/"/ 9jn8ij

tflffijinojao aixs>HNV

r>i

isaqims

r\

3XVU8133HM

Q8NI OMd HI

3XVU9133HM

130aixs

asino OMd hi

130aixs

r\

3XVdS133HM

aaino uv hi

o o jHHimSf o3XVHS133HM

xoalOdlNOO

Z| aixs-iiNV

130aixs

09NI IdV HI1S31 QNO

1 IMyHUBTq

ddONO

t t ♦ " " t T ''S3A1VA

0ION31OSONidwna

3dnSS3Ud ONVONiivinaow

3dnSS3Ud OI

HOUMSaixs-iiNv

IA1HON

l-Olfrl-0101

961-1 m»8ij

86fr-l

/^\y3iiid

3AlVAd3ll3d ,SS»;

3A1VAM03H0 ,SS»,

H010ldlS3dAVM OMI

3ovo oNiavsy-iosyla <g)

c3A1VA yO10313S

031VU3dO ATlVnNVW

3A1VA Nivyaa31Vd3dO AllVONVW

Nyni3H in3isas [HI

synsssyd AON3oy3W3 jj^

Q33d AllAVdO

W31SASyV30 ONIONV1 *$#######£#*###»#»#■&

3SON 01 $######### A>#»###A/M&77_

IAI31SAS 0N31X3 A0N30H31AI3BV30 9NI0.NV1 3S0N

aiinr

NIVHO

UIOAB3S3d11X3 y3W3 01N

1N3A

=^

l-Otfrl-Ol 01

66fr-t

(Zf° I &*MS) J°9D 8mpuirj swa/ '161-1 9Jn8tj

NOINNndlJJldlSXOOHS 81(HOOO OdVMdOd Hd) XNVdOTBB L \

(dOOaidV)XNVH0113aHd "91HOlvniOV SNId331S SI

A18W3SSV 3UI1 ONV 133HM HH > IHOOO OdVMdOd HI Xi

(uooa auvMdOd hi) xNvuonsa 21A18W3SSV 3dll ONV 133HM HI 11

(uooaidv)xNVdon38Hi oi

dOOOldV 6S9NIUV3S 8

A18W3SSVWdV3nOd01 LWSINVH03WX0OlNMOa/dn 9

HOivniovonnvdOAH sNOINNndl >

A18W3SSV 30VH8 OVdO edOivniovxooiNMoa/dn z

inHlSXOOHS I

/*%

■^

UV30 9NIQNV1 3SONt-Olfrl-Ot OI

T01C-141C-1

^ )

LEFT WHEELREMOVED FORCLARITY

1. RIGHT NLG CRANK2 UP/DOWN LOCK ACTUATOR3 NLG POSITION SWITCH NO. 24. NLG POSITIVE DOWNLOCK

SWITCH5. LEFT NLG CRANK6 UP/DOWN LOCK PUSHROD

7 UP/DOWN LOCK LEVER8 UP/DOWN LOCK EMERGENCY

RELEASE HANDLE9. FILLER VALVE

10 DRAG BRACE ASSEMBLY11. SPHERICAL BEARING12. BEARING

13. NLG TRUNNION14. BEARING15. DISCONNECT PINS16 TORQUE ARM ASSEMBLIES17. NLG ACTUATOR18. SPHERICAL BEARING19 SHOCK STRUT TRUNNION2 0 . S H O C K S T R U T , „ , „ „ „ „21. NLG UP/DOWN LOCK SWITCH

-■ 0

Figure 1-197. Nose Landing Gear (Sheet 2 of 2)

1-500

Documents

C-141C Dash 1 011 1- 451-500