International Space Station Assembly Operations … space station assembly operations book - 3a ......

JSC-48502-3A

International Space StationAssembly Operations Book

ISS-3A

Mission Operations DirectorateOperations Division

Final, Revision ASeptember 21, 2000

National Aeronautics andSpace Administration

Lyndon B. Johnson Space CenterHouston, Texas

United StatesSystems Operations Data File JSC-48502-3A

INTERNATIONAL SPACE STATION

ASSEMBLY OPERATIONS BOOK

ISS-3A

FINAL, REVISION ASeptember 21, 2000

APPROVED BY:

___________________________________________Michael Halverson

Book Manager

_____________________________ _____________________________Joseph H. Cavallaro Debbie D. Stapleton

Lead, Cargo Support Operations Chief, Cargo Integration andGroup Operations Branch

___________________________________________Kent H. Adams

3A SODF Coordinator

ACCEPTED BY:

___________________________________________Michael T. HurtSODF Manager

This document is under the configuration control of the Systems Operations DataFile Control Board (SODFCB).

United StatesSystems Operations Data File JSC-48502-3A

21 SEP 00 ASSY OPSii

Incorporates the following:

CR: Assy_OpsU52AAssy_OpsU57Assy_OpsU58Assy_OpsU59Assy_OpsU60Assy_OpsU61

Assy_OpsU62Assy_OpsU64Assy_OpsU65Assy_OpsU66Assy_OpsU67

∗ - Omit from flight book

21 SEP 00 iii ASSY OPS

INTERNATIONAL SPACE STATIONASSEMBLY OPERATIONS BOOK - 3A

LIST OF EFFECTIVE PAGES

FINAL 26 JUN 00REV A 21 SEP 00

Sign Off .......................... ∗ 21 SEP 00ii ..................................... ∗ 21 SEP 00iii..................................... ∗ 21 SEP 00iv .................................... ∗ 21 SEP 00v ..................................... ∗ 21 SEP 00vi .................................... ∗ 21 SEP 00vii.................................... 21 SEP 00viii ................................... 21 SEP 001 ..................................... 21 SEP 002 ..................................... 21 SEP 003 ..................................... 21 JUN 004 ..................................... 20 SEP 005 ..................................... 22 JUN 006 ..................................... 20 SEP 007 ..................................... 21 SEP 008 ..................................... 21 SEP 009 ..................................... 19 SEP 0010 ................................... 19 SEP 0011 ................................... 19 SEP 0012 ................................... 20 SEP 0013 ................................... 19 SEP 0014 ................................... 20 SEP 0015 ................................... 19 SEP 0016 ................................... 19 SEP 0017 ................................... 16 SEP 0018 ................................... 20 SEP 0019 ................................... 16 SEP 0020 ................................... 20 SEP 0021 ................................... 21 SEP 0022 ................................... 21 SEP 0023 ................................... 19 SEP 0024 ................................... 19 SEP 0025 ................................... 19 SEP 0026 ................................... 19 SEP 0027 ................................... 19 SEP 0028 ................................... 20 SEP 0029 ................................... 19 SEP 0030 ................................... 19 SEP 0031 ................................... 19 SEP 0032 ................................... 19 SEP 0033 ................................... 19 SEP 0034 ................................... 19 SEP 00

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128 .................................. 23 JUN 00129 .................................. 23 JUN 00130 .................................. 20 SEP 00131 .................................. 22 JUN 00132 .................................. 20 SEP 00133 .................................. 23 JUN 00134 .................................. 23 JUN 00135 .................................. 23 JUN 00136 .................................. 23 JUN 00137 .................................. 21 SEP 00138 .................................. 21 SEP 00139 .................................. 23 JUN 00140 .................................. 23 JUN 00141 .................................. 23 JUN 00142 .................................. 20 SEP 00143 .................................. 12 SEP 00144 .................................. 20 SEP 00145 .................................. 20 SEP 00146 .................................. 20 SEP 00147 .................................. 20 SEP 00148 .................................. 20 SEP 00149 .................................. 20 SEP 00150 .................................. 20 SEP 00151 .................................. 20 SEP 00152 .................................. 20 SEP 00153 .................................. 20 SEP 00154 .................................. 20 SEP 00155 .................................. 20 SEP 00156 .................................. 20 SEP 00157 .................................. 20 SEP 00158 .................................. 20 SEP 00159 .................................. 20 SEP 00160 .................................. 20 SEP 00161 .................................. 20 SEP 00162 .................................. 20 SEP 00163 .................................. 20 SEP 00164 .................................. 20 SEP 00165 .................................. 20 SEP 00166 .................................. 20 SEP 00167 .................................. 20 SEP 00168 .................................. 20 SEP 00169 .................................. 20 SEP 00170 .................................. 20 SEP 00171 .................................. 20 SEP 00172 .................................. 20 SEP 00173 .................................. 20 SEP 00174 .................................. 20 SEP 00175 .................................. 20 SEP 00176 .................................. 20 SEP 00177 .................................. 20 SEP 00178 .................................. 20 SEP 00

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This Page Intentionally Blank

21 SEP 00 ASSY OPSvii

CONTENTS

APCU PROCEDURES .......................................................................................... 1

APCU ACTIVATION.............................................................................................. 3

APCU DEACTIVATION ......................................................................................... 5

SWIS PROCEDURES ........................................................................................... 7

SWIS SETUP ........................................................................................................ 9

DISABLE SWIS ..................................................................................................... 13

RESTORE SWIS................................................................................................... 15

VIEW SWIS DATA................................................................................................. 17

SWIS DEACTIVATION.......................................................................................... 19

ASSEMBLY PROCEDURES ................................................................................. 21

N1-1 CONFIGURATION PRE-3A UMBILICAL OPERATIONS .............................. 23

N1-1 CONFIGURATION POST 3A UMBILICAL OPERATIONS ............................ 29

N1-2 CONFIGURATION PRE-3A UMBILICAL OPERATIONS .............................. 33

N1-2 CONFIGURATION POST 3A UMBILICAL OPERATIONS ............................ 39

ACT & C/O PROCEDURES .................................................................................. 45

Z1 STRING 1 HEATER ACTIVATION/SGANT UMBILICAL SAFING .................... 47

Z1 STRING 2/SGANT HEATER ACTIVATION ...................................................... 49

DDCU-HP ON ORBIT TEST.................................................................................. 51

TRANSFER OPERATIONS................................................................................... 55

RESUPPLY TO ISS TRANSFER LIST .................................................................. 57

RETURN TO SHUTTLE TRANSFER LIST............................................................ 63

DEORBIT PREPARATION PROCEDURES .......................................................... 71

PAYLOAD DEACTIVATION .................................................................................. 73

PAYLOAD REACTIVATION .................................................................................. 75

PAYLOAD ENTRY SWITCH LIST/VERIFICATION ............................................... 77

MALFUNCTION PROCEDURES........................................................................... 79

ORBITER CRITICAL EQUIPMENT LOST PROCEDURES

BUS LOSS MATRIX ......................................................................................... 81

ELECTRICAL BUS/CRITICAL EQUIPMENT LOSS IMPACTS ......................... 83

MDM LOSS IMPACTS...................................................................................... 87

ISS CRITICAL EQUIPMENT LOST PROCEDURES

POWER BUS CONNECTIVITY - RACU 5 ........................................................ 91

POWER BUS CONNECTIVITY - RACU 6 ........................................................ 95

N1-1 MDM CHANNEL ASSIGNMENTS............................................................ 97

N1-2 MDM CHANNEL ASSIGNMENTS............................................................ 105

PL/DPS RECONFIG PROCEDURES

COMM MALFUNCTION POINTS...................................................................... 113

PL/DPS RECONFIGURATION ......................................................................... 115

21 SEP 00 ASSY OPSviii

APCU PROCEDURES

APCU AMPS .................................................................................................. 117

APCU TEMP ¯................................................................................................ 119

APCU TRIP....................................................................................................... 121

APCU VOLTS ¯.............................................................................................. 125

COMM PROCEDURES

OIU FAIL TO COMMAND ................................................................................. 127

OIU TEMP ..................................................................................................... 131

S212 OIU AD 1,2,3,4 NOLK/LOSS OF NODE MDM TELEMTRY ..................... 133

S62 PDI DECOM FAIL...................................................................................... 135

REFERENCE ........................................................................................................ 137

WIS

WIS REFERENCE DATA.................................................................................. 139

STANDARD SWITCH PANELS

STANDARD SWITCH PANEL #1...................................................................... 141

STANDARD SWITCH PANEL #2...................................................................... 143

DISPLAYS

MULTIFUNCTION CRT DISPLAY SYSTEM..................................................... 145

3A FDA TABLE ..................................................................................................... 215

21 SEP 00

APCU PROCEDURES

APCU

1

21 SEP 00


APCU

2

APCU ACTIVATION(ASSY OPS/3A/FIN) Page 1 of 1 page

21 JUN 006321.doc

NOTEIf the shuttle is not docked to the ISS, the APCUtelemetry will not be valid. Use APCU talkbacks only.

CRT SM 200 APCU Status

1. VERIFY ORBITER PAYLOAD BUS CONFIGURATIONR1 √PL PRI MNC tb − ON

√PL CAB − MNB(MNA)√PL AUX − ON

2. VERIFYING SWITCH POWERSSP1 √SW PWR 1 cb − CL

3. CLOSING APCU OUTPUT RELAY√APCU 1(2) CONV tb − bp

APCU 1(2) OUTPUT RLY − CL

4. TURNING APCU CONVERTER ONAPCU 1(2) CONV − ON

√APCU 1(2) CONV tb − gray√APCU 1(2) OUTPUT RLY tb − gray


√APCU1(2) OUT VOLTS RES HIGH between 122 and 126.5

3

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4

APCU DEACTIVATION(ASSY OPS/3A/FIN) Page 1 of 1 page

22 JUN 006322.doc

NOTEIf shuttle is not docked to the ISS, the APCUtelemetry will not be valid. Use APCU talkbacks only.


1. TURNING APCU CONVERTER OFFSSP1 APCU 1(2) CONV − OFF

√APCU 1(2) CONV tb − bp√APCU 1(2) OUTPUT RLY tb − bp

2. OPENING APCU OUTPUT RELAYAPCU 1(2) OUTPUT RLY − OP

5

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6

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SWIS PROCEDURES

SWIS

7

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SWIS

8

SWIS SETUP(ASSY OPS/3A/FIN A) Page 1 of 3 pages

19 SEP 006323.doc

1. UNSTOW EQUIPMENTMF71E Unstow:

NCUAntennaParallel port data cable assembly

2. SETUP SWISPGSC Close all applications, exit Windows.

Pwr → Off

Move SWIS hardware to AFD.Antenna →|←NCUData cable →|← NCU P PARALLEL PORTData cable →|← PGSC LPT portSecure NCU to port side aft bulkhead behind CCTV monitors.

3. ACTIVATING WISPGSC Pwr – On

At start menu, select appropriate chassis configuration.

NCU Pwr → On

PGSC From Desktop, select Shuttle Aps.Select SWIS folder.Double click SWIS icon.

WIS PGSC SW

4. SETTING NCU SERIAL NUMBERPreferences: Misc. Settings

‘NCU S/N’

sel 1002cmd SET

5. NCU GMT WITH PGSC SYNCRONIZATIONCommands: Set/Get GMT TimeSet/Get NCU GMT

cmd Sync NCU clock with PCcmd Get NCU time

√Date/Time agrees with GMT within ± 2 seconds

cmd Return

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6. CONFIGURING NCUUtilities: Network UtilityNetwork Utility

‘Action’

sel Reset NCUcmd Configurecmd OK in confirmation dialog

‘Command File Name’

Select flt 3a_swis_cmd_v1cmd Open

‘Command File Editor/Viewer’

Report ACQ start time to MCC-H.

sel RSU scroll [X] where [X] = 3210

√RSU S/N per table

NOTELocation provided for information only.

Table 1. RSU S/NRSU 0 1 2 3S/N 1008 1009 1021 1022

LOCN Z1 Z1 PLB Stbd PLB Port

√Command File Name − flt 3a_swis_cmd_v1√ACQ Setup File – flt3a_swis_acq_v1

Repeat

cmd Update NCU

At Confirmation dialog boxcmd ‘OK’cmd Return

7. NETWORK CHECKOUT

WIS PGSC SW

Utilities: Network MonitorNetwork Monitor

10


19 SEP 006323.doc

cmd Get StatusWait 120 seconds.

sel RSU Scroll – [X] where [X] = 3210

√ERROR − none√Data signal strength meter − in green range

Repeat

cmd Return

8. DATA DOWNLOAD

WIS PGSC SW

Commands: Download DataDownload Data

cmd Download Remaining Data

**********************************************************If Return pressed before download is complete,expect popup dialog.

sel ‘Cancel’ to return**********************************************************

cmd Return

Commands: Download Data

sel Download Rate − every 30 minutescmd Periodic Download

√Window disappears

Window: Download Data

√‘Stop Download ’ grayed out

Record MET: ___/__:__:__

Notify MCC-H, “SWIS setup complete.”

11

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12

DISABLE SWIS(ASSY OPS/3A/FIN A) Page 1 of 1 page

19 SEP 009717.doc

1. DISABLING DOWNLOAD

WIS PGSC SW


cmd Stop Downloadcmd Download Remaining Data

**********************************************************If Return pressed before download is complete,expect pop-up dialog.

sel ‘Cancel ’ to return**********************************************************

cmd Return

2. STOPPING SWIS SOFTWARE

WIS PGSC SW

PGSC File: Exit

3. DEACTIVATING NCUNCU PWR → Off

NOTEThe SWIS NCU can now be temp stowed out of the way ofthe aft window.

Notify MCC-H, “SWIS disabled.”

13

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14

RESTORE SWIS(ASSY OPS/3A/FIN A) Page 1 of 2 pages

19 SEP 009718.doc

1. ACTIVATING WISNCU Pwr → On

PGSC From Windows select WIS icon.

WIS PGSC SW

2. SETTING NCU SERIAL NUMBERPreferences: Misc. Settings‘NCU S/N’

sel 1002cmd SET

3. NCU GMT WITH PGSC SYNCRONIZATIONCommands: Set/Get GMT TimeSet/Get NCU GMT

cmd Sync NCU clock with PCcmd Get NCU time

√Date/Time agrees with GMT within ± 2 seconds

cmd Return

4. DATA DOWNLOAD

WIS PGSC SW


cmd Download Remaining Data

**********************************************************If Return pressed before download is complete,expect pop-up dialog.

sel ‘Cancel ’ to return**********************************************************

cmd Return

Commands: Download Data

sel Download Rate − every 30 minutescmd Periodic Download

√Window disappears

15

RESTORE SWIS(ASSY OPS/3A/FIN A) Page 2 of 2 pages

19 SEP 009718.doc

Window: Download Data

√‘Stop Download ’ grayed out

Record MET: ___/__:__:__

Notify MCC-H, “SWIS downlinking resumed.”

16

VIEW SWIS DATA(ASSY OPS/3A/FIN A) Page 1 of 1 page

16 SEP 006324.doc

1. VIEWING CHANNEL DATA

WIS PGSC SW‘Data’

sel desired color for plot trace

SELECT CHANNEL FILE

In ‘Temp’ folder selectZ1-1\accum-1a.wisZ1-2\accum-2a.wisZ1-1\tray-1h.wisZ1-2\sgant-2g.wisRSU-1\stchia-hp-1a.wisRSU-2\ptchia-tp-2b.wis

sel Open

Repeat as required for other channels.

WIS PGSC SW

cmd Refresh (auto refresh as desired)Scale as needed.

Figue 1.- Channel Data.

X Scale Button

Y Scale Button

17

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18

SWIS DEACTIVATION(ASSY OPS/3A/FIN A) Page 1 of 1 page

16 SEP 006325.doc

SWIS DEACTIVATION

WIS PGSC SW

PGSC File: Exit

Close all other PGSC software applications as required.

NCU Pwr → Off

Data Cable ←|→PGSC LPT portData Cable ←|→ NCU Parallel portRemove NCU from bulkhead.

Antenna ←|→ NCU

MF71E Stow NCU, NCU Antenna, and Data Cable for return to Ground.

Notify MCC, “SWIS Deact complete.”

19

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20

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ASSEMBLY PROCEDURES

ASSEMBLY

21

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ASSEMBLY

22

N1-1 CONFIGURATION PRE-3A UMBILICAL OPERATIONS(ASSY OPS/3A/FIN A/MULTI) Page 1 of 5 pages

19 SEP 006326.doc

NOTEVerify EPCS configured for both MDMs.

1. VERIFYING MDM STATESNode 1: C&DH: MDM N1-2Primary NCS MDM Node 1

Verify Frame Count <incrementing>Verify MDM ID − N1-2Verify Processing State − Primary

Node 1: C&DH: MDM N1-1Secondary NCS MDM Node 1

Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify Processing State − Secondary

********************************************************If frame counts not incrementing or if states arenot correct, exit this procedure, √MCC-H.

********************************************************

2. DISABLING NCS AUTO RETRY AND AUTO TRANSITION TODIAGNOSTIC

Node 1: C&DH: MDM N1-2Primary NCS MDM Node 1

‘Software Control’

sel MDM Utilities

Primary NCS MDM Utilities

√Auto Retry Status − INH

If Auto Retry Status − ENAcmd Inhibit Execute

√Auto Retry − INH


sel Processing State

Primary NCS Processing State Transitions‘Primary MDM Transitions’

√Auto Transition to Diag State – INH

23


19 SEP 006326.doc

If Auto Transition to Diag State – ENAcmd Inhibit Execute


3. CONFIGURING DATA BUSES

Primary NCS MDM Node 1

sel UB EPS N1 14sel Bus Status

√Channel Selected – B√Auto Channel Switch Status – INH




UB EPS N1 23

sel RT Status

√06 MDM N1-1 RT FDIR Status – INH


sel LB SYS LAB-2sel Bus Status



sel CB GNC-2sel Bus Status


24


19 SEP 006326.doc

4. COMMANDING N1-1 TO DIAGNOSTIC

NOTE1. Expect PCS FDA ‘CDH Node 1-2 MDM Detected RT

Fail of Node 1-1 MDM-PMA1 ’ message.

2. The Node 1/PMA1 Shell A Heater setpoints will defaultto very low values, rendering them inoperable.Recovery will occur after this procedure is complete.

3. N1-1 transition to Diagnostic takes 2 minutes.

Task: 3A Assembly Config3A Assembly Config

‘N1-1 MDM’

√Auth Xtion Diagnostic State − Enable

If Auth Xtion Diagnostic State − Disablecmd Auth Xtion Diagnostic State − Ena


cmd N1-1 MDM – Transition to Diagnostic State

5. REMOVING N1-1 MDM POWER AT RPC‘N1-1 MDM Power’

cmd RPCM N1 RS1 A RPC 11 – Op (Verify – Op)

6. DISABLING RT I/O TO DEVICES ON EPS BUSES‘UB EPS N1 14 RPCM’

cmd N1RS1 A − Inhcmd N1RS1 B − Inhcmd N1RS1 C − Inh

√RT Inhibit 20, 19, 18 (three) − X

25


19 SEP 006326.doc

NOTE1. Only one of the following steps (7, 8, or 9) should be

performed based on the location from which the RACUwill be commanded off.

2. Upon deactivation of RACU 6, the following messagesmay be annunciated.

On Orbiter MCDS:‘SPEC 204 RACU6 VOLT LMT ’

On PCS:‘RPCM N1RS1_A Loss Of Comm – Nod1 ’‘RPCM N1RS1_B Loss Of Comm – Nod1 ’‘RPCM N1RS1_C Loss Of Comm – Nod1 ’‘RPCM Z14B_A Loss Of Comm – Z1 ’‘RPCM Z14B_B Loss Of Comm – Z1 ’

7. MCC-M COMMANDING FGB RACU 6 OFFCrew ⇓ MCC-H, “Ready for RACU 6 Power Off.”MCC-H ⇒ MCC-M, “Go for RACU 6 Power Off.”

Record planned RACU Off Command opportunities based on RussianGround Site coverage.

RUSSIAN GROUND AOS LOS

Pass 1 ___/___:___:___ ___/___:___:___

Pass 2 ___/___:___:___ ___/___:___:___

MCC-M ⇒ MCC-H ⇑ crew,“RACU 6 Powered Off at __/___:___:__ GMT.” >>

PCS FGB: EPS: RACUFGB_RACUs

√RACU 6 Converter − Off√Input Current < 2.0 A√Output Voltage ~90 V

8. CREW COMMANDING FGB RACU 6 OFF FROM MCDS

CRT SM 224 FGB – 2N

√COMMANDING – ENA

MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 6 Power Off.”MCC-H ⇑ crew, “Moscow Go for RACU 6 Power Off.”

26


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On MCC GO


RACU 6 PWR OFF VIA NCS − ITEM 8 EXEC

√RACU 6 INP AMPS < 2.0 A√OUT VOLTS ~90 V√PWR OFF − ∗

9. CREW COMMANDING FGB RACU 6 OFF FROM PCSPCS FGB: CDH: FGB MDM

FGB MDM

√Direction_Of_Cmd – MU√Relay_Cmd_Matrix_MU_Inh − <blank>

MCC-M ⇒ MCC-H: “�� Inhibited and Command Matrix Enabled. Gofor RACU 6 Power Off.”

MCC-H ⇑ crew, “Moscow Go for RACU 6 Power Off.”

On MCC-H GO

FGB: EPS: RACUFGB_RACUs

cmd RACU 6 − Off Execute

√RACU 6 Converter − Off√Input Current < 2.0 A√Output Voltage ~90 V

10. CONNECTING STRING 1 UMBILICAL BUNDLESIV Notify EVA crew: “RACU 6 Off. Go for String 1 umbilical connections.”

NOTEEV connects Node 1 String 1 umbilicals per EVA procedure.

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28

N1-1 CONFIGURATION POST 3A UMBILICAL OPERATIONS(ASSY OPS/3A/FIN A/MULTI) Page 1 of 4 pages

19 SEP 006327.doc

NOTEOnly one of the following steps (1, 2, or 3) should beperformed based on the location from which theRACU will be commanded on.

1. MCC-M COMMANDING RACU 6 ONCrew ⇓ MCC-H, “Ready for RACU 6 Power On.”MCC-H ⇒ MCC-M, “Go for RACU 6 Power On.”


Pass 1 ___/___:___:___ ___/___:___:___

Pass 2 ___/___:___:___ ___/___:___:___

MCC-M ⇒ MCC-H ⇑ Crew,“RACU 6 Power On at ___/___:___:___ GMT.”

2. CREW COMMANDING FROM MCDS



Crew ⇓ MCC-H: “Relay Matrix Enabled. Ready for RACU 6 Power On.”MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 6 Power On.”MCC-H ⇑ crew, “Go for RACU 6 Power On.”

On MCC GO

SM 224 FGB – 2N

√MAIN BUS V1, V2 (two): 28.0 --- 29.0 V√BATT VOLTS 1 --- 6 (six) > 25.5 V

SM 220 NODE 1 – 2N

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Verify PRI MDM FRM CTR incrementing.

If FRM CTR staticSM 224 FGB – 2N

RACU 6 PWR ON VIA FGB − ITEM 3 EXEC

√RACU 6 Power On − ∗√Input Amps ≥ 2.5 A√Output Volts: 121 --- 125 V

√Amps: 0.3 --- 10 A

NOTEAmperage should be at 0.5 amps at power On. Amperagecould be as high as 10 amps after MDM initialization(approximately 2.5 minutes), depending on heater usage.

***********************************************************If RACU 6 OUT AMPS > 10

RACU 6 PWR OFF VIA FGB − ITEM 7 EXEC***********************************************************

If FRM CTR incrementing

SM 224 FGB – 2NRACU 6 PWR ON VIA NCS − ITEM 4 EXEC

√RACU 6 PWR ON − ∗√INP AMPS ≥ 2.5 A√OUT VOLTS: 121 --- 125 V

√AMPS: 0.3 --- 10 A


**********************************************************If RACU 6 OUT AMPS > 10

RACU 6 PWR OFF VIA FGB − ITEM 8 EXEC**********************************************************

3. CREW COMMANDING FROM PCSFGB: CDH: FGB MDMFGB MDM


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MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 6 Power On.”

PCS FGB: EPSFGB: EPS

√Main Bus Voltage 1,2 (two): 28.0 --- 29.0 V√Battery Voltage 1 --- 6 (six) > 25.5 V

**************************************************If any FGB Batt Voltage < 25.5 Volts, then

Notify MCC: “FGB Batteries Low.”Wait one orbit for FGB Batteries tocharge.

**************************************************


cmd RACU 6 − On Execute

√RACU 6 Converter − On√RACU 6 Input Current ≥ 2.5 A

√Output Current: 0.3 --- 10 A√Voltage: 121 --- 125 V


***************************************If RACU 6 Output Current > 10

cmd RACU 6 − Off Execute**************************************




Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify Processing State − Standby

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NOTEIf frame count not incrementing, wait up to 2 minutes forMDM to complete POST.

************************************************************************If N1-2 powerdown will be delayed one orbit, perform

Node 1: C&DH: MDM N1-2Primary NCS MDM Node 1‘Software Control’

sel MDM Utilities

‘Auto Retry Status’

cmd Enable Execute (Verify – ENA)



Primary NCS State Transition‘Primary MDM Transitions’

cmd Auto Transition to Diagnostic State Enable Execute

√Auto Transition to Diag State − ENA

‘N1-1 MDM Transitions’

cmd Transition to Secondary State Execute


Verify Processing State − Secondary************************************************************************

32


19 SEP 006328.doc

NOTEVerify EPCS configured for both MDMs.

1. VERIFYING MDM STATESPCS2 Node 1: C&DH: MDM N1-2




Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify Processing State − Standby

**********************************************************If frame counts not incrementing or states are notcorrect, exit this procedure.

√MCC-H**********************************************************

2. INHIBITING NCS AUTO RETRY AND AUTO TRANSITION TODIAGNOSTIC



sel MDM Utilities

Secondary NCS MDM Utilities

√Auto Retry Status – INH

If Auto Retry Status − Enacmd Inhibit Execute

√Auto Retry Status – Inh


33


19 SEP 006328.doc


Secondary NCS Processing State Transitions‘Secondary MDM State Transitions’


If Auto Transition to Diag State – ENAcmd Inhibit Execute


3. COMMANDING N1-2 TO DIAGNOSTICOn MCC GO

NOTE1. N1-1 MDM will go to Primary when N1-2 goes to Diagnostic.

2. The Node 1/PMA1 Shell B Heater setpoints will default tovery low values, rendering them inoperable. Recovery willoccur after this procedure is complete.

Task: 3A Assembly Config3A Assembly Config

‘N1-2 MDM’


If Auth Xtion Diagnostic State − Disablecmd Auth Xtion Diagnostic State − Ena


NOTE1. Expect ‘MDM Connection Fail ’ message on PCS2.

2. Expect possible ‘S62 PDI DECOM FAIL ’ message.

cmd N1-2 − Transition to Diagnostic State

Wait 2 minutes for transition to complete.

Verify N1-2 Frame Count − <static>

Wait 1 minute, proceed (allows N1-1 to go to Primary).

34


19 SEP 006328.doc

4. TELEMETRY RECOVERY ON OIU

CRT SM 212 OIU

BUS 4 BC − ITEM 15 EXEC (∗)BUS 3 RT − ITEM 10 EXEC (∗)Change OIU N1 Physical Device to N1-1 − ITEM 18 +4 EXEC

NOTEExpect possible ‘S62 PDI DECOM FAIL ’ message.

Reload OIU FORMAT 2 − ITEM 1 +2 EXEC

5. TELEMETRY RECOVERY ON PCS

NOTEC&W tone and ‘Node 1-1 MDM Detected RT Fail ofNode 1-2 MDM-PMA1 ’ message will be generated asN1-1 becomes Primary and detects N1-2 fail.

PCS1 If requiredsel Arrow above PCS logosel Start/Restart PCS CDSsel Icon to open PCS CDS Main Control Panel Window, enlarge(may be buried behind displays)

Verify Status Box − yellow

sel ‘Connect to MDM’

Verify Status Box − greenVerify ‘connected ’ indicated.

NOTEAfter PCSCDS has been selected, wait 30 seconds beforestarting CDDF displays.

If displays not loadedsel arrow above PCS logosel Start PCS CDDF display

Home page will display when load complete (~1 minute).

35


19 SEP 006328.doc

6. CONFIGURING DATA BUSESPCS Node 1: C&DH: MDM N1-1


Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify MDM State – Primary


√Auto Channel Switch Status − INH√Channel Selected − A



sel LB SYS LAB 1sel Bus Status


sel CB GNC 1sel Bus Status


7. POWERING OFF N1-2 MDMTask: 3A Assembly Config3A Assembly Config

‘N1-2 MDM’

cmd RPCM N1 RS2 C RPC 13 – Op (Verify – Op)

8. DISABLING RT I/O TO DEVICES ON EPS BUSES‘UB EPS N1 23 RPCM’

cmd N1RS2 A − Inhcmd N1RS2 B − Inhcmd N1RS2 C − Inh

√RT Inhibit 20, 19, 18 (three) − X

36


19 SEP 006328.doc

NOTE1. Only one of the following steps (9, 10, or 11) should be

performed based on the location from which the RACUwill be commanded off.

2. Upon deactivation of RACU 5, the following messagesmay be annunciated.

On Orbiter MCDS‘SPEC 204 RACU5 VOLT LMT ’

On PCS‘RPCM N1RS2_A Loss Of Comm – Nod1 ’‘RPCM N1RS2_B Loss Of Comm – Nod1 ’‘RPCM N1RS2_C Loss Of Comm – Nod1 ’‘RPCM Z13B_A Loss Of Comm – Z1 ’‘RPCM Z13B_B Loss Of Comm – Z1 ’

9. MCC-M COMMANDING FGB RACU 5 OFFCrew ⇓ MCC-H, “Ready for RACU 5 Power Off.”MCC-H ⇒ MCC-M, “Go for RACU 5 Power Off.”

Record planned RACU Off Command opportunities based on RussianGround Site coverage.


Pass 1 ___/___:___:___ ___/___:___:___

Pass 2 ___/___:___:___ ___/___:___:___

MCC-M ⇒ MCC-H ⇑ crew,“RACU 5 Powered Off at __/___:___:__GMT.” >>

PCS FGB: EPS: RACUFGB_RACUs

√RACU 5 Converter − Off√Input Current < 2.0 A√Output Voltage ~90 V >>

10. CREW COMMANDING FGB RACU 5 OFF FROM ORBITER MCDS



MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 5 Power Off.”MCC-H ⇑ crew, “Moscow Go for RACU 5 Power Off.”

37


19 SEP 006328.doc

On MCC-H GO

SM 224 FGB – 2N

RACU 5 Power OFF VIA NCS − ITEM 6 EXEC

√RACU 5 INP AMPS < 2.0 A√OUT VOLTS ~90 V√PWR OFF − ∗ >>

11. CREW COMMANDING FGB RACU 5 OFF FROM PCSPCS FGB: CDH: FGB MDM

FGB MDM


MCC-M ⇒ MCC-H: “�� Inhibited and Command Matrix Enabled. Gofor RACU 5 Power Off.”

MCC-H ⇑ crew, “Moscow Go for RACU 5 Power Off.”

On MCC-H GO


cmd RACU 5 − Off Execute

√RACU 5 Converter − Off√Input Current < 2.0 A√Output Voltage ~90 V >>

12. STRING 2 UMBILICAL BUNDLES CONNECTIONIV EVA crew: “RACU 5 Off. Go for String 2 umbilical connections.”

NOTEEV connects Node 1 String 2 umbilicals per EVA procedure.

38


19 SEP 006329.doc

NOTEOnly one of the following steps (1, 2, or 3) should beperformed based on the location from which theRACU will be commanded on.

1. MCC-M COMMANDING RACU 5 ON

Crew ⇓ MCC-H, “Ready for RACU 5 Power On.”MCC-H ⇒ MCC-M, “Go for RACU 5 Power On.”


Pass 1 ___/___:___:___ ___/___:___:___

Pass 2 ___/___:___:___ ___/___:___:___

MCC-M ⇒ MCC-H ⇑ Crew,“RACU 5 Power On at ___/___:___:___ GMT.”

2. CREW COMMANDING RACU 5 ON FROM MCDS



Crew ⇓ MCC-H: “Relay Matrix Enabled. Ready for RACU 5 Power On.”MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 5 Power On.”MCC-H ⇑ crew, “Go for RACU 5 Power On.”

On MCC GO

SM 224 FGB – 2N

√MAIN BUS V1, V2 (two): 28.0 --- 29.0 V√BATT VOLTS 1 --- 6 (six) > 25.5 V

SM 220 NODE 1 – 2N

39


19 SEP 006329.doc

Verify PRI MDM FRM CTR incrementing.

If FRM CTR staticSM 224 FGB – 2N

RACU 5 PWR ON VIA FGB − ITEM 1 EXEC

√RACU 5 Power On − ∗√Input Amps ≥ 2.5 A√Output Volts: 121 --- 125 V

√Amps: 0.3 --- 10 A


**********************************************************If RACU 5 OUT AMPS > 10

RACU 5 PWR OFF VIA FGB − ITEM 5 EXEC**********************************************************

If FRM CTR incrementing

SM 224 FGB – 2NRACU 5 PWR ON VIA NCS − ITEM 2 EXEC

√RACU 5 PWR ON − ∗√INP AMPS ≥ 2.5 A√OUT VOLTS: 121 --- 125 V

√AMPS: 0.3 --- 10 A


***********************************************************If RACU 5 OUT AMPS > 10

RACU 5 PWR OFF VIA FGB − ITEM 6 EXEC***********************************************************

3. CREW COMMANDING FROM PCSFGB: CDH: FGB MDMFGB MDM


40


19 SEP 006329.doc

MCC-M ⇒ MCC-H: “�� Inhibited. Go for RACU 5 Power On.”

PCS FGB: EPSFGB: EPS

√Main Bus Voltage 1,2 (two): 28.0 --- 29.0 V√Battery Voltage 1 --- 6 (six) > 25.5 V

***********************************************************If any FGB Batt Voltage < 25.5 Volts, then

Notify MCC: “FGB Batteries Low.”

Wait one orbit for FGB Batteries to charge.***********************************************************


cmd RACU 5 − On Execute

√RACU 5 Converter − On√RACU 5 Input Current ≥ 2.5 A

√Output Current: 0.3 --- 10 A√Voltage: 121 --- 125 V


*****************************************If RACU 5 Output Current > 10

cmd RACU 5 − Off Execute*****************************************

4. VERIFYING MDM STATESTask: 3A Assembly Config3A_Assembly_Config

‘Primary NCS’

Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify Major State − Primary

‘Secondary NCS’

Verify Frame Count <incrementing>Verify MDM ID − N1-2Verify Major State − Standby

41


19 SEP 006329.doc

5. COMMANDING N1-1 TO SECONDARY‘N1-1 MDM’

cmd N1-1 − Transition to Secondary State

Verify Frame Count static.

NOTEN1-2 will go to Primary in 20 seconds.

6. TELEMETRY RECOVERY ON OIU

NOTEExpect ‘S62 PDI DECOM FAIL ’ message.

CRT SM 212 OIU

BUS 3 BC − ITEM 11 EXECBUS 4 RT − ITEM 14 EXECChange OIU N1 Phys Dev to N1-2 − ITEM 18 +3 EXECReload OIU FORMAT − ITEM 1 +2 EXEC

7. CTP POWERUPVerify there is no PCS active on the UB-ORB buses (AFT Flight Deck)

CRT SM 223 EARLY COMM-2N

N1RS2A RPC 10 CL – ITEM 13 EXEC (*)

Wait 60 seconds to allow the CTP to establish a connection with thePrimary MDM before proceeding.

√CTP POST − PASS√DECRYPT POST − PASS

8. TELEMETRY RECOVERY ON PCSPCS2 sel Icon to open PCS CDS Main Control Panel Window

Verify Status box − yellow

sel ‘Connect to MDM ’

Verify Status box − greenVerify ‘connected to MDM ’ indicated.

42


19 SEP 006329.doc




Verify Frame Count <incrementing>Verify MDM ID − N1-1Verify Processing State − Secondary

**********************************************************If frame counts are not incrementing or no N1-2telemetry, √MCC-H.

**********************************************************

10. POWERING ON SDO CARDSNode 1: EPS: RPCM_N1RS1_A

sel RPC 5

RPCM_N1RS1_A_RPC_5

cmd RPC Position – Close (Verify – Cl)

Node 1: EPS: RPCM_N1RS2_C

sel RPC 4

RPCM_N1RS2_C_RPC_4


11. ENABLING NCS AUTO RETRY AND AUTO TRANSITION TODIAGNOSTIC



sel MDM Utilities

‘Auto Retry Status’

43


19 SEP 006329.doc


Secondary NCS MDM Node 1


Secondary NCS Processing State Transitions‘Secondary MDM State Transitions’‘Auto Transition to Diag State’


44

21 SEP 00

ACT & C/O PROCEDURES

AC

T &

C/O

45

21 SEP 00


AC

T &

C/O

46

Z1 STRING 1 HEATER ACTIVATION/SGANT UMBILICAL SAFING

(ASSY OPS/3A/FIN A) Page 1 of 2 pages

20 SEP 006330.doc

1. STRING 1 Z1 RT DEVICE I/O ENABLEDPCS2 Task: 3A Assembly Config

3A Assembly Config

�UB EPS N1 14 RPCM�

ÖRT Inhibit 12, 11 (two) - blank

If RT Inhibit 12, 11 (two) - X

cmd Z14B A - Ena

cmd Z14B B - Ena

ÖRT Inhibit 12, 11 (two) - blank

2. VERIFYING SGANT UMBILICALS DEADFACEDPCS2 Z1: EPS: RPCM Z14B_B

RPCM Z14B_B

sel RPC 5

RPCM Z14B_B RPC 5

Verify RPC Position � Op

cmd Close Cmd � Inhibit (Verify � Inh)

If Z1 STRING 2/SGANT HEATER ACTIVATION (SODF: ASSY OPS:ACTIVATION AND CHECKOUT) performedZ1: EPS: RPCM Z13B_B

RPCM Z13B_B

sel RPC 5

RPCM Z13B_B RPC 5

cmd Close Cmd � Inhibit (Verify � Inh)

IV Notify EVA crew, �Go for SGANT Dish installation.�

3. Z1 STRING 1 HEATERS ACTIVATIONZ1: EPS: RPCM Z14B_B

RPCM Z14B_B

sel RPC 7

RPCM Z14B_B RPC 7

cmd RPC Position - Close (Verify - Cl)

sel RPC 10

47

Z1 STRING 1 HEATER ACTIVATION/SGANT UMBILICAL SAFING

(ASSY OPS/3A/FIN A) Page 2 of 2 pages

20 SEP 006330.doc

RPCM Z14B_B RPC 10


sel RPC 12

RPCM Z14B_B RPC 12


sel RPC 14

RPCM Z14B_B RPC 14


48

Z1 STRING 2/SGANT HEATER ACTIVATION(ASSY OPS/3A/FIN A) Page 1 of 2 pages

19 SEP 006331.doc

1. STRING 2 Z1 RT DEVICE I/O ENABLEDPCS2 Task: 3A Assembly Config

3A Assembly Config‘UB EPS N1 23 RPCM’

√RT Inhibit 12, 11 (two) − blank

If RT Inhibit 12, 11 (two) − Xcmd Z13B A − Enacmd Z13B B − Ena

√RT Inhibit 12, 11 (two) − blank

IV Wait until EV crew completes SGANT dish install before proceeding.

2. SGANT AND TRC HEATER ACTIVATIONZ1: EPS: RPCM Z14B_BRPCM Z1 4B_B

sel RPC 5

RPCM Z1 4B_B RPC 5

cmd Close Cmd – Enable (Verify – Ena)cmd RPC Position – Close (Verify – Cl)

sel RPC 6

RPCM Z1 4B_B RPC 6


IV Notify EV crew, “Go for SGANT Boom Deploy.”

3. STRING 2 Z1 HEATERS ACTIVATIONZ1: EPS: RPCM Z13B_BRPCM Z1 3B_B

sel RPC 7

RPCM Z1 3B_B RPC 7

cmd RPC Position − Close (Verify − Cl)

sel RPC 10

RPCM Z1 3B_B RPC 10


49

Z1 STRING 2/SGANT HEATER ACTIVATION(ASSY OPS/3A/FIN A) Page 2 of 2 pages

19 SEP 006331.doc

sel RPC 12

RPCM Z1 3B_B RPC 12


sel RPC 16

RPCM Z1 3B_B RPC 16


50

DDCU-HP ON ORBIT TEST(ASSY OPS/3A/FIN) Page 1 of 3 pages

26 JUN 006768.doc

NOTEThe DDCU Z13B Trip Status display provides Reverse inhibit/enableindications for the following parameters: input undervoltage trip,125 % Current trip, thermal trip, input overvoltage trip, and 150 %current trip. If “INH” appears in the associated telemetry field, thefunction is enabled.

1. APPLYING INPUT POWER TO DDCU Z13B(Z14B)Perform APCU 1(2) ACTIVATION (SODF: ASSY OPS: OIU/APCU), then:

2. ESTABLISHING COMMUNICATION WITH DDCU Z13B(Z14B)2.1 Enabling and Initializing NCS DDCU Control Software in Primary

MDMNode 1: C&DH: Primary NCS MDM: Applications: EPS AppsPrimary NCS EPS Applications

Verify DDCU Control − INH

cmd DDCU Control − Enable

√DDCU Control − ENA

2.2 Enabling DDCU Z13B(Z14B) RT and FDIRNode 1: C&DH: Primary NCS MDM: UB EPS N1-23(N1-14): RTStatusUB EPS N1 23(N1 14) RT

Verify 15 DDCU Z1-3B(Z1-4B) RT Status − INH

cmd 15 DDCU Z1-3B(Z1-4B) RT Status − Enable

√15 DDCU Z1-3B(Z1-4B) RT Status − ENA√15 DDCU Z1-3B(Z1-4B) RT Failed Status − <blank>

Verify 15 DDCU Z1-3B(Z1-4B) FDIR Status − INH

cmd 15 DDCU Z1-3B(Z1-4B) FDIR Status − Enable FDIR

√15 DDCU Z1-3B(Z1-4B) FDIR Status − ENA

3. VERIFYING DDCU Z13B(Z14B) ACTIVEZ1: EPS: DDCU Z13B (Z14B)DDCU Z13B(Z14B)

√Integration Counter − incrementing√Input Voltage > 115 V

51


26 JUN 006768.doc

4. CLEARING DDCU POWER ON RESETsel Firmware

DDCU Z13B(Z14B) Firmware

cmd Clear Cmds − Common Clear

√Power On Reset − <blank>

5. TURNING ON DDCU CONVERTER

NOTEDDCU Converter Status (On/Off) telemetry is indicated as “0” or “1,”where “0” indicates that the converter is off and “1” indicates theconverter is on.

Z1: EPS: DDCU Z13B(Z14B)DDCU Z13B(Z14B)

sel Converter

DDCU Z13B(Z14B) Converter

cmd On Armcmd On

√Output Voltage − 121 --- 128 V

6. ESTABLISHING AND CONFIRMING COMMUNICATION WITHDOWNSTREAM RPCMS

MCC-H Perform RPCM N13B(N14B) ENABLE (SODF: ISS OPS: C&DH), then:

If Checking DDCU Z13BNode 1: EPS: RPCM N13B A,B,CRPCM N13B A,B,C

√Integ Counter − incrementing√Bus Voltage, V > 120 V

If Checking DDCU Z14BNode 1: EPS: RPCM N14B A,B,CRPCM N14B A,B,C

√Integ Counter − incrementing√Bus Voltage, V > 120 V

52


26 JUN 006768.doc

7. VERIFYING DDCU FIRMWARE OPERATIONMCC-H Perform DDCU Z13B(Z14B) BDT FOR BIT SUMMARY DATA, all

(SODF: ISS GND: EPS), then:

8. TURNING OFF DDCU CONVERTERZ1: EPS: DDCU Z13B(Z14B)DDCU Z13B(Z14B)

sel Converter

DDCU Z13B(Z14B) Converter

cmd Off

√Output Voltage < 14 V

9. REMOVING INPUT POWER FROM DDCU Z13B(Z14B)Go to APCU 1(2) DEACTIVATION, all (SODF: ASSY OPS: OIU/APCU).

53

20 SEP 00


54

21 SEP 00

TRANSFER PROCEDURES

TRANSFER

55

21 SEP 00


TRANSFER

56

RESUPPLY TO ISS TRANSFER LIST(ASSY OPS/3A/FIN A) Page 1 of 6 pages

20 SEP 006333.doc

LABL

FD Initials Item # Item Name Qty ShuttleStowage

ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)

PROCEDURES/Constraints /**Comments

FD4 TRANSFERN/A Stowage Outfitting Bag 1 N/A FGB_209* Crew

preference0 ITEM NOT TRANSFERRED

Do not use bungees in theNode, thermalconstraint.

**Use Velcro, bungees, tie-downs as needed forstowage from this bag.This bag stays on-orbit,replace at the end oftransfer activities for theday.

4 1 ISS TRANSFER FD4 CTB

(Note: items 1a-1f are stowed in this bagpre-launch)

1sngl

MA16D 30total

**Equipment not called outin 1a-1f remains in bagand will return tomiddeck with CBMequipment (flashlight,pliers, etc.) in this bag onFD9.

4 1a DIDB (2), DIDB Restraint Bag (1) MA16D MF43H **Prior to transfer, removethe DIDBs and the DIDBRestraint Bag and placein MF43H CTB (item 10).These bags are xfer onFD9 with other EVAitems.

4 1b Ground Strap Assy (2), RTL Pip Pins (4),Protective Caps (16)

MA16D Z1 VEST NODE 1 TO Z1VESTIBULE OUTFITTING-INGRESS #1 (SODF: ISSOPS: S&M)** Ground Straps and

associated hardware forabove procedure arecontained within thisCTB.

4 1c PCMCIA Hard Card (7) MA16D FGB_426/427 **Stow in EPCS-2 singleCTB

4 1d Medical Equip Computer CDCase (1)

MA16D FGB_426/427 **Stow in CHECS tripleCTB

57


20 SEP 006333.doc

LABL


ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)


4 1e Dry Wipes BagRubber Gloves Bag

MA16D NOD1O1* 0.140.50

**ISS crew items. Stow inCTB with 3A MPEV

4 1f Modified 5/32” L-Wrenches (2) MA16D NOD1S4 0.05 **Stow in IVA Seal Kit #2

4 1g Seat Track Button Assemblies (8), SeatTrack Button Fastener Assemblies (28)(stowed in Ziplock Bag)

MA16D **ISS Crew item. Stowonly.

4 2 SODF 1sngl

MF57H FGB_312 FGB tempstow

0 15 16.1 **ISS crew item. Swap outwith PCG-EGN Dewar(item 222) in FGB onFD9

4 3 FORMALDEHYDE MONITORING KIT 1 MDK CEIL(UPPER)

PORT SMALLBAG

FGB_426/427

1 15 0.1 **ISS crew item. Stow inCHECS triple CTB.

4 4 CHECS SUPPLEMENTAL PACK –Bioinstrumentation Bag

1 MDK CEIL(UPPER)

PORT SMALLBAG

FGB_426/427

15 2.27 **ISS crew item. Stow inCHECS triple CTB.

4 5 TISSUE EQUIVALENT PROPORTIONALCOUNTER (TEPC)

1 MDK CEIL(UPPER)

PORT SMALLBAG

FGB_426/427

15 8.2 **ISS crew item. Stow inCHECS triple CTB.

4 6 CWC 1 MDK CEIL(LOWER)

PORT SMALLBAG

FGB_224* MiddeckTemp Stow

0 15 45 **Pre-fill, CWCs are locatedin the middeck ceilinglower port small bag.

Post-fill, CWCs are stowedas necessary to support aShuttle Next-PLS untilCWCs are transferred toISS.Weight shown is approx.value for CWC and water.**Bungees needed from

Stowage Outfitting Bag(FGB_209*) to secureCWCs. Strap per photoin xfer book.


PORT SMALLBAG


0 15 45 **Refer to item 6.

58


20 SEP 006333.doc

LABL


ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)



PORT SMALLBAG




PORT SMALLBAG



59


20 SEP 006333.doc

LABL


ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)


FD9 TRANSFER (Note: Retrieve “Bungee bag” from NOD1D4_D1 as needed to secure items onboard ISS)9 10 EVA CTB

PGT (1), PGT Batts (2), PGT ProgramCable (1), Adjustable Fuse Teather (1),Crew Hook Lock w/lanyards (4), DropProof Tether Adapter (1), DIDB (2), DIDBRestraint Bag (1)

1sngl

MF43H NOD1O4_B1 15 16.0 **Charge PGT Batteriesprior to xfer. Removecrew lock EVA Bag andthe upper foam aroundthe bag (not lower PGTfoam), restow both inMF43H. Retrieve 1Adjustable fuse teatherfrom MF71H (or Airlock iftemp stowed there) andplace in CTB in lidnetting.

**Place DIDBs (2) andDIDB restraint bag (1)from MA16D (item #1a)in this CTB on FD4.


PORT SMALLBAG


0 15 45 **Pre-fill, CWCs are locatedin middeck ceiling lowerport small bag.

**Post-fill, CWCs arestowed as necessary tosupport a Shuttle Next-PLS until CWCs aretransferred to ISS.

**Weight shown is approx.value for CWC andwater.


PORT SMALLBAG




PORT SMALLBAG



9 14 Dedicated Laptop (for CMG ops)Removable Harddrive, Removable CD-Rom Drive, Battery Pack, Floppy Disk,CD-ROM, 20’ 1553 cable, DC PowerAdapter, 10’ PGSC DC Power Cable

MF71C CMG CHECKOUT USINGDATA ANALYSIS TOOL(SODF: JNT OPS:MATED)

**This equipment staysonboard ISS.

60


20 SEP 006333.doc

LABL


ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)


9 212 IMAX 1dbl

NOD1O4_J1 MiddeckTemp Stow

30 **IMAX3D equipment istransferred to orbiter onFD4 for middeck filmingof EVA preparation.Equipment is returned toISS on FD9.

9 213 IMAX3D Accessories Kit(see items 213a and 213b)

1 FGB_303 MiddeckTemp Stow

15 1.66 **IMAX3D equipment istransferred to orbiter onFD4 for middeck filmingof EVA preparation.Equipment is returned toISS on FD9. Place kitinside IMAX CTB thatwas left onboard FGB.

9 213a IMAX Audio Recorder Battery Charger 1 MF71K FGB_303 IMAX3DAccess. Kit

0 2.9 **Swap out with old chargerin Accessories Kit (item213) prior to ISS return.Old Charger isreconnected to Audiorecorder for ICBC3D.Use AUDIORECORDERPROCEDURES (P/TV,P/TV08) as applicable

9 213b IMAX Audio Recorder Batteries 2 MF71K FGB_303 IMAX3DAccess. Kit

0 3.7 **Swap out old Batteries inAccessories Kit (item213) prior to ISS return.Old Batteries are usedfor Audio recorder forICBC3D. Use AUDIORECORDERPROCEDURES (P/TV,P/TV08) as applicable

9 214 IMAX ASSY BAG #3

30mm Lens (1), 40mm Lens (1),50mm Lens (1)

1half

NOD1O4_H1 MiddeckTemp Stow

15 13.2 **IMAX3D equipment istransferred to orbiter onFD4 for middeck filmingof EVA preparation.Equipment is returned toISS on FD9.

61


20 SEP 006333.doc

LABL


ISSStowage

(* = outsiderack)

TempStowage

TOXLevel

XFERTime(min)

TotalWt(kg)



Magazine (1), Right Hand Grip (1), LeftHand Grip (1), VDA Cables(1 long, 1 short), photoflood clamps (2),changing bag (1)

1sngl

NOD1O4_H3 MiddeckTemp Stow



Camera body (1), VDA(1), Opticalviewfinder and eyecup (1), Optics box (1)

1sngl

NOD1O4_J3 MiddeckTemp Stow


62

RETURN TO SHUTTLE TRANSFER LIST(ASSY OPS/3A/FIN A) Page 1 of 7 pages

19 SEP 008868.doc

LABL

FD Initials Item # Item Name Qty ISSStowage

ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)


FD4 TRANSFER4 204 EXTERNAL SAMPLING ADAPTER (ESA) 1 Node 1

FWD HatchMDK CEIL(UPPER)

PORTSMALL BAG

Jettison/Stowage

Bag

0 1.47 NODE 1 INGRESS #1(SODF: JNT OPS:INGRESS STATION)**ESA is removed and

returned on 3A.4 212 IMAX3D Equipment 1

dblNOD1O4_J1 Middeck

tempstow

30 **IMAX3D equipment istransferred to orbiter onFD4 for middeck filmingof EVA preparation.Equipment is returned toISS on FD9.

4 213 IMAX3D Accessories Kit 1 FGB_303 Middecktempstow

15 1.66 **See item 212. RemoveAccessories Kit fromCTB in FGB. Onlytransfer Accessories Kit.


30mm Lens (1), 40mm Lens (1), 50mm Lens(1)

1half

NOD1O4_H1

Middecktempstow

15 13.2 **See item 212.


Magazine (1), Right Hand Grip (1), LeftHand Grip (1), VDA Cables(1 long, 1 short), photoflood clamps(2),changing bag (1)

1sngl

NOD1O4_H3

Middecktempstow

15 22.0 **See item 212.


Camera body (1), VDA (1), Opticalviewfinder and eyecup (1), Optics box (1)

1sngl

NOD1O4_J3

Middecktempstow

15 27.0 **See item 212.

63


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)


64


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)


FD9 TRANSFER9 222 PCG-DEWAR

Contains:PCG-EGN Electronics BoxDewar Bag, Dewar, Insert, Dewar Cap,insert cap

1 FGB_312 MA16D 15 24.5 Dewar is extremelyfragile. Exercise cautionduring unstow/transfer/stow.**Swap Dewar with SODF

bag from MF57H (item 2)**ISS Payload, launched on

STS-106. Dewar is intwo parts, thermal bagand electronics box.Bungee together for xfer.If bungee not aroundboth parts, unstow frominside foam lid cutout ontop of electronics box.

9 205 CBM CONTROLLER ASSY (CPA) 1 Node1/Z1VEST

MF43H NOD1O4_J3

(in CTB)

0 14.43kg

NODE 1 TO Z1 TRUSSVESTIBULE OUTFITTING-INGRESS #1 (SODF: ISSOPS: S&M)One CPA per Middecklocker due to weightrestrictions.**Stow in CTB (single) on

FD4. Stow CTB in NodeZSR where IMAX3Dequipment was untilFD9.

**On Middeck, place CrewLock EVA Bag and foamin this CTB from EVACTB (item 10)

65


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)



MF57H NOD1O4_J1

(in CTB)

0 14.43kg

NODE 1 TO Z1 TRUSSVESTIBULE OUTFITTING-INGRESS #1 (SODF: ISSOPS: S&M)One CPA per Middecklocker due to weightrestrictions.**On FD4, stow CPA and 4

Fans (items 206a-206d)in CTB. Stow CTB inNode ZSR whereIMAX3D equipment wasuntil FD9. Swap withIMAX3D bag on FD9

9 206a PORTABLE FAN ASSY (W/BATTERIES) 1 Node1 MF57H NOD1O4_J1

2 1.94 PMA1 INGRESS (SODF:JNT OPS: INGRESSSTATION)**Stow fan in same CTB

with CPA (item 206).9 206b PORTABLE FAN ASSY (W/BATTERIES) 1 Node1 MF57H NOD1O4

_J12 1.94 PMA1 INGRESS (SODF:

JNT OPS: INGRESSSTATION)**Stow fan in same CTB

with CPA (item 206).9 206c PORTABLE FAN ASSY (W/BATTERIES) 1 Node1 MF57H NOD1O4


JNT OPS: INGRESSSTATION)**Stow fan in same CTB

with CPA (item 206).9 206d PORTABLE FAN ASSY (W/BATTERIES) 1 Node1 MF57H NOD1O4


JNT OPS: INGRESSSTATION)**Stow Fan in same CTB

with CPA (item 206).

66


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)



MF28E NOD1O4_J1

(in CTB)

0 14.43kg

NODE 1 TO Z1 TRUSSVESTIBULE OUTFITTING-INGRESS #2 (SODF: ISSOPS: S&M)One CPA perCTB/Middeck locker dueto weight restrictions.**On FD4, Stow CPA and

latches (item 208) inCTB. Stow CTB in NodeZSR where IMAX3dequip was until FD9.Swap with IMAX Bag onFD9.

9 208 CAPTURE LATCH ASSY 2 Node1/Z1VEST

MF28E NOD1O4_J1

0 0.10kg

NODE 1 TO Z1 TRUSSVESTIBULEOUTFITTING-INGRESS#2 (SODF: ISS OPS:S&M)

**Stow with CPA (item 207)in same CTB.


MF28M NOD1O4_H3

(in CTB)

0 14.43kg

NODE 1 TO Z1 TRUSSVESTIBULE OUTFITTING-INGRESS #2 (SODF: ISSOPS: S&M)One CPA per Middecklocker due to weightrestrictions.**On FD4, Stow CPA and

latches in CTB. StowCTB in Node ZSR untilFD9. Swap with IMAXBag on FD9.

9 210 CAPTURE LATCH ASSY 2 Node1/Z1VEST

MF28M NOD1O4_H3

0 0.10kg

NODE 1 TO Z1 TRUSSVESTIBULEOUTFITTING-INGRESS#2 (SODF: ISS OPS:S&M)

**Stow with CPA (item 209)in same CTB.

67


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)


9 217 D-CELL BATTERIES 1hlf

NOD1D4_K4

2 15 2.32kg

NODE1 EGRESS #2(SODF: JNT OPS:EGRESS STATION).Remove 16 fresh Batteriesfrom bag per procedure andplace in MRK Fans.**Remove 4 used Batteries

from MRK Fan used toprovide air circulation forZ1 vestibule ops (ifapplicable) and place inhalf CTB. Return entirebag containing 32Batteries (fresh andused) to middeck onFD9.

9 218 PMA IMV DUCT EXTENSION ASSY 1 PMA2 MDK CEIL(UPPER)

PORTSMALL BAG

0 0.77kg

NODE 1 EGRESS #2(SODF: JNT OPS:EGRESS STATION)**Stow duct, V-band clamp,

and Velcro ties perprocedure.

9 221 PMA TARGET COVER ASSY 1 PMA2 MDK CEIL(UPPER)

PORTSMALL BAG

Jett/StowBag

0 0.2 PMA2 EGRESS #2 (SODF:JNT OPS: EGRESSSTATION)**Base plate removed from

cover and installed onPMA2.

**Cover returns to ground.9 223 TARGET STOWAGE BOX 1 NOD1P4_

B20 PMA2 CENTERLINE

CAMERA TARGETINSTALLATION/REMOVAL(SODF: ISS OPS: S&M)**Box is returned to ground

after PMA2 CenterlineCamera Target isinstalled on PMA2. Seedrawing in xfer book forstowage.

68


19 SEP 008868.doc

LABL


ShuttleStowage

Temp.Stowage

Tox.Level

XFERTime(min)

TotalWt(kg)


69

20 SEP 00


70

21 SEP 00

DEORBIT PREP PROCEDURES

DE

OR

BIT

PR

EP

71

21 SEP 00


DE

OR

BIT

PR

EP

72

PAYLOAD DEACTIVATION(ASSY OPS/3A/FIN A) Page 1 of 1 page

19 SEP 006282.doc

NOTEExpect ‘SM 200 APCU 1 TRIP’ and ‘SM 200 APCU 2TRIP’ messages.

1. DEACTIVATING PAYLOAD BUSESR1 PL CAB − OFF

PRI MNC – OFF (tb-OFF)AUX − OFF

SSP1 cb SW PWR 1,2 – opSSP2 cb SW PWR 1,2,3,4 – op

73

20 SEP 00


74

PAYLOAD REACTIVATION(ASSY OPS/3A/FIN) Page 1 of 1 page

23 JUN 006283.doc

N/A for STS-92.

75

20 SEP 00


76

PAYLOAD ENTRY SWITCH LIST/VERIFICATION(ASSY OPS/3A/FIN A) Page 1 of 1 page

16 SEP 006284.doc

R1 √PL CAB − OFF√PRI MNC − ctr (tb-OFF)

√MNB,FC3 (two) − ctr (tb-OFF)√AUX − OFF√AFT MNB − OFF

√MNC − OFF

L12 √APCU 1,2 CONV (two) − OFF (tb-bp)(SSP1) √APCU 1,2 OUTPUT RLY (two) − OP (tb-bp)

√cb SW PWR 1 − op

√PRI C/L CAM PWR − OFF√SEC C/L CAM PWR − OFF√ODS CONN MATE X1 TLM PWR − OFF

√X2 TLM PWR − OFF√TCS PWR − OFF (tb-bp)√cb SW PWR 2 − op√cb PDIP PWR 1 − op√cb PDIP PWR 2/ KuBAND RLY − op

√OIU PWR − OFF (tb-bp)

L12 √RMS SIDE VIEW CAM PWR − OFF(SSP2) √HTR − OFF

√SLP CAM PORT CAM − OFF√C/L CAM − OFF

√ICBC3D OVERIDE − OFF (tb-bp)√PWR − OFF (tb-bp)

√DDCU HTR THRMST PORT CKT A − OFF (tb-bp)√CKT B − OFF (tb-bp)

√STBD CKT A − OFF (tb-bp)√CKT B − OFF (tb-bp)

√cb SW PWR 1-4 (four) − op

77

20 SEP 00


78

21 SEP 00

MALFUNCTION PROCEDURES

MALFUNCTIO

N

79

21 SEP 00


MALFUNCTIO

N

80

BUS LOSS MATRIX (ASSY OPS/3A/FIN A) Page 1 of 1 page

ESS MNA DA1 MNB DA2 FC3 MNC DA3

1BC 2CA 3ABPNLO14

FPC 1 MPC 1 MPC 2PNL

ML86BPNLO15

(R) (R) P APC 6 FPC 3 PNL O16

ORBITER EPS BUSES AC 1PNLA7A3(A6)

SPEEPWR

AUXPLA

P (R)AUXPLB

PNLA7A3(A6)

PNLML85E(MUP)

PNLA7A3(A6)

PRI PL APC 3 AC 3PNLA7A3(A6)

CABINAFTPLC

PL1 PL2 PL3ORBITER EQUIPMENT

OIU 1 (SSP 1A) X OIU 2 (SSP 1A) X APCU 1 (SSP 1B) XC X APCU 2 (SSP 1B) XC X ODS X1 Conn Mate Ind Pwr (SSP 1A) R R ODS X2 Conn Mate Ind Pwr (SSP 2A) R R SLP Camera #1 (SSP 2B) X SLP Camera #2 (SSP 2B) X Primary C/L Camera (SSP 1A) X RMS Side Camera (SSP 2A) X RMS Side Camera Heaters (SSP 2A) X PDIP X Payload Timing Buffer X

ISS EQUIPMENT PMA-2/3 Hooks - Sys A XRC X XRC PMA-2/3 Hooks - Sys B XRC X XRC DDCU PORT Thermostats R R DDCU STBD Thermostats R R

PAYLOADSICBC - Main Pwr (SSP 2A - APC Interface) XC X

ICBC - PGSC Power XPAYLOAD BUS CONTROL POWER

Cabin P/L Bus - Main A Control Power XC Cabin P/L Bus - Main B Control Power XC Aux P/L A Bus - Main A Control Power XC Aux P/L B Bus - Main B Control Power XC P/L PRI - Main B Control Power XRC XRC P/L PRI - Main C Control Power XRC XRC P/L PRI - FC 3 Control Power XRC XRC Aft P/L B Bus - Main B Control Power XRC XRC Aft P/L C Bus - Main C Control Power XRC XRC

X - Total Loss of Operational PowerP - Loss of Primary Power SourceR - Loss of Redundant Power Source(R) - Requires an Action to use Redundant SourceXC - Total Loss of Control PowerXRC - Loss of Redundant Control Power

19 SEP 00 6285.xls

81

20 SEP 00


82

ELECTRICAL BUS/CRITICAL EQUIPMENT LOSS IMPACTS(ASSY OPS/3A/FIN A) Page 1 of 3 pages

18 SEP 006286.doc

MNA DA1MNA MPC1

CABIN PL1 (REDUN POWER AVAILABLE)SSP 1

CB 2APCU #1 CONVAPCU #1 OUTPUTSLP CAMERA #1SEC C/L CAM

SSP 2CB 2

DDCU PORT HTR CKT AICBC MAIN POWERICBC OVERRIDESLP CAMERA #2


CB 1PDIP

DC POWER 2KU-BAND RATE RELAY

CB 3X1 (ODS)/X2 (PMA2)

ODS CONN MATE X1 TLM (REDUN POWER AVAILABLE)X2 (ODS)/X1 (PMA2)

ODS CONN MATE X2 TLM (REDUN POWER AVAILABLE)PDIP

DC POWER 1SSP 2

CB 1DDCU STBD HTR CKT A

CB 3DDCU PORT HTR CKT B

CABIN PL3SSP1


ODS CONN MATE X1 TLM (REDUN POWER)X2 (ODS)/X1 (PMA2)

ODS CONN MATE X2 TLM (REDUN POWER)PNL A7A3 (A6 CONSOLE)

CTVC KEEL CAMERA HTR PWRPRI C/L CAMERA POWER/ON CNTL

F1PAYLOAD TIMING BUFFER

F4OIU 1 (PDI TLM 1)

83


18 SEP 006286.doc

SSP2CB 4

DDCU STBD HTR CKT BF1

RMS SIDEVIEW CAMERA POWERF2

CTVC KEEL CAMERA CNTLF4

CTVC KEEL CAMERA POWERMNB DA2

MNB MPC2CABIN PL1 (REDUN POWER AVAILABLE)

SSP 1CB 2

APCU #1 CONVAPCU #1 OUTPUTSLP CAMERA #1SEC C/L CAM

SSP 2CB 2

DDCU PORT HTR CKT AICBC MAIN POWERICBC OVERRIDESLP CAMERA #2


CB 1PDIP

DC POWER 2KU-BAND RATE RELAY


ODS CONN MATE X1 TLM (REDUN POWER AVAILABLE)X2 (ODS)/X1 (PMA2)

ODS CONN MATE X2 TLM (REDUN POWER AVAILABLE)PDIP

DC POWER 1SSP 2

CB 1DDCU STBD HTR CKT A

CB 3DDCU PORT HTR CKT B

CABIN PL3SSP1


ODS CONN MATE X1 TLM (REDUN POWER)X2 (ODS)/X1 (PMA2)

ODS CONN MATE X2 TLM (REDUN POWER)

84


18 SEP 006286.doc

PNL A7A3 (A6 CONSOLE)CTVC KEEL CAMERA HTR PWRPRI C/L CAMERA POWER/ON CNTL

F1PAYLOAD TIMING BUFFER

F4OIU 1 (PDI TLM 1)

SSP2CB 4

DDCU STBD HTR CKT BF1

RMS SIDEVIEW CAMERA POWERF2

CTVC KEEL CAMERA CNTL

AUX PLBSSP 1

F3OIU 2 (PDI TLM 2)

SSP 2F3

APCU 2 CONVAPCU 2 OUTPUTRMS SIDEVIEW CAMERA HTR

PRI PL (REDUN POWER AVAILABLE)APCU 1

X1 (ODS)/X2 (PMA2)RPDA N1-3B

APCU 2X2 (ODS)/X1 (PMA2)

RPDA N1-4BICBC

MNC DA3MNC MPC3

PRI PL (REDUN POWER AVAILABLE)APCU 1

X1 (ODS)/X2 (PMA2)RPDA N1-3B

APCU 2X2 (ODS)/X1 (PMA2)

RPDA N1-4BICBC

85

20 SEP 00


86

MDM LOSS IMPACTS(ASSY OPS/3A/FIN) Page 1 of 3 pages

22 JUN 006287.doc

FF1Uplink Through NSP 1 (Secondary)

FF3Uplink Through NSP 2 (Primary)

PF1(PL1)ISS Primary Command Path (via PSP 1 - UMB 1/OIU 1)APCU 1 TelemetryOIU 1 Telemetry (PDI TLM 1)DIH - CARD 06 - CH 02

X2 (ODS)/X1 (PMA2)input 14 - ORB X2 CONN MATE (TLM/SIG)


PF2(PL2)ISS Redundant Command Path (via PSP 2 - UMB 1/OIU 2)APCU 2 TelemetryOIU 2 Telemetry (PDI TLM 2)OSVS InterfaceDIH CARD 06 - CH 02



OF1Ku-Band Gyro TempPCMMU 1 FORMAT monPCMMU PWR 1,2 monBFS Auto TFLPL BAY MECH PWR SYS 1 & 2 monPL RETEN LOGIC PWR SYS 1 & 2 monMID MCA 3 OP STATUS 1 mon

2 mon3 mon4 mon5 mon

DSC OF1Ku-Band Gyro TempPCMMU 1 - Mode Select

87


22 JUN 006287.doc

OF2P/L INTRG 1,2 CHAN SEL monPSP 1, 2 - Bit & Frame SyncPCMMU 2 FORMAT monALL PL RETEN LATCH CMD monALL PL RETEN RELEASE CMD monPL SEL 1 1B REL/LAT monPL SEL 1 2B REL/LAT monPL SEL 1 3B REL/LAT monPL SEL 1 4B REL/LAT monPL SEL 1 5B REL/LAT monPL SEL 1 1B R-F-L monPL SEL 1 2B R-F-L monPL SEL 1 3B R-F-L monPL SEL 1 4B R-F-L monPL SEL 1 5B R-F-L monMID MCA 1 OP STATUS 5 monMID MCA 1 OP STATUS 6 monMID MCA 3 OP STATUS 5 monMID MCA 3 OP STATUS 7 monMID MCA 3 OP STATUS 8 mon

DSC OF2PCMMU 2 - Mode Select

OF3Orbiter Comm Telemetry (S-Band PM/FM, Ku-Band, UHF, NSP 1&2, COMSEC)GCIL Telemetry (revert to panel)PL PRI FC3 ON tlm

MNB ON tlmMNC ON tlm

Ku-Band Alpha/Beta Gimbal Temp

DSC OF3Ku-Band Alpha Gimbal Temp

OF4PSP Command Capability

NOTEIf only one port is lost, command capability can beregained by switching to the opposite PCMMU.

KU-BAND RADAR PWR monS-BAND (P/L, PM, FM) & KU-BAND CONTROL monOrbiter Comm - GCIL Driver Telemetry (S-Band PM, P/L, FM, Ku-Band, CCTV)

PSP, PI, GCIL, COMSEC - ON/OFF TelemetryCAB P/L MNA(MNB) ON tlmPL AUX ON tlmPL RETEN PL SELECT SW mon

88


22 JUN 006287.doc

DSC OM2Ku-Band Beta Gimbal Temp

OA1X4 (ODS)/X3 (PMA2)ORB X4 CONN MATE (TLM/SIG)

PMA2 GRP 1 PASS MECH HKS 1, 3, 5 CLOSED INDPMA2 GRP 1 PASS MECH HKS 7, 9, 11 CLOSED IND

DSC OA1X4 (ODS)/X3 (PMA2)ORB X4 CONN MATE (TLM/POWER)

PMA2 GRP 1 PASS MECH HKS 1, 3, 5 CLOSED IND/SOURCEPMA2 GRP 1 PASS MECH HKS 7, 9, 11 CLOSED IND/SOURCE

OA2X3 (ODS)/X4 (PMA2)

ORB X3 CONN MATE (TLM/SIG)PMA2 GRP 2 PASS MECH HKS 2, 4, 6 CLOSED INDPMA2 GRP 2 PASS MECH HKS 8, 10, 12 CLOSED IND

DSC OA2X3 (ODS)/X4 (PMA2)

ORB X3 CONN MATE (TLM/POWER)PMA2 GRP 2 PASS MECH HKS 2, 4, 6 CLOSED IND/SOURCEPMA2 GRP 2 PASS MECH HKS 8, 10, 12 CLOSED IND/SOURCE

OA3PL SEL 1 1A REL/LAT monPL SEL 1 2A REL/LAT monPL SEL 1 3A REL/LAT monPL SEL 1 4A REL/LAT monPL SEL 1 5A REL/LAT monPL SEL 1 1A R-F-L monPL SEL 1 2A R-F-L monPL SEL 1 3A R-F-L monPL SEL 1 4A R-F-L monPL SEL 1 5A R-F-L mon

89

20 SEP 00


90

POWER BUS CONNECTIVITY - RACU 5(ASSY OPS/3A/FIN) Page 1 of 4 pages

23 JUN 006334.doc

BUS LOST EQUIPMENT LOST FUNCTION/EQUIPMENTREDUNDANCY LOST

CONTROL/INSTRUMENTATIONLOST

RPDA N1RS2

RPCM N1RS2 A RPC 1: N1 Htr 1BRPC 2: N1 Htr 2BRPC 3: N1 Htr 3BRPC 4: N1 Htr 4BRPC 5: CBM N1 Stbd Pri 1

(Early Comm TransceiverPwr & Htr)

RPC 6: CBM N1 Stbd Pri 2(Early Comm Spare)

RPC 10: CBM N1 Stbd Pri 3(Early Comm CTP)

RPC 11: CBM N1 Stbd Pri 4(Early Comm RFPDB)

RPC 12: N1 Htr 5BRPC 13: N1 Htr 6BRPC 14: N1 Htr 7BRPC 15: N1 Htr 8BRPC 16: N1 Htr 9B

1 of 2 Node1 Shell HeaterStrings (N1 B Heaters)

1 of 2 Stbd CBM Power Sources

Early Comm Command and Telemetry

RPCM N1RS2 B RPC 1: PMA3 Htr 1ARPC 2: PMA3 Htr 1BRPC 3: PMA3 Htr 2ARPC 4: PMA3 Htr 2BRPC 5: PMA3 Htr 3ARPC 12: PMA3 Htr 3BRPC 13: PMA3 Htr 4ARPC 14: PMA3 Htr 4BRPC 15: PMA3 Htr 5ARPC 16: PMA3 Htr 5B

2 of 2 PMA3 Shell Heater Strings

RPCM N1RS2 C RPC 1: PMA1 Htr 1BRPC 2: PMA1 Htr 2BRPC 3: N1-2 SDO Card 1ARPC 4: N1-2 SDO Card 1BRPC 7: CBM N1 Port Pri 1RPC 8: CBM N1 Port Pri 2

1 of 2 Node1 MDMs (N1-2)1 of 2 PMA1 Shell Heater

Strings (PMA1 B Heaters)1 of 2 Port CBM Power Sources

Control of RPCM N13B A, B, and CInstrumentation from RPCM N13B A, B,

and C

RACU5

91


23 JUN 006334.doc



RPDA N1RS2

RPCM N1RS2 C RPC 10: CBM N1 Port Pri 3RPC 11: CBM N1 Port Pri 4RPC 13: N1-2 MDMRPC 14: PMA1 Htr 3BRPC 15: MDM N1-1 Srv HtrRPC 16: PMA1 Htr 5B

RPDA Z13B

RPCM Z13B A None

RPCM Z13B B RPC 1: S-Band SASA 2RPC 4: S-Band BSP 2RPC 5: KU-Band SGANTRPC 6: DDCU Z14B Htr 2RPC 7: EEATCS Non-op Htr

A-1RPC 8: SPDA Z14B Htr ARPC 9: SPDA Z13B Htr ARPC 10: CMG 1 Ext HtrRPC 11: DDCU Z13B Htr 1RPC 12: CMG 4 Ext HtrRPC 14: KU-Band SGTRCRPC 15: PCU 1RPC 16: PCU 2 HtrRPC 17: CMG 3RPC 18: CMG 2

Power to CMG 1 and CMG 4Heaters

Power to EEATCS HeaterPower to PCU 1 HeaterPower to 1 of 2 Heaters to all

other Z1 Heater LoadsPower to 1 of 2 Plasma

Contactors

RACU5

92


23 JUN 006334.doc



RPDA N13B

RPCM N13B A RPC 4: IMV Stbd Aft FanRPC 5: Lt Int NOD1OS4RPC 13: Lt Int NOD1OS2-1RPC 16: SD 2

Power to Interior Lights

RPCM N13B B RPC 1: Lt Int NOD1PD2RPC 3: CBM N1 Nad Pri 1RPC 4: CBM N1 Nad Pri 2RPC 5: CBM N1 Nad Pri 3RPC 6: CBM N1 Nad Pri 4RPC 11: CBM N1 Zen Pri 1(Z1 PCBM Htr 2)

RPC 12: CBM N1 Zen Pri 2RPC 13: CBM N1 Zen Pri 3RPC 14: CBM N1 Zen Pri 4RPC 15: IMV Deck Aft VlvRPC 16: IMV Deck Fwd Vlv

Power to Interior Lights1 of 2 Nad CBM Power Sources1 of 2 Zen CBM Power Sources

RPCM N13B C RPC 1: Lt Int NOD1OS2RPC 3: CBM N1 Fwd Pri 1RPC 4: CBM N1 Fwd Pri 2RPC 5: CBM N1 Fwd Pri 3RPC 6: CBM N1 Fwd Pri 4RPC 13: IMV Fwd Stbd VlvRPC 14: IMV Fwd Port VlvRPC 16: IMV Port Fwd Fan

Power to Interior Lights1 of 2 Fwd CBM Power Sources

APCU1

93


23 JUN 006334.doc



RPDA N14B

RPCM N14B A RPC 2: CBM N1 Fwd Sec 1RPC 3: CBM N1 Fwd Sec 2RPC 14: CBM N1 Fwd Sec 3RPC 15: CBM N1 Fwd Sec 4RPC 16: IMV Stbd Fwd Vlv

1 of 2 Fwd CBM Power Sources

RPCM N14B B RPC 1: Lt Int NOD1SD2RPC 3: CBM N1 Zen Sec 1(Z1 PCBM Htr 1)

RPC 4: CBM N1 Zen Sec 2RPC 5: CBM N1 Zen Sec 3RPC 6: CBM N1 Zen Sec 4RPC 11: CBM N1 Nad Sec 1RPC 12: CBM N1 Nad Sec 2RPC 13: CBM N1 Nad Sec 3RPC 14: CBM N1 Nad Sec 4RPC 16: RAMVRPC 17: Cab Fan

Power to Interior Lights1 of 2 Zen CBM Power Sources1 of 2 Nad CBM Power Sources

RPCM N14B C RPC 2: Lt Int NOD1OP4RPC 3: SD 1RPC 4: IMV Aft Stbd VlvRPC 5: IMV Aft Port VlvRPC 12: IMV Aft Port FanRPC 13: IMV Stbd Aft VlvRPC 14: IMV Port Fwd VlvRPC 15: Lt Int NOD10P2-1RPC 16: Lt Int NOD10O2-2

Power to Interior Lights

APCU2

94


23 JUN 006335.doc



RPDA N1RS1

RA

RPCM N1RS1 A RPC 1: N1 Htr 1ARPC 2: N1 Htr 2ARPC 3: N1 Htr 3ARPC 4: N1 Htr 4ARPC 5: N1-1 SDO Card 1ARPC 6: N1-1 SDO Card 1BRPC 11: N1-1 MDMRPC 12: N1 Htr 5ARPC 13: N1 Htr 6ARPC 14: N1 Htr 7ARPC 15: N1 Htr 8ARPC 16: N1 Htr 9A

1 of 2 Node 1 MDMs (N1-1)1 of 2 Node 1 Shell Heater

Strings (N1 A Heaters)

Control of RPCM N14B A, B, and CInstrumentation from RPCM N14B A, B,

and C

CU6

RPCM N1RS1 B RPC 5: CBM N1 Port Sec 1RPC 6: CBM N1 Port Sec 2RPC 13: CBM N1 Port Sec 3RPC 14: CBM N1 Port Sec 4

1 of 2 Port CBM Power Sources

RPCM N1RS1 C RPC 1: PMA1 Htr 1ARPC 2: MDM N1-2 Srv HtrRPC 5: CBM N1 Stbd Sec 1

(Early Comm Port Ant Pwr)RPC 6: CBM N1 Stbd Sec 2

(Early Comm Port Ant Htr)RPC 12: CBM N1 Stbd Sec 3

(Early Comm Stbd Ant Pwr)RPC 13: CBM N1 Stbd Sec 4

(Early Comm Stbd Ant Htr)RPC 14: PMA1 Htr 3ARPC 15: PMA1 Htr 4ARPC 16: PMA1 Htr 5A

1 of 2 PMA1 Shell Heater Strings(PMA1 A Heaters)

1 of 2 Stbd CBM Power Sources

Early Comm Command and Telemetry

95


23 JUN 006335.doc



RPDA N1RS1

RPDA Z14B

RPCM Z14B A None

RACU6

RPCM Z14B B RPC 1: S-Band SASA 2 HtrRPC 4: S-Band BSP 2 HtrRPC 5: KU-Band SGANT HtrRPC 6: KU-Band SGTRC HtrRPC 7: EEATCS Non-op Htr

B-1RPC 8: SPDA Z13B Htr BRPC 9: SPDA Z14B Htr BRPC 10: CMG 2 Ext HtrRPC 11: DDCU Z14B Htr 1RPC 12: CMG 3 Ext HtrRPC 14: PCU 1 HtrRPC 15: PCU 2RPC 16: DDCU Z13B Htr 2RPC 17: CMG 4RPC 18: CMG 1

Power to CMG 2 and CMG 3Heaters

Power to PCU 2 HeaterPower to S-Band SASA 2 and

BSP 2 HeatersPower to KU-Band SGANT and

SGTRC HeatersPower to EEATCS HeaterPower to 1 of 2 Heaters to all

other Z1 Heater LoadsPower to 1 of 2 Plasma

Contactors

96

N1-1 MDM CHANNEL ASSIGNMENTS(ASSY OPS/3A/FIN/MULTI) Page 1 of 7 pages

Name Description MDM Card Refdes

Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

HX Lab LT-A Inl V Norm Fl Pos Lab LT-A HX Inlet Byp Vlv Norm Flow Pos Ind N1-1 A09 DIO SL02 CH00 A Lab ECLSS 5A 12AHX Lab LT-A Inl V Byp Fl Pos Lab LT-A HX Inlet Byp Vlv Byp Flow Pos N1-1 A09 DIO SL02 CH01 A Lab ECLSS 5A 12AHX Lab LT-A Out V Open Pos Lab LT-A HX Outlet Isln/Rlf Vlv Open Pos Ind N1-1 A09 DIO SL02 CH02 B Lab ECLSS 5A 12AHX Lab LT-A Out V Cls Pos Lab LT-A HX Outlet Isln/Rlf Vlv Cls Pos Ind N1-1 A09 DIO SL02 CH03 B Lab 5A 12ASmk Det N1-1 Bit Enbl Node-1 Smk Det-1 Bit Enbl N1-1 A09 DIO SL02 CH04 B Node-1 2A ACVAV Dmpr N1-N1 EnableCmd Node-1 Air Mix Vlv Enable Cmd N1-1 A09 DIO SL02 CH05 A Node-1 ECLSS 2A ACIMV Fan N1-Aft Rtn On/Off Cmd Node-1 Aft lMV Fan On/Off Cmd N1-1 A09 DIO SL02 CH06 A Node-1 ECLSS 2A ACCab Vent Fan N1 On/Off Cmd Node-1 Cabin Fan On/Off Cmd N1-1 A09 DIO SL02 CH07 A Node-1 ECLSS 2A ACTWV N1-1 Pos A Node-1 3-Way SDS Vlv-1 Pos A N1-1 A09 DIO SL02 CH08 A Node-1 ? 2A ACTWV N1-1 Pos B Node-1 3-Way SDS Vlv-1 Pos B N1-1 A09 DIO SL02 CH09 A Node-1 ? 2A ACTWV N1-2 Pos A Node-1 3-Way SDS Vlv-2 PosA N1-1 A09 DIO SL02 CH10 B Node-1 ? 2A ACTWV N1-2 Pos B Node-1 3-Way SDS Vlv-2 Pos B N1-1 A09 DIO SL02 CH11 B Node-1 ? 2A ACTWV N1-3 Pos A Node-1 3-Way SDS Vlv-3 Pos A N1-1 A09 DIO SL02 CH12 B Node-1 ? 2A ACTWV N1-3 Pos B Node-1 3-Way SDS Vlv-3 Pos B N1-1 A09 DIO SL02 CH13 A Node-1 ? 2A ACTWV N1-4 Pos A Node-1 3-Way SDS Vlv 4 PosA N1-1 A09 DIO SL02 CH14 A Node-1 ? 2A ACTWV N1-4 Pos B Node-1 3-Way SDS Vlv-4 Pos B N1-1 A09 DIO SL02 CH15 A Node-1 ? 2A ACIMV V N1-Aft Rtn Cls Pos Node-1 Aft Rtn IMV Vlv Cls Pos N1-1 A09 DIO SL02 CH16 A Node-1 ECLSS 2A ACIMV V N1-Aft Rtn Enbl Cmd Node-1 Aft Rtn IMV Vlv Enable Cmd N1-1 A09 DIO SL02 CH17 A Node-1 ECLSS 2A ACIMV V N1-Aft Rtn Open Pos Node-1 Aft Rtn IMV Vlv Open Pos N1-1 A09 DIO SL02 CH18 B Node-1 ECLSS 2A ACIMV V N1-Aft Sply Open Pos Node-1 Aft Sply IMV Vlv Open Pos N1-1 A09 DIO SL02 CH19 B Node-1 ECLSS 2A ACIMV V N1-Aft Sply Cls Pos Node-1 Aft Sply IMV Vlv Cls Pos N1-1 A09 DIO SL02 CH20 B Node-1 ECLSS 2A ACIMV V N1-Aft Sply Enbl Cmd Node-1 Aft Sply IMV Vlv Enable Cmd N1-1 A09 DIO SL02 CH21 A Node-1 ECLSS 2A ACIMV V N1-Port Sply Open Pos Node-1 Port Sply IMV Vlv Open Pos N1-1 A09 DIO SL02 CH22 A Node-1 ECLSS 2A ACIMV V N1-Port Sply Cls Pos Node-1 Port Sply IMV Vlv Cls Pos N1-1 A09 DIO SL02 CH23 A Node-1 ECLSS 2A ACIMV V N1-Port Sply Enbl Cmd Node-1 Port Sply IMV Vlv Enable Cmd N1-1 A09 DIO SL02 CH24 A Node-1 ECLSS 2A ACIMV V N1-Stbd Rtn Enbl Cmd Node-1 Stbd Rtn IMV Vlv Enable Cmd N1-1 A09 DIO SL02 CH25 A Node-1 ECLSS 2A ACIMV V N1-Stbd Rtn Open Pos Node-1 Stbd Rtn IMV Vlv Open Pos N1-1 A09 DIO SL02 CH26 B Node-1 ECLSS 2A ACIMV V N1-Stbd Rtn Cls Pos Node-1 Stbd Rtn lMV Vlv Cls Pos N1-1 A09 DIO SL02 CH27 B Node-1 ECLSS 2A ACIMV V N1-Stbd Sply Open Pos Node-1 Stbd Sply IMV Vlv Open Pos N1-1 A09 DIO SL02 CH28 B Node-1 ECLSS 2A ACIMV V N1-Stbd Sply Cls Pos Node-1 Stbd Sply IMV Vlv Cls Pos N1-1 A09 DIO SL02 CH29 A Node-1 ECLSS 2A ACIMV V N1-Stbd Sply Enbl Cmd Node-1 Stbd Sply IMV Vlv Enable Cmd N1-1 A09 DIO SL02 CH30 A Node-1 ECLSS 2A ACSPARE SPARE N1-1 A09 DIO SL02 CH31 SPARE SPARE SPARE

SSMDM N1-2 Htr Pwr MDM PMAl-2 Htr Pwr N1-1 A05 SDO SL03 CH00 n/a PMA-1 TCS 2A ACHX Lab LT-A Inl V Norm Fl Cmd Lab LT-A HX Inlet Byp Vlv Norm Flow Cmd N1-1 A05 SDO SL03 CH01 n/a Lab ECLSS 5A 12AHX Lab LT-A Inl V Byp Fl Cmd Lab LT-A HX Inlet Byp Vlv Byp Flow Cmd N1-1 A05 SDO SL03 CH02 n/a Lab ECLSS 5A 12AHX Lab LT-A Out V Open Cmd Lab LT-A HX Outlet lsln/Rlf Vlv Open Cmd N1-1 A05 SDO SL03 CH03 n/a Lab ECLSS 5A 12AHX Lab LT-A Out V Cls Cmd Lab LT-A HX Outlet Isln/Rlf Vlv Cls Cmd N1-1 A05 SDO SL03 CH04 n/a Lab ECLSS 5A 12ATWV N1-1 Solenoid Cmd Node-1 3-Way SDS Vlv-1 Solenoid Cmd N1-1 A05 SDO SL03 CH05 n/a Node-1 ? 2A AC

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

TWV N1-1 Latch Cmd Node-1 3-Way SDS Vlv-1 Latch Cmd N1-1 A05 SDO SL03 CH06 n/a Node-1 ? 2A ACTWV N1-2 Solenoid Cmd Node-1 3-Way SDS Vlv-2 Solenoid Cmd N1-1 A05 SDO SL03 CH07 n/a Node-1 ? 2A ACTWV N1-2 Latch Cmd Node-1 3-Way SDS Vlv-2 Latch Cmd N1-1 A05 SDO SL03 CH08 n/a Node-1 ? 2A ACTWV N1-3 Solenoid Cmd Node-1 3-Way SDS Vlv-3 Solenoid Cmd N1-1 A05 SDO SL03 CH09 n/a Node-1 ? 2A ACTWV N1-3 Latch Cmd Node-1 3-Way SDS Vlv-3 Latch Cmd N1-1 A05 SDO SL03 CH10 n/a Node-1 ? 2A ACTWV N1-4 Solenoid Cmd Node-1 3-Way SDS Vlv-4 Solenoid Cmd N1-1 A05 SDO SL03 CH11 n/a Node-1 ? 2A ACTWV N1-4 Latch Cmd Node-1 3-Way SDS Vlv-4 Latch Cmd N1-1 A05 SDO SL03 CH12 n/a Node-1 ? 2A ACSPARE SPARE N1-1 A05 SDO SL03 CH13 n/a SPARE SPARESPARE SPARE N1-1 A05 SDO SL03 CH14 n/a SPARE SPARESPARE SPARE N1-1 A05 SDO SL03 CH15 n/a SPARE SPARESPARE SPARE N1-1 A05 SDO SL03 CH16 n/a SPARE SPARE

SPARE SPARE N1-1 A10 DIO SL04 CH00 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH01 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH02 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH03 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH04 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH05 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH06 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH07 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH08 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH09 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH10 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH11 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH12 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH13 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH14 SPARE SPARE SPARESPARE SPARE N1-1 A10 DIO SL04 CH15 SPARE SPARE SPAREPsiv APAS PMA2 Cap Plngr L-1 Pos PMA-2 Passive APAS Capture Plunger

Long-1 PosN1-1 A10 DIO SL04 CH16 A PMA-2 OSO 2A 5A

Psiv APAS PMA2 Cap Plngr S-1 Pos PMA-2 Passive APAS Capture Plunger Short-1 Pos

N1-1 A10 DIO SL04 CH17 A PMA-2 OSO 2A 5A

Psiv APAS PMA2 Dep Plngr-1 Pos PMA-2 Passive APAS Departure Plunger-1 N1-1 A10 DIO SL04 CH18 B PMA-2 OSO 2A 5APsiv APAS PMA2 Intf Sealed-1 Pos PMA-2 Passive APAS lnterface Sealed-1 Pos N1-1 A10 DIO SL04 CH19 B PMA-2 OSO 2A 5ASPARE SPARE N1-1 A10 DIO SL04 CH20 SPARE SPARE SPAREGNC Moding Ind PMA2 Active ACS Ind Cmd-1

PMA-2 Talkback Panel Active ACS Ind Cmd-1 N1-1 A10 DIO SL04 CH21 A PMA-2 MCS 2A 5A

GNC Moding lnd PMA2 Free Drift lnd Cmd-1

PMA-2 Talkback Panel Free Drift lnd Cmd-1 N1-1 A10 DIO SL04 CH22 A PMA-2 MCS 2A 5A

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Psiv APAS PMA3 Cap Plngr L-1 Pos PMA-3 Passive APAS Capture Plunger Long-1 Pos




Psiv APAS PMA3 Dep Plngr-1 Pos PMA-3 Passive APAS Departure Plunger-1 Pos


Psiv APAS PMA3 Intf Sealed-1 Pos PMA-3 Passive APAS Interface Sealed-1 Pos N1-1 A10 DIO SL04 CH26 B PMA-3 OSO 3A 16ASPARE SPARE N1-1 A10 DIO SL04 CH27 SPARESPARE SPARE N1-1 A10 DIO SL04 CH28 SPAREGNC Moding Ind PMA3 Active ACS Ind Cmd-1


GNC Moding Ind PMA3 Free Drift Ind Cmd-1

PMA-3 Talkback Panel Free Drift Ind Cmd-1 N1-1 A10 DIO SL04 CH30 A PMA-3 MCS 2A 5A

SPARE SPARE N1-1 A10 DIO SL04 CH31 SPARE

VAV Cont N1-N1 Exc Node-1 Air Mix Rheostat Exc N1-1 A04 LLA SL05 CH00 A Node-1 ECLSS 2A ACVAV Cont N1-N1 Pos Node-1 Air Mix Rheostat Pos N1-1 A04 LLA SL05 CH01 B Node-1 ECLSS 2A ACSmk Det N1-1 Scatter Meas Node-1 Smk Det-1 Scatter Meas N1-1 A04 LLA SL05 CH02 B Node-1 ECLSS 2A ACSmk Det N1-1 Obscuration Meas Node-1 Smk Det-1 Obscuration Meas N1-1 A04 LLA SL05 CH03 A Node-1 ECLSS 2A ACSPARE SPARE N1-1 A04 LLA SL05 CH04 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH05 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH06 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH07 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH08 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH09 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH10 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH11 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH12 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH13 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH14 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH15 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH16 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH17 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH18 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH19 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH20 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH21 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH22 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH23 SPARE SPARE SPARE

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

SPARE SPARE N1-1 A04 LLA SL05 CH24 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH25 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH26 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH27 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH28 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH29 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH30 SPARE SPARE SPARESPARE SPARE N1-1 A04 LLA SL05 CH31 SPARE SPARE SPARE

SPARE SPARE N1-1 All AIO SL06 CH00 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH01 SPARE SPARE SPAREVAV Dmpr N1-N1 Pos Cmd Node-1 Air Mix Vlv Pos Cmd N1-1 All AIO SL06 CH02 B Node-1 ECLSS 2A ACCab Vent Fan N1 Speed Cmd Node-1 Cabin Fan Speed Cmd N1-1 All AIO SL06 CH03 A Node-1 ECLSS 2A ACIMV V N1-Aft Rtn Speed Cmd Node-1 Aft Rtn IMV Vlv Speed Cmd N1-1 All AIO SL06 CH04 B Node-1 ECLSS 2A ACIMV V N1-Aft Sply Speed Cmd Node-1 Aft Sply lMV Vlv Speed Cmd N1-1 All AIO SL06 CH05 A Node-1 ECLSS 2A ACIMV V N1-Port Sply Speed Cmd Node-1 Port Sply IMV Vlv Speed Cmd N1-1 All AIO SL06 CH06 A Node-1 ECLSS 2A ACIMV V N1-Stbd Rtn Speed Cmd Node-1 Stbd Rtn IMV Vlv Speed Cmd N1-1 All AIO SL06 CH07 B Node-1 ECLSS 2A ACIMV V N1-Stbd Sply Speed Cmd Node-1 Stbd Sply lMV Vlv Speed Cmd N1-1 All AIO SL06 CH08 B Node-1 ECLSS 2A ACSPARE SPARE N1-1 All AIO SL06 CH09 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH10 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH11 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH12 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH13 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH14 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH15 SPARE SPARE SPARESPARE SPARE N1-1 All AIO SL06 CH16 SPARE SPARE SPARE

HX Lab LT-A Out RTD Meas Lab LT-A HX Outlet RTD Meas N1-1 A03 LLA SL07 CH00 A Lab TCS 5A 12APri Struct N1 RTD Zone 1-1 Meas Node-1 Shell Zone-1 RTD-1 Meas N1-1 A03 LLA SL07 CH01 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 1-3 Meas Node-1 Shell Zone-1 RTD-3 Meas N1-1 A03 LLA SL07 CH02 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 2-1 Meas Node-1 Shell Zone-2 RTD-1 Meas N1-1 A03 LLA SL07 CH03 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 3-1 Meas Node-1 Shell Zone-3 RTD-1 Meas N1-1 A03 LLA SL07 CH04 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 3-3 Meas Node-1 Shell Zone-3 RTD-3 Meas N1-1 A03 LLA SL07 CH05 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 4-1 Meas Node-1 Shell Zone-4 RTD-1 Meas N1-1 A03 LLA SL07 CH06 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 5-1 Meas Node-1 Shell Zone-5 RTD-1 Meas N1-1 A03 LLA SL07 CH07 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 5-3 Meas Node-1 Shell Zone-5 RTD-3 Meas N1-1 A03 LLA SL07 CH08 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 6-1 Meas Node-1 Shell Zone-6 RTD-1 Meas N1-1 A03 LLA SL07 CH09 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 6-3 Meas Node-1 Shell Zone-6 RTD-3 Meas N1-1 A03 LLA SL07 CH10 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 7-1 Meas Node-1 Shell Zone-7 RTD-1 Meas N1-1 A03 LLA SL07 CH11 B Node-1 TCS 2A AC

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Pri Struct N1 RTD Zone 7-3 Meas Node-1 Shell Zone-7 RTD-3 Meas N1-1 A03 LLA SL07 CH12 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 8-1 Meas Node-1 Shell Zone-8 RTD-1 Meas N1-1 A03 LLA SL07 CH13 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 9-1 Meas Node-1 Shell Zone-9 RTD-1 Meas N1-1 A03 LLA SL07 CH14 B Node-1 TCS 2A ACSPARE SPARE N1-1 A03 LLA SL07 CH15 SPARE SPARE SPARESPARE SPARE N1-1 A03 LLA SL07 CH16 SPARE SPARE SPARESPARE SPARE N1-1 A03 LLA SL07 CH17 SPARE SPARE SPAREPri Struct N2 RTD Zone 1-1 Meas Node-2 Shell Zone-1 RTD-1 Meas N1-1 A03 LLA SL07 CH18 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 2-1 Meas Node-2 Shell Zone-1 RTD-3 Meas N1-1 A03 LLA SL07 CH19 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 9-1 Meas Node-2 Shell Zone-2 RTD-1 Meas N1-1 A03 LLA SL07 CH20 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 3-2 Meas Node-2 Shell Zone-3 RTD-1 Meas N1-1 A03 LLA SL07 CH21 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 5-1 Meas Node-2 Shell Zone-3 RTD-3 Meas N1-1 A03 LLA SL07 CH22 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 6-1 Meas Node-2 Shell Zone-4 RTD-1 Meas N1-1 A03 LLA SL07 CH23 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 7-1 Meas Node-2 Shell Zone-5 RTD-1 Meas N1-1 A03 LLA SL07 CH24 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 1-3 Meas Node-2 Shell Zone-5 RTD-3 Meas N1-1 A03 LLA SL07 CH25 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 2-2 Meas Node-2 Shell Zone-6 RTD-1 Meas N1-1 A03 LLA SL07 CH26 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 9-2 Meas Node-2 Shell Zone-6 RTD-3 Meas N1-1 A03 LLA SL07 CH27 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 3-4 Meas Node-2 Shell Zone-7 RTD-1 Meas N1-1 A03 LLA SL07 CH28 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 5-3 Meas Node-2 Shell Zone-7 RTD-3 Meas N1-1 A03 LLA SL07 CH29 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 6-3 Meas Node-2 Shell Zone-8 RTD-1 Meas N1-1 A03 LLA SL07 CH30 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 7-3 Meas Node-2 Shell Zone-9 RTD-1 Meas N1-1 A03 LLA SL07 CH31 B Node-2 TCS 10A 10A

VAV Dmpr N1-N1 Pos Fdbk Node-1 Air Mix Vlv Pos Fdbk N1-1 A12 HLA SL08 CH00 A Node-1 ECLSS 2A ACIMV Fan N1-Aft Rtn Speed Fdbk Node-1 Aft IMV Fan Speed Fdbk N1-1 A12 HLA SL08 CH01 B Node-1 ECLSS 2A ACCab Vent Fan N1 Speed Fdbk Node-1 Cabin Fan Speed Fdbk N1-1 A12 HLA SL08 CH02 B Node-1 ECLSS 2A ACCab Vent Fan N1 Diff Press Xdcr Meas Node-1 Cabin Fan Diff Press Xdcr Meas N1-1 A12 HLA SL08 CH03 A Node-1 ECLSS 2A ACSPARE SPARE N1-1 A12 HLA SL08 CH04 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH05 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH06 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH07 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH08 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH09 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH10 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH11 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH12 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH13 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH14 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH15 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH16 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH17 SPARE SPARE SPARE

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

SPARE SPARE N1-1 A12 HLA SL08 CH18 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH19 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH20 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH21 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH22 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH23 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH24 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH25 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH26 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH27 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH28 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH29 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH30 SPARE SPARE SPARESPARE SPARE N1-1 A12 HLA SL08 CH31 SPARE SPARE SPARE

SSMDM N1-2 RTD Meas MDM PMA1-2 RTD Meas N1-1 A02 LLA SL09 CH00 A PMA-2 TCS 2A ACPress Shl PMA1 RTD-1 Meas PMA-1 Shell RTD-1 Meas N1-1 A02 LLA SL09 CH01 B PMA-1 TCS 2A ACPress Shl PMA1 RTD-2 Meas PMA-1 Shell RTD-2 Meas N1-1 A02 LLA SL09 CH02 B PMA-1 TCS 2A ACPress Shl PMA1 RTD-3 Meas PMA-1 Shell RTD-3 Meas N1-1 A02 LLA SL09 CH03 A PMA-1 TCS 2A ACPress Shl PMA1 RTD 4 Meas PMA-1 Shell RTD 4 Meas N1-1 A02 LLA SL09 CH04 B PMA-1 TCS 2A ACPress Shl PMA1 RTD-5 Meas PMA-1 Shell RTD-5 Meas N1-1 A02 LLA SL09 CH05 A PMA-1 TCS 2A ACPsiv APAS PMA2 Htch RTD-1 Meas PMA-2 APAS Hatch RTD-1 Meas N1-1 A02 LLA SL09 CH06 A PMA-2 TCS 2A 5APsiv APAS PMA2 Htch RTD-2 Meas PMA-2 APAS Hatch RTD-2 Meas N1-1 A02 LLA SL09 CH07 B PMA-2 TCS 2A 5APsiv APAS PMA2 Htch RTD-3 Meas PMA-2 APAS Hatch RTD-3 Meas N1-1 A02 LLA SL09 CH08 B PMA-2 TCS 2A 5APsiv APAS PMA2 Htch RTD 4 Meas PMA-2 APAS Hatch RTD 4 Meas N1-1 A02 LLA SL09 CH09 A PMA-2 TCS 2A 5ASPARE SPARE N1-1 A02 LLA SL09 CH10 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH11 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH12 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH13 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH14 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH15 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH16 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH17 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH18 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH19 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH20 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH21 SPARE SPARE SPARECMGEA-2 RTD-1 Meas CMGEA-2 RTD-1 Meas N1-1 A02 LLA SL09 CH22 B ITC-Z1 ? ? ?CMGEA-2 RTD-2 Meas CMGEA-2 RTD-2 Meas N1-1 A02 LLA SL09 CH23 A ITC-Z1 ? ? ?

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Card Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

CMGEA-3 RTD-1 Meas CMGEA-3 RTD-1 Meas N1-1 A02 LLA SL09 CH24 A ITC-Z1 ? ? ?CMGEA-3 RTD-2 Meas CMGEA-3 RTD-2 Meas N1-1 A02 LLA SL09 CH25 B ITC-Z1 ? ? ?SPARE SPARE N1-1 A02 LLA SL09 CH26 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH27 SPARE SPARE SPARESPDA Z1-3B Util Rail RTD-1 Meas SPDA Z1-3B Util Rail RTD-1 Meas N1-1 A02 LLA SL09 CH28 B ITC-Z1 TCS 3A ACSPARE SPARE N1-1 A02 LLA SL09 CH29 SPARE SPARE SPARESPARE SPARE N1-1 A02 LLA SL09 CH30 SPARE SPARE SPARESPDA Z1-4B Util Rail RTD-2 Meas SPDA Z1-4B Util Rail RTD-2 Meas N1-1 A02 LLA SL09 CH31 B ITC-Z1 TCS 3A AC

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20 SEP 00


104

N1-2 MDM CHANNEL ASSIGNMENTS(ASSY OPS/3A/FIN/MULTI) Page 1 of 7 PagesName Description MDM Card

RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

HX Lab MT-B lN1 V Norm Fl Pos Lab MT-B HX lnlet Byp Vlv Norm Flow Pos Ind N1-2 A09 DIO SL02 CH00 A LAB TCS 5A 12AHX Lab MT-B IN1 V Byp Fl Cmd Lab MT-B HX Inlet Byp Vlv Byp Flow Pos Ind N1-2 A09 DIO SL02 CH01 A LAB TCS 5A 12AHX Lab MT-B Out V Open Pos Lab MT-B HX Outlet Isln/Rlf Vlv Open Pos Ind N1-2 A09 DIO SL02 CH02 B LAB TCS 5A 12AHX Lab MT-B Out V Cls Pos Lab MT-B HX Outlet Isln/Rlf Vlv Cls Pos Ind N1-2 A09 DIO SL02 CH03 B LAB TCS 5A 12ASmk Det N2-1 Bit Enbl Node-1 Smk Det-2 Bit Enbl N1-2 A09 DIO SL02 CH04 B Node-1 TCS 2A ACVAV Dmpr N1-CU Enbl Cmd Cupola Air Mix Vlv Enable Cmd N1-2 A09 DIO SL02 CH05 A Node-1 ECLSS 2A ACIMV Fan N1-Port Sply On/Off Cmd Node-1 Port IMV Fan On/Off Cmd N1-2 A09 DIO SL02 CH06 A Node-1 ECLSS 2A ACIMV Fan N1-Stbd Rtn On/Off Cmd Node-1 Stbd IMV Fan On/Off Cmd N1-2 A09 DIO SL02 CH07 A Node-1 ECLSS 2A ACSpare Spare N1-2 A09 DIO SL02 CH08 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH09 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH10 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH11 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH12 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH13 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH14 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH15 Spare Spare SpareIMV V N1-Fwd Rtn Open Pos Node-1 Fwd Rtn IMV Vlv Cls Pos N1-2 A09 DIO SL02 CH16 A Node-1 ECLSS 2A ACIMV V N1-Fwd Rtn Enbl Cmd Node-1 Fwd Rtn IMV Vlv Enbl Cmd N1-2 A09 DIO SL02 CH17 A Node-1 ECLSS 2A ACIMV V N1-Fwd Rtn Cls Pos Node-1 Fwd Rtn IMV Vlv Open Pos N1-2 A09 DIO SL02 CH18 B Node-1 ECLSS 2A ACIMV V N1-Fwd Sply Open Pos Node-1 Fwd Sply IMV Vlv Open Pos N1-2 A09 DIO SL02 CH19 B Node-1 ECLSS 2A ACIMV V N1-Fwd Sply Cls Pos Node-1 Fwd Sply IMV Vlv Cls Pos N1-2 A09 DIO SL02 CH20 B Node-1 ECLSS 2A ACIMV V N1-Fwd Sply Enbl Cmd Node-1 Fwd Sply IMV Vlv Enbl Cmd N1-2 A09 DIO SL02 CH21 A Node-1 ECLSS 2A ACIMV V N1-Nad Rtn Open Pos Node-1 Nad Rtn IMV Vlv Open Pos N1-2 A09 DIO SL02 CH22 A Node-1 ECLSS 2A ACIMV V N1-Nad Rtn Cls Pos Node-1 Nad Rtn IMV Vlv Cls Pos N1-2 A09 DIO SL02 CH23 A Node-1 ECLSS 2A ACIMV V N1-Nad Rtn Enbl Cmd Node-1 Nad Rtn IMV Vlv Enbl Cmd N1-2 A09 DIO SL02 CH24 A Node-1 ECLSS 2A ACIMV V N1-Nad Sply Enbl Cmd Node-1 Nad Sply IMV Vlv Enbl Cmd N1-2 A09 DIO SL02 CH25 A Node-1 ECLSS 2A ACIMV V N1-Nad Sply Open Pos Node-1 Nad Sply IMV Vlv Open Pos N1-2 A09 DIO SL02 CH26 B Node-1 ECLSS 2A ACIMV V N1-Nad Sply Cls Pos Node-1 Nad Sply IMV Vlv Cls Pos N1-2 A09 DIO SL02 CH27 B Node-1 ECLSS 2A ACSpare Spare N1-2 A09 DIO SL02 CH28 Spare Spare ECLSSSpare Spare N1-2 A09 DIO SL02 CH29 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH30 Spare Spare SpareSpare Spare N1-2 A09 DIO SL02 CH31 Spare Spare Spare

SSMDM N1-1 Htr Pwr MDM PMA1-1 Htr Pwr N1-2 A05 SDO SL03 CH00 n/a PMA-1 TCS 2A ACHX Lab MT-B IN1 V Norm Fl Cmd Lab MT-B HX Inlet Byp Vlv Norm Flow Cmd N1-2 A05 SDO SL03 CH01 n/a LAB TCS 5A 12AHX Lab MT-B IN1 V Byp Fl Cmd Lab MT-B HX Inlet Byp Vlv Byp Flow Cmd N1-2 A05 SDO SL03 CH02 n/a LAB TCS 5A 12AHX Lab MT-B Out V Open Cmd Lab MT-B HX Outlet Isln/Rlf Vlv Open Cmd N1-2 A05 SDO SL03 CH03 n/a LAB TCS 5A 12AHX Lab MT-B Out V Cls Cmd Lab MT-B HX Outlet Isln/Rlf Vlv Cls Cmd N1-2 A05 SDO SL03 CH04 n/a LAB TCS 5A 12ARnd Win Htr-1 Enbl Cmd Cupola Rnd Window Htr-1 Enbl Cmd N1-2 A05 SDO SL03 CH05 n/a Cupola TCS 10A AC

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RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Rnd Win Htr-2 Enbl Cmd Cupola Rnd Window Htr-2 Enbl Cmd N1-2 A05 SDO SL03 CH06 n/a Cupola TCS 10A ACTrap Win 1 Htr Enbl Cmd Cupola Trap Window-1 Htr Enbl Cmd N1-2 A05 SDO SL03 CH07 n/a Cupola TCS 10A ACTrap Win 2 Htr Enbl Cmd Cupola Trap Window-2 Htr Enbl Cmd N1-2 A05 SDO SL03 CH08 n/a Cupola TCS 10A ACTrap Win 3 Htr Enbl Cmd Cupola Trap Window-3 Htr Enbl Cmd N1-2 A05 SDO SL03 CH09 n/a Cupola TCS 10A ACTrap Win 4 Htr Enbl Cmd Cupola Trap Window-4 Htr Enbl Cmd N1-2 A05 SDO SL03 CH10 n/a Cupola TCS 10A ACTrap Win 5 RTD-1 Meas Cupola Trap Window-5 Hrt Enbl Cmd N1-2 A05 SDO SL03 CH11 n/a Cupola TCS 10A ACTrap Win 6 RTD-1 Meas Cupola Trap Window-6 Htr Enbl Cmd N1-2 A05 SDO SL03 CH12 n/a Cupola TCS 10A ACSpare Spare N1-2 A05 SDO SL03 CH13 n/a Spare SpareSpare Spare N1-2 A05 SDO SL03 CH14 n/a Spare SpareSpare Spare N1-2 A05 SDO SL03 CH15 n/a Spare SpareSpare Spare N1-2 A05 SDO SL03 CH16 n/a Spare SpareSpare Spare N1-2 A10 DIO SL04 CH00 Spare Spare Spare

Spare Spare N1-2 A10 DIO SL04 CH01 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH02 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH03 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH04 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH05 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH06 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH07 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH08 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH09 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH10 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH11 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH12 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH13 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH14 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH15 Spare Spare SparePsiv APAS PMA2 Cap Plngr L-2 Pos PMA-2 Passive APAS Capture Plunger

Long-2 PosN1-2 A10 DIO SL04 CH16 A PMA-2 OSO 2A 5A



Psiv APAS PMA2 Dep Plngr-2 Pos PMA-2 Passive APAS Departure Plngr-2 Pos N1-2 A10 DIO SL04 CH18 B PMA-2 OSO 2A 5APsiv APAS PMA2 Intf Sealed-2 Pos PMA-2 Passive APAS Interface Sealed-2 Pos N1-2 A10 DIO SL04 CH19 B PMA-2 OSO 2A 5ASpare Spare DIO SL04 CH20 Spare Spare SpareGNC Moding Ind PMA2 Active ACS Ind Cmd-2


GNC Moding Ind PMA2 Free Drift Ind PMA-2 Talkback Panel Free Drift Ind Cmd-2 N1-2 A10 DIO SL04 CH22 A PMA-2 MCS 2A 5A

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RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Psiv APAS PMA3 Cap Plngr L-2 Pos PMA-3 Passive APAS Capture Plngr Long-2 Pos


Psiv APAS PMA3 Cap Plngr S-2 Pos PMA-3 Passive APAS Capture Plngr Short-2 Pos


Psiv APAS PMA3 Dep Plngr-2 Pos PMA-3 Passive APAS Departure Plngr-2 Pos N1-2 A10 DIO SL04 CH25 A PMA-3 OSO 3A 16APsiv APAS PMA3 Intf Sealed-2 Pos PMA-3 Passive APAS Interface Sealed-2 Pos N1-2 A10 DIO SL04 CH26 B PMA-3 OSO 3A 16ASpare Spare N1-2 A10 DIO SL04 CH27 Spare Spare SpareSpare Spare N1-2 A10 DIO SL04 CH28 Spare Spare SpareGNC Moding Ind PMA3 Active ACS Ind Cmd-2

PMA3 Talkback Panel Active ACS Ind Cmd-2 N1-2 A10 DIO SL04 CH29 A PMA-3 MCS 3A 16A

GNC Moding Ind PMA3 Free Drift Ind Cmd-2

PMA-3 Talkback Panel Free Drift Ind Cmd-2 N1-2 A10 DIO SL04 CH30 A PMA-3 MCS 3A 16A

Spare Spare N1-2 A10 DIO SL04 CH31 Spare Spare Spare

VAV Cont CU-CU Pos CUPOLA Air Mix Rheostat Pos N1-2 A04 LLA SL05 CH00 A Cupola ECLSS 2A ACVAV Cont CU-CU Exc CUPOLA Air Mix Rheostat Exc N1-2 A04 LLA SL05 CH01 B Cupola ECLSS 2A ACSmk Det N2-1 Scatter Meas Node-1 Smk Det-2 Scatter Meas N1-2 A04 LLA SL05 CH02 B Node-1 ECLSS 2A ACSmk Det N2-1 Obscuration Meas Node-1 Smk Det-2 Obscuration Meas N1-2 A04 LLA SL05 CH03 A Node-1 ECLSS 2A ACRnd Win RTD-1 Meas Cupola Rnd Window RTD-1A Meas N1-2 A04 LLA SL05 CH04 B Cupola TCS 10A ACRnd Win RTD-3 Meas Cupola Rnd Window RTD-2A Meas N1-2 A04 LLA SL05 CH05 A Cupola TCS 10A ACTrap Win 1 RTD-1 Meas Cupola Trap Window-1 RTD-1 Meas N1-2 A04 LLA SL05 CH06 A Cupola TCS 10A ACTrap Win 1 RTD-3 Meas Cupola Trap Window-1 RTD-3 Meas N1-2 A04 LLA SL05 CH07 B Cupola TCS 10A ACTrap Win 2 RTD-1 Meas Cupola Trap Window-2 RTD-1 Meas N1-2 A04 LLA SL05 CH08 B Cupola TCS 10A ACTrap Win 2 RTD-3 Meas Cupola Trap Window-2 RTD-3 Meas N1-2 A04 LLA SL05 CH09 A Cupola TCS 10A ACTrap Win 3 RTD-1 Meas Cupola Trap Window-3 RTD-1 Meas N1-2 A04 LLA SL05 CH10 A Cupola TCS 10A ACTrap Win 3 RTD-3 Meas Cupola Trap Window-3 RTD-3 Meas N1-2 A04 LLA SL05 CH11 B Cupola TCS 10A ACTrap Win 4 RTD-1 Meas Cupola Trap Window 4 RTD-1 Meas N1-2 A04 LLA SL05 CH12 A Cupola TCS 10A ACTrap Win 4 RTD-3 Meas Cupola Trap Window-4 RTD-3 Meas N1-2 A04 LLA SL05 CH13 B Cupola TCS 10A ACTrap Win 5 Htr Enbl Cmd Cupola Trap Window-5 RTD-1 Meas N1-2 A04 LLA SL05 CH14 B Cupola TCS 10A ACTrap Win 5 RTD-3 Meas Cupola Trap Window-5 RTD-3 Meas N1-2 A04 LLA SL05 CH15 A Cupola TCS 10A ACTrap Win 6 Htr Enbl Cmd Cupola Trap Window-6 RTD-1 Meas N1-2 A04 LLA SL05 CH16 B Cupola TCS 10A ACTrap Win 6 RTD-3 Meas Cupola Trap Window-6 RTD-3 Meas N1-2 A04 LLA SL05 CH17 A Cupola TCS 10A ACRnd Win RTD-2 Meas Cupola Rnd Window RTD-1B Meas N1-2 A04 LLA SL05 CH18 A Cupola TCS 10A ACRnd Win RTD-4 Meas Cupola Rnd Window RTD-2B Meas N1-2 A04 LLA SL05 CH19 B Cupola TCS 10A ACTrap Win 1 RTD-2 Meas Cupola Trap Window-1 RTD-2 Meas N1-2 A04 LLA SL05 CH20 A Cupola TCS 10A ACTrap Win 1 RTD 4 Meas Cupola Trap Window-1 RTD-4 Meas N1-2 A04 LLA SL05 CH21 B Cupola TCS 10A ACTrap Win 2 RTD-2 Meas Cupola Trap Window-2 RTD-2 Meas N1-2 A04 LLA SL05 CH22 B Cupola TCS 10A ACTrap Win 2 RTD 4 Meas Cupola Trap Window-2 RTD-4 Meas N1-2 A04 LLA SL05 CH23 A Cupola TCS 10A ACTrap Win 3 RTD-2 Meas Cupola Trap Window-3 RTD-2 Meas N1-2 A04 LLA SL05 CH24 A Cupola TCS 10A AC

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RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Trap Win 3 RTD-4 Meas Cupola Trap Window-3 RTD-4 Meas N1-2 A04 LLA SL05 CH25 B Cupola TCS 10A ACTrap Win 4 RTD-2 Meas Cupola Trap Window-4 RTD-2 Meas N1-2 A04 LLA SL05 CH26 B Cupola TCS 10A ACTrap Win 4 RTD 4 Meas Cupola Trap Window 4 RTD-4 Meas N1-2 A04 LLA SL05 CH27 A Cupola TCS 10A ACTrap Win 5 RTD-2 Meas Cupola Trap Window-5 RTD-2 Meas N1-2 A04 LLA SL05 CH28 B Cupola TCS 10A ACTrap Win 5 RTD-4 Meas Cupola Trap Window-5 RTD-4 Meas N1-2 A04 LLA SL05 CH29 A Cupola TCS 10A ACTrap Win 6 RTD-2 Meas Cupola Trap Window-6 RTD-2 Meas N1-2 A04 LLA SL05 CH30 A Cupola TCS 10A ACTrap Win 6 RTD-4 Meas Cupola Trap Window-6 RTD-4 Meas N1-2 A04 LLA SL05 CH31 B Cupola TCS 10A AC

Spare Spare N1-2 A11 AIO SL06 CH00 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH01 Spare Spare SpareVAV Dmpr N1-CU Pos Cmd Cupola Air Mix Vlv Pos Cmd N1-2 A11 AIO SL06 CH02 B LS TCS 2A ACSpare Spare N1-2 A11 AIO SL06 CH03 Spare Spare SpareIMV V N1-Fwd Rtn Speed Cmd Node-1 Fwd Rtn IMV Vlv Speed Cmd N1-2 A11 AIO SL06 CH04 B Node-1 ECLSS 2A ACIMV V N1-Fwd Sply Speed Cmd Node-1 Fwd Sply IMV Vlv Speed Cmd N1-2 A11 AIO SL06 CH05 A Node-1 ECLSS 2A ACIMV V N1-Nad Rtn Speed Cmd Node-1 Nad Rtn IMV Vlv Speed Cmd N1-2 A11 AIO SL06 CH06 A Node-1 ECLSS 2A ACIMV V N1-Nad Sply Speed Cmd Node-1 Nad Sply IMV Vlv Speed Cmd N1-2 A11 AIO SL06 CH07 B Node-1 ECLSS 2A ACSpare Spare N1-2 A11 AIO SL06 CH08 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH09 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH10 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH11 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH12 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH13 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH14 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH15 Spare Spare SpareSpare Spare N1-2 A11 AIO SL06 CH16 Spare Spare Spare

HX Lab MT-B Out Rtd Meas Lab MT-B HX Outlet RTD Meas N1-2 A03 LLA SL07 CH00 A LAB TCSPn Struct N1 RTD Zone 1-2 Meas Node-1 Shell Zone-1 RTD-2 Meas N1-2 A03 LLA SL07 CH01 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 1-4 Meas Node-1 Shell Zone-1 RTD-4 Meas N1-2 A03 LLA SL07 CH02 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 2-2 Meas Node-1 Shell Zone-2 RTD-2 Meas N1-2 A03 LLA SL07 CH03 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 3-2 Meas Node-1 Shell Zone-3 RTD-2 Meas N1-2 A03 LLA SL07 CH04 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 3-4 Meas Node-1 Shell Zone-3 RTD-4 Meas N1-2 A03 LLA SL07 CH05 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 4-2 Meas Node-1 Shell Zone 4 RTD-2 Meas N1-2 A03 LLA SL07 CH06 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 5-2 Meas Node-1 Shell Zone-5 RTD-2 Meas N1-2 A03 LLA SL07 CH07 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 5-4 Meas Node-1 Shell Zone-5 RTD-4 Meas N1-2 A03 LLA SL07 CH08 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 6-2 Meas Node-1 Shell Zone-6 RTD-2 Meas N1-2 A03 LLA SL07 CH09 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 6-4 Meas Node-1 Shell Zone-6 RTD-4 Meas N1-2 A03 LLA SL07 CH10 A Node-1 TCS 2A ACPri Struct N1 RTD Zone 7-2 Meas Node-1 Shell Zone-7 RTD-2 Meas N1-2 A03 LLA SL07 CH11 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 7-4 Meas Node-1 Shell Zone-7 RTD-4 Meas N1-2 A03 LLA SL07 CH12 A Node-1 TCS 2A AC

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RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Pri Struct N1 RTD Zone 8-2 Meas Node-1 Shell Zone-8 RTD-2 Meas N1-2 A03 LLA SL07 CH13 B Node-1 TCS 2A ACPri Struct N1 RTD Zone 9-2 Meas Node-1 Shell Zone-9 RTD-2 Meas N1-2 A03 LLA SL07 CH14 B Node-1 TCS 2A ACSpare Spare N1-2 A03 LLA SL07 CH15 Spare Spare SpareSpare Spare N1-2 A03 LLA SL07 CH16 Spare Spare SpareSpare Spare N1-2 A03 LLA SL07 CH17 Spare Spare SparePri Struct N2 RTD Zone 1-2 Meas Node-2 Shell Zone-1 RTD-2 Meas N1-2 A03 LLA SL07 CH18 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 8-1 Meas Node-2 Shell Zone-1 RTD-4 Meas N1-2 A03 LLA SL07 CH19 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 3-1 Meas Node-2 Shell Zone-2 RTD-2 Meas N1-2 A03 LLA SL07 CH20 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 4-1 Meas Node-2 Shell Zone-3 RTD-2 Meas N1-2 A03 LLA SL07 CH21 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 5-2 Meas Node-2 Shell Zone-3 RTD-4 Meas N1-2 A03 LLA SL07 CH22 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 6-2 Meas Node-2 Shell Zone 4 RTD-2 Meas N1-2 A03 LLA SL07 CH23 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 7-2 Meas Node-2 Shell Zone-5 RTD-2 Meas N1-2 A03 LLA SL07 CH24 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 1-4 Meas Node-2 Shell Zone-5 RTD-4 Meas N1-2 A03 LLA SL07 CH25 B Node-2 TCS 10A 10APrl Struct N2 RTD Zone 8-2 Meas Node-2 Shell Zone-6 RTD-2 Meas N1-2 A03 LLA SL07 CH26 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 3-3 Meas Node-2 Shell Zone-6 RTD-4 Meas N1-2 A03 LLA SL07 CH27 A Node-2 TCS 10A 10APri Struct N2 RTD Zone 4-2 Meas Node-2 Shell Zone-7 RTD-2 Meas N1-2 A03 LLA SL07 CH28 B Node-2 TCS 10A 10APri Struct N2 RTD Zone 5-4 Meas Node-2 Shell Zone-7 RTD-4 Meas N1-2 A03 LLA SL07 CH29 A Node-2 TCS 10A 10APn Struct N2 RTD Zone 6-4 Meas Node-2 Shell Zone-8 RTD-2 Meas N1-2 A03 LLA SL07 CH30 A Node-2 TCS 10A 10APn Struct N2 RTD Zone 7-4 Meas Node-2 Shell Zone-9 RTD-2 Meas N1-2 A03 LLA SL07 CH31 B Node-2 TCS 10A 10A

VAV Dmpr N1-CU Pos Fdbk Cupola Air Mix Vlv Pos Fdbk N1-2 A12 HLA SL08 CH00 A LS ECLSS 2A ACIMV Fan N1-Port Sply Speed Cmd Node-1 Port IMV Fan Speed Fdbk N1-2 A12 HLA SL08 CH01 B Node-1 ECLSS 2A ACIMV Fan N1-Stbd Rtn Speed Cmd Node-1 Stbd IMV Fan Speed Fdbk N1-2 A12 HLA SL08 CH02 B Node-1 ECLSS 2A ACAbs Press Xdcr N1 Meas Node-1 Cabin Press Xdcr Meas N1-2 A12 HLA SL08 CH03 A Node-1 ECLSS 2A ACSpare Spare N1-2 A12 HLA SL08 CH04 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH05 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH06 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH07 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH08 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH09 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH10 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH11 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH12 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH13 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH14 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH15 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH16 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH17 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH18 Spare Spare Spare

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RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

Spare Spare N1-2 A12 HLA SL08 CH19 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH20 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH21 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH22 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH23 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH24 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH25 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH26 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH27 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH28 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH29 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH30 Spare Spare SpareSpare Spare N1-2 A12 HLA SL08 CH31 Spare Spare Spare

SSMDM N1-1 RTD Meas MDM PMA1-1 RTD Meas N1-2 A02 LLA SL09 CH00 A PMA-1 TCSPress Shl PMA1 RTD-6 Meas PMA-1 Shell RTD-6 Meas N1-2 A02 LLA SL09 CH01 B PMA-1 TCS 2A ACPress Shl PMA1 RTD-7 Meas PMA-1 Shell RTD-7 Meas N1-2 A02 LLA SL09 CH02 B PMA-1 TCS 2A ACPress Shl PMA1 RTD-8 Meas PMA-1 Shell RTD-8 Meas N1-2 A02 LLA SL09 CH03 A PMA-1 TCS 2A ACPress Shl PMA1 RTD-9 Meas PMA-1 Shell RTD-9 Meas N1-2 A02 LLA SL09 CH04 B PMA-1 TCSPress Shl PMA1 RTD-10 Meas PMA-1 Shell RTD-10 Meas N1-2 A02 LLA SL09 CH05 A PMA-1 TCS 2A ACPsiv APAS PMA3 Htch RTD-1 Meas PMA-3 APAS Hatch RTD-1 Meas N1-2 A02 LLA SL09 CH06 A PMA-3 TCS 3A 16APslv APAS PMA3 Htch RTD-2 Meas PMA-3 APAS Hatch RTD-2 Meas N1-2 A02 LLA SL09 CH07 B PMA-3 TCS 3A 16APsiv APAS PMA3 Htch RTD-3 Meas PMA-3 APAS Hatch RTD-3 Meas N1-2 A02 LLA SL09 CH08 B PMA-3 TCS 3A 16APsiv APAS PMA3 Htch RTD-4 Meas PMA-3 APAS Hatch RTD-4 Meas N1-2 A02 LLA SL09 CH09 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-1 Meas PMA-3 Shell RTD-1 Meas N1-2 A02 LLA SL09 CH10 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-2 Meas PMA-3 Shell RTD-2 Meas N1-2 A02 LLA SL09 CH11 B PMA-3 TCS 3A 16APress Shl PMA3 RTD-3 Meas PMA-3 Shell RTD-3 Meas N1-2 A02 LLA SL09 CH12 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-4 Meas PMA-3 Shell RTD-4 Meas N1-2 A02 LLA SL09 CH13 B PMA-3 TCS 3A 16APress Shl PMA3 RTD-5 Meas PMA-3 Shell RTD-5 Meas N1-2 A02 LLA SL09 CH14 B PMA-3 TCS 3A 16APress Shl PMA3 RTD-6 Meas PMA-3 Shell RTD-6 Meas N1-2 A02 LLA SL09 CH15 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-7 Meas PMA-3 Shell RTD-7 Meas N1-2 A02 LLA SL09 CH16 B PMA-3 TCS 3A 16APress Shl PMA3 RTD-8 Meas PMA-3 Shell RTD-8 Meas N1-2 A02 LLA SL09 CH17 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-9 Meas PMA-3 Shell RTD-9 Meas N1-2 A02 LLA SL09 CH18 A PMA-3 TCS 3A 16APress Shl PMA3 RTD-10 Meas PMA-3 Shell RTD-10 Meas N1-2 A02 LLA SL09 CH19 B PMA-3 TCS 3A 16ASpare Spare N1-2 A02 LLA SL09 CH20 Spare Spare SpareSpare Spare N1-2 A02 LLA SL09 CH21 Spare Spare SpareCMGEA-1 RTD-1 Meas CMGEA-1 RTD-1 Meas N1-2 A02 LLA SL09 CH22 B FGB MCSCMGEA-1 RTD-2 Meas CMGEA-1 RTD-2 Meas N1 2 A02 LLA SL09 CH23 A ITS-Z1 MCSCMGEA-4 RTD-1 Meas CMGEA-4 RTD-1 Meas N1-2 A02 LLA SL09 CH24 A ITS-Z1 MCS

23 JUN 00 6337.xls

110


RefdesCard Type

Slot No.

Chanl No.

Chanl Type

ISS Element

OPS Position

Flight Activation

Flight Deactivation

CMGEA-4 RTD-2 Meas CMGEA-4 RTD-2 Meas N1-2 A02 LLA SL09 CH25 B ITS-Z1 MCSSpare Spare N1-2 A02 LLA SL09 CH26 Spare SpareSpare Spare N1-2 A02 LLA SL09 CH27 Spare SpareSPDA Z1-3B Util Rail RTD-2 Meas SPDA Z1-3B Util Rail RTD-2 Meas N1-2 A02 LLA SL09 CH28 B ITS-Z1 EPSSpare Spare N1-2 A02 LLA SL09 CH29 Spare Spare SpareSpare Spare N1-2 A02 LLA SL09 CH30 Spare Spare SpareSPDA Z1-4B Util Rail RTD-1 Meas SPDA Z1-4B Util Rail RTD-1 Meas N1-2 A02 LLA SL09 CH31 B ITS-Z1 EPS

23 JUN 00 6337.xls

111

20 SEP 00


112

COMM MALFUNCTION POINTS(ASSY OPS/3A/FIN) Page 1 of 1 page

23 JUN 007729.doc

113

20 SEP 00


114

PL/DPS RECONFIGURATION(ASSY OPS/3A/FIN A) Page 1 of 2 pages

19 SEP 006292.doc

PROCEDURE SECUREACTION

RECOVERYACTION

INFO

PL1(2) MDM I/O ERROR/MDM OUTPUT (FDF, ORBPKT, DPS)

N/A A,C N/A

I/O ERROR PL 1(2); MDM OUTPUT PL1(2) (FDF,MAL, DPS)

N/A A,C N/A

PASS SM GPC FAIL (FDF, ORB PKT, DPS) N/A C,D BCS SPLIT (FDF, MAL, DPS) N/A C,D BGNC RECOVERY VIA G2FD (FDF, ORB PKT, DPS) N/A N/A N/AI/O ERROR FLEX (FDF, MAL, DPS) N/A N/A N/ABCE BYP FLEX (FDF, MAL, DPS) N/A N/A N/ABCE BYP PL1(2) (FDF, MAL) N/A A,C N/AGPC FRP-4 PASS RECOVERY AFTER BFS ENGAGE(FDF, MAL, DPS)

N/A C,D B

GPC FRP-7 DPS RECONFIG FOR LOSS OF AV BAYCOOLING (FDF, MAL)

N/A C,D B

DPS SSR-3 GNC REASSIGNMENT (FDF, MAL) N/A N/A BDPS SSR-4 SM REASSIGNMENT (FDF, MAL) N/A C,D BECLS SSR-10 H20 PUMP OPS VIA GPC (FDF, MAL,ECLS)

N/A N/A N/A

ACTION AIf ‘I/O ERROR PL1’ message

Loss of primary ground and crew interface to ISS via PSP 1/OIU 1.If failure at IOP XMTR/RCVR at SM GPC, port mode to select PF2.

If ‘I/O ERROR PL2’ messageLoss of secondary ground and crew interface to ISS via PSP 2/OIU 2.If failure at IOP XMTR/RCVR at SM GPC

If PL1 interface with SM GPC failed, √MCC for SM reassignment.If PL2 interface with SM GPC OK, port mode to select PF1.

ACTION BLoss of ground and orbiter commanding to ISS via OIU 1(2).

ACTION CIf PF1 failed, √MCC and perform following

If PSP 2 I/O reset not previously performedSM 62 PCMMU/PL COMM

I/O RESET PSP 2 − ITEM 7 EXECNotify MCC when complete.

If PF1 or SM GPC recoveredIf PSP 1 I/O reset not previously performed

SM 62 PCMMU/PL COMMI/O RESET PSP 1 − ITEM 6 EXECNotify MCC when complete.

If PF2 or SM GPC recoveredIf OSVS powered

SM 225 SVS CONTROL

115

PL/DPS RECONFIGURATION(ASSY OPS/3A/FIN A) Page 2 of 2 pages

19 SEP 006292.doc

PROCESS SVS COMMANDS – ITEM 1 EXEC (*)ITEM 1 EXEC ( )

ACTION DReload PDI DECOM FORMAT (FDF, ORB OPS FS, COMM/INST).As required, reenable PDI DECOM FDA.Resume SPEC 62.

116

APCU APCU AMPS ↑(ASSY OPS/3A/FIN) Page 1 of 2 pages

23 JUN 006293.doc

2

1

3

1

Assumes RPCMRTs are enabled.

2

MCC will determinebetween atransducer shift anda real singleconverter failure.

3

Total output for eachAPCU must bemaintained less than14.7 amps and eachconv output must bemaintained less than8.5 amps.

APCU TRIP

RPC TRIP OR POWER LOSS,all (SODF: ISS MAL: EPS)

SMALERT

S200 APCU 1(2)AMPS HIGH

Nominal Config:L12 (SSP 1)cb SW PWR 1 − clAPCU 1 CONV − ON(tb-gray)

APCU 1 OUTPUTRLY − CL (tb-gray)

APCU 2 CONV − ON(tb-gray)


(R1)PRI PL MNC − ON(tb-ON)

PL CAB − MNB(MNA)

PL AUX − ON

If any APCU CONVAMPS ≥ 8.5

1 √APCU Status

SM 200 APCU STATUS

APCU 1(2) TRIP > -4.40?

3 √RPCM Status

NODE 1: EPSNODE 1: EPS

•√RPCM N13B(4B) A,B,C(three) − active

All three RPCMs active?4

Affected APCU CONV AAMPS = CONV B AMPS± 3?

5 Transient condition

6

• Continue nominaloperations

9

7 Transducer shift orsingle conv failure

8

•√MCC

9

Affected APCU CONV AAMPS + CONV B AMPS> 14.7?

4

10 APCU heavily loaded.

11 CONV A and CONVB outputs not balanced.

12

Manage APCU loads suchthat CONV A amps +CONV B amps < 14.7 amps

• Perform EPS SSR-7(8)APCU 1(2) LOADPOWERDOWN (SODF:ISS MAL: EPS) until totaloutput < 14.7 amps orsingle CONV output < 8.5amps.

1No

Yes

No

13

Yes

No

2

Any APCU 1(2) CONV A(B)AMPS > 8.5?

Yes

No

Yes

Yes No

117

APCU APCU AMPS ↑(ASSY OPS/3A/FIN) Page 2 of 2 pages

23 JUN 006293.doc

4

4

Loss of APCU 1causes the loss ofthe N13B. Loss ofAPCU 2 causes theloss of the N14Bbus.

EPS SSR-3(4) (SODF: ISS MAL:EPS) for N13B (N14B) bus loss

13

Is CONV A amps + CONVB amps still > 14.7 or singleconverter amps > 8.5?

14

• Continue with currentconfiguration.

15

(L12/SSP 1)• APCU 1(2) CONV − OFF

(tb-bp)• APCU 1(2) OUTPUT

RLY − OP (tb-bp)

If APCU 2 affected andcrew ingressed,• Turn on portable fans

installed in NODE 1

16

On MCC GO• APCU 1(2) CONV − ON

(tb-gray)

•√APCU AMPS

CONV A + CONV B amps> 14.7 or single converteramps > 8.5?

17 APCU internal short.

18 Short downstream ofAPCU.

19


(tb-bp)

12

Yes

No

No

Yes

118

APCU APCU TEMP ↓↑(ASSY OPS/3A/FIN) Page 1 of 1 page

23 JUN 006294.doc

1

1

1

Loss of APCU 1causes the loss ofthe N13B bus. Lossof APCU 2 causesthe loss of the N14Bbus.

2

MCC will determinebetween atransducer shift anda real circuitryfailure.

2

APCU VOLTS

APCU AMPS

APCU TRIP

SMALERT

S200 APCU 1(2)TMP LIMIT






PL CAB − MNB(MNA)

PL AUX − ON

1 √APCU Status

SM 200 APCUSTATUS

APCU 1(2) TRIP > -4.40

Any APCU 1(2) CONV A(B)AMPS > 8.5

APCU 1(2) VOLTS RESHIGH < 122 or > 126.5

All APCU 1,2 CONV A,BTEMPS (four) ≥ 130 and/orrising or ≤ 20

None of the above

If APCU 1(2) CONVTEMP A(B)≤ 20 or ≥ 130

2 Orbiter coolingproblem

3

(L12/SSP 1)• APCU 1,2 CONV (two) −

OFF (tb-bp)• APCU 1,2 OUTPUT RLY

(two) − OP (tb-bp)

4

CONV A and CONV BTEMPS in a singleoperating APCU ≥ 130 andrising or ≤ 20?

5 Single APCU coolingproblem or circuit failure 6

• Go to EPS SSR-3,4(SODF: ISS MAL: EPS)for N13B and N14B busloss

7

Affected APCU:(L12/SSP 1)• APCU 1(2) CONV − OFF


RLY − OP (tb-bp)

8

• Go to EPS SSR-3(4)(SODF: ISS MAL: EPS)for N13B(N14B) bus loss

9

Single CONV TEMP ≥ 130or ≤ 20?

10 Temp ducer shift orconverter circuit failure

11

•√MCC

12 Transient temperatureshift or transducer shift

13

• Continue nominaloperations.

1

1

1

No

Yes

No

Yes

119

20 SEP 00


120

APCU APCU TRIP(ASSY OPS/3A/FIN) Page 1 of 3 pages

23 JUN 006296.doc

1

MCC will determinecause of interruptionof power or signal tothe APCUs.

1

APCU AMPS

APCU VOLTS

APCU TEMPSM

ALERT

S200 APCU 1(2)TRIP






PL CAB − MNB(MNA)

PL AUX − ON

If APCU TRIP> -4.4

√APCU TRIPSTATUS TABLE

1 √APCU Status

(L12/SSP 1)APCU 1,2 CONV (two)tb - bp

andAPCU 1,2 OUTPUT RLY(two) tb - bp

andSM 200 APCUSTATUS

bothAPCU 1 TRIP and APCU 2TRIP approx = 0

Both APCU 1 TRIP > -4.40and APCU 2 TRIP > -4.40

None of the above

2

(ORB R1)•√PRI PL tbs

All tbs OFF? 3

•√MCC

4 PRI PL Busdisconnect

5 Both APCUs tripped 6

•√APCU TRIP STATUSTABLE

•√MCC

8 Transient tripindication

9


10

•√Affected APCU CONVamps

Both A and B amps = 0.3L? 11 Both A and BConverters tripped

12

SM 200 APCUSTATUS

• Record TRIP Status ____•√APCU TRIP STATUS

TABLE

(L12/SSP 1)• Affected APCU 1(2)

CONV − OFF (tb-bp)• Affected APCU 1(2)

OUTPUT RLY − OP(tb-bp)

13

•√Affected APCU CONVamps

CONV A amps = 0.3L orCONV B amps = 0.3L?

14 False trip indicator

15

•√MCC

Yes

No

17

19

16

1

1

1

7

Either APCU 1 TRIP > -4.40or APCU 2 TRIP > -4.40?

No

Yes

1

No

Yes

No

Yes

121


23 JUN 006296.doc

23

2


3

MCC will considerrecovery actions.May activatedownstream loadsone at a time to findshorted load.

EPS SSR-3(4) N13B(N14B)(SODF: ISS MAL: EPS)

EPS SSR 9(10) APCU 1(2)CONTROLLED REPOWER,step 2, (SODF: ISS MAL: EPS)

16 Repower PRI PL BUS

• Perform A PWRDN (FDFPL PWRDN, ORB PKT,PL PWRDN ORB), then:

• Perform EPS SSR-150ALTERNATE PRIMARYPAYLOAD PWR (FDF,MAL, EPS), then

If PRI PL recovered,• Perform A PWRUP (FDF

PL PWRDN, ORB PKT,PL PWRDN ORB), then

17

(L12/SSP 1)• Affected APCU CONV −

ON (tb-gray)

•√Affected APCU CONVamps and TRIP STATUS

Affected APCU TRIPindication or affected APCUCONV A amps + CONV Bamps > 14.7

orSingle CONV amps > 8.5?

18 Unisolatable short inAPCU or trip circuitryfailure

19 Single Convertertripped

20


OFF (tb-bp)• Affected APCU OUTPUT

RLY − CL (tb-bp)• Affected APCU CONV −

ON (tb-gray)•√APCU OUTPUT RLY

tb - gray

•√APCU CONV amps andTRIP STATUS

Affected APCU TRIPindication or affected APCUCONV A amps + CONV Bamps > 14.7

orSingle CONV amps > 8.5?

21

SM 200 APCUSTATUS

• Record Trip Status ____•√APCU TRIP STATUS

TABLE• Manage remaining

converters so that CONVamps ≤ 8.5.

• If required, performSSR-7(8) APCU 1(2)LOAD POWERDOWN(SODF: ISS MAL: EPS),then:

22 Unisolatable shortdownstream of APCU

23 Inadvertent trip orpossible short downstreamof affected APCU

24


OFF (tb-bp)• Affected APCU OUTPUT

RLY − OP (tb-bp)25

•√MCC

4 12

24

13

Yes

No

18

Yes

No

122


23 JUN 006296.doc

Table 1. APCU TRIP STATUS

TRIP TRIP CAUSE(S)(STATUS VOLTAGE) OV OUV OC IUV

+4.88 X X X X+4.23 X X X+3.59 X X X+2.95 X X+2.27 X X X+1.62 X X+0.98 X X+0.34 X-0.30 X X X-0.95 X X-1.59 X X-2.23 X-2.91 X X-3.56 X-4.20 X

-4.84 (no trip)NOTE

OV: Output OvervoltageOUV: Output UndervoltageOC: Output OvercurrentIUV: Input UndervoltageTolerance for all reported voltages is ± 0.20 volts

123

20 SEP 00


124

APCU APCU VOLTS ↓↑(ASSY OPS/3A/FIN) Page 1 of 1 page

23 JUN 006295.doc

1

SPEC voltage forAPCU in the 120Volts mode is 122 to126.5 volts. InAPCU volts areoutside this rangebut stable andusuable for ISSloads, considerationwill be given tocontinuing APCUoperation.

2

APCU tripped butfailed to set tripindicator (possiblefor a short circuitdirectly at the APCUoutput).

3


4

There is a singlepoint failure whichwill cause both theHIGH and LOWRES VOLTS to readlow (broken wire).

4

2

APCU AMPS

APCU TRIP

SMALERT

S200 APCU 1(2)VOLT LMT






PL CAB − MNB(MNA)

PL AUX − ON

If APCU VOLTSRES HIGH ≥126.5 or ≤ 122

1 √APCU Status

SM 200 APCUSTATUS

APCU 1(2) TRIP > -4.40

Any APCU 1(2) CONV A(B)AMPS > 8.5

All APCU 1,2 OUT VOLTS(four) > 122 and < 126.5

None of the above

2 Transient voltage shift. 3


5 APCU voltageregulation problem.

8


1

1

APCU TEMP 1

4

•√Affected APCU VOLTS

APCU 1(2) OUT VOLTSRES HIGH = OUT VOLTSRES LOW = OSL

APCU 1(2) OUT VOLTSRES HIGH = OUT VOLTSRES LOW ± 2

Neither

(SODF: ASSY OPS)

(SODF: ASSY OPS)

(SODF: ASSY OPS)

11

6 Transducer failure. 7

APCU 1(2) OUT VOLTSRES HIGH between 115and 130.5?

9

MCC Available?

1

10

•√MCC

11

(L12/SSP1)•√Affected APCU 1(2)

OUTPUT RLY tb

Is tb gray?

4

12 Unannunciated APCUtrip.

13 Power down affectedAPCU



RLY − OPEN (tb-bp)

14 Both transducersfailed.

15


16

• Go to EPS SSR-3(4)POWER BUS LOSSN13B (N14B) (SODF:ISS MAL: EPS)

No

Yes

No

Yes

3

No

Yes

125

20 SEP 00


126

COMM OIU FAIL TO COMMAND(ASSY OPS/3A/FIN) Page 1 of 3 pages

23 JUN 006300.doc

1

Power cycle willplace OIU in Format255. OIU StationTLM will be lost untilOIU CMDrecovered. OIUH&S TLM will alsobe lost if PDI is notconfigured for OIUFMT 255.

1

No response toOIU Configurationor RoutedCommands

Nominal Config:(A1L)S-BD PLCNTL − CMDPWR SYS − 1PWR SEL − PSPPSP OUTPUT − PL UMB

(SSP1)OIU PWR – OIU 1(2)ON

OIU tb – UP(DN)

(R1)PLCAB –MNB(MNA)

PLAUX − ON

1 Request PSP DummyCMDs

• MCC will uplink PSPDummy CMDs and verifytelemetry.

• PSP Dummy CMD 2(then 1)

•√PSP CONFIG ID 2(1)•√UMB #4(1)•√No SM/PSP LOAD errors•√PSP I/F to OIU OFF(ON)

MCC CMD successful? 2 Power Cycle PSP 1(2)

(A1L)•√S-BD PL CNTL − CMD• S-BD PL PWR SYS − OFF• S-BD PL CNTL − PNL• S-BD PL PWR SYS − 1(2)• S-BD PL CNTL − CMD• S-BD PL PWR SYS − OFF

Expect ‘S62 BCE BYP PSP 1(2) ’

SM 62 PCMMU/PL COMM• I/O RESET PSP 1(2) − ITEM 6(7) EXEC

3 √OIU CMD

SM 212 OIU•√Bus 2 A − * (ITEM 8)• BUS 2 B − ITEM 9 EXEC

(*)

CMD successful? 4 Transient PSP 1(2)failure.

5 Determine CurrentOIU FMT

SM 212 OIU

•√FMT (ITEM 1), andlog____

6 Return BUS 2 toNominal Configuration

SM 212 OIU• BUS 2 A − ITEM 8 EXEC

(*)

7 Pwr Cycle OIU 1(2)

On MCC GO(SSP1)• OIU PWR− ctr, then• OIU PWR − OIU 1(2) −

ON•√OIU tb − UP(DN)• Expect ‘S62 PDI DECOM

FAIL ’

OIU FMT block 5 = 255? 9

10

8


No

Yes

Yes

No

No

Yes

127


23 JUN 006300.doc

9 Determine AffectedDECOM

SM 62 PCMMU/PLCOMM

•√DECOM indicating (↑),and log ____

7

10 √OIU CMD

SM 212 OIU• BUS 2 B − ITEM 9 EXEC

(*)

CMD successful?

7

17

11 Transient OIU 1(2)failure.

12 √OIU CMD byAttempting to LoadOriginal OIU FMT

SM 212 OIU• ITEM 1 + X X X EXEC,

where X X X is originalOIU FMT logged inblock 5.

•√PDI DCM SYNC foraffected Decom

All three ‘B’, ‘W’, ‘F’columns display an ‘*’?

17



(*)

14


15 Transient OIU 1(2)failure.

16


Yes

No

Yes

No

128


23 JUN 006300.doc

17 Switch to OIU 2(1)

On MCC GO(SSP1)• OIU PWR − OIU 2(1) ON•√OIU tb − DN(UP)

If OIU FMT in block 5 = 255, expect ‘S62 PDIDECOM FAIL ’

Switch to PSP 2(1)(A1L)•√S-BD PL CNTL − CMD•√S-BD PL PWR OUTPUT − PL UMB• S-BD PL PWR SYS − 2(1)•√S-BD PL SEL − PSP• S-BD PL CNTL − PNL,CMD

Expect ‘S62 BCE BYP PSP 1(2) ’.

SM 62 PCMMU/PL COMM• I/O RESET PSP 2(1) − ITEM 7(6) EXEC (*)

Config PDI for OIU 2• sel DECOM − ITEM 9 +X EXEC• sel INPUT − ITEM 12 +2(1) EXEC• LOAD − ITEM 13 EXEC

OIU FMT block 5 = 255?

18

SM 212 OIU• BUS 2 B − ITEM 9 EXEC

(*)

CMD successful?

10 12

23

19 PSP 1(2) to OIU 1(2)interface failure.

21

•√MCC

Yes

No

Yes

No



(*)

22


23 √OIU CMD byAttempting to LoadOriginal OIU FMT

SM 212 OIU• ITEM 1 + X X X EXEC,

where X X X is originalOIU FMT logged inblock 5.

•√PDI DCM SYNC foraffected Decom

All three ‘B’, ‘W’, ‘F’columns display an ‘*’?

24

•√MCC

25 PSP 1(2) to OIU 1(2)interface failure.

26


Yes

No

17

129

20 SEP 00


130

COMM OIU TEMP ↑(ASSY OPS/3A/FIN) Page 1 of 1 page

22 JUN 006298.doc

SM 212 OIUTEMP

Nominal Config:(R1)PLCAB −MNB(MNA)

PL AUX − ON

(SSP 1)OIU PWR − OIU 1(2)ON

OIU tb − UP(DN)

1

SM 212 OIU

OIU 1(2) TEMP?OIU message:OIU TEMP > 212

2

AOS or LOS?

3

•√MCC

4

• Select OIU 2(1)

SSP1• OIU PWR − OIU 2(1) ON• √OIU tb – DN(UP)

5 Switch to PSP 2(1)

(A1L)•√S-BD PL CNTL − CMD•√S-BD PSP CMD OUTPUT − PL UMB• S-BD PWR SYS − 2(1)•√S-BD PWR SEL − PSP• S-BD PL CNTL − PNL,CMD

• Expect ‘S62 BCE BYP PSP 1(2) ’

S62 PCMMU/PL COMM• I/O RESET PSP 2(1) − ITEM 7(6) EXEC

6 Configure PDI for OIU2(1)

• sel DECOM − ITEM 9 +XEXEC

• sel INPUT − ITEM 12+2(1) EXEC

• LOAD − ITEM 13 EXEC

7 Load OIU FMT andConfig if Required

•√MCC for correct OIUFMT/CONFIG

• Perform LOAD OIUFMT/CONF (FDF, ORBOPS FS, COMM/INST),then:

8


No

Yes

AOS

LOS

131

20 SEP 00


132

COMM S212 OIU AD 1,2,3,4 NOLK/LOSS OF NODE MDM TELEMETRY(ASSY OPS/3A/FIN) Page 1 of 2 pages

23 JUN 006299.doc

LOSS OF PCS TELEMETRY,all (SODF: ISS MAL: C&DH)

S62 PDI DECOM FAIL, all(SODF: ASSY OPS: MALFUNCTION)

S212 OIU AD1,2,3,4 NOLK

Nominal Config:(R1)PLCAB −MNB(MNA)

PLAUX – ON

(SSP 1)OIU PWR − OIU1(2) ON

OIU tb − UP(DN)One PCS connectedto N1-2 MDM

Loss of NodeTelemetry onMCDS Displays,Static FrameCounter

1

SM 62 PCMMU/PLCOMM

•√PDI DECOM for OIU islocked

OIU DECOM locked?No

Yes

2

SM 212 OIU

•√OIU SYNC

AD 1 LOCK = YES? 3 Momentary loss ofnode telemetry.

4


5

•√MDM status using PCS

PCS CDS Main ControlPanel Window• sel Connect To MDM

icon

Is MDM connected statusbox green?

6

•√Node MDM status

7 Resync OIU to NodeMDM; Reload OIUFMT 002

• Item 1 + 0 0 2 EXEC

Active Device Lock − YES?

No

Yes

8 Momentary loss ofnode telemetry.

Yes

No

9 Cycle OIU Power

(SSP1)• OIU PWR − ctr (tb-bp)• OIU PWR − OIU 1(2) ON•√OIU tb – UP(DN)

• For NODE MDM, performLOAD OIUFMT/CONFIG, all (FDF,ORB OPS FS,COMM/INST), then:

Active Device Lock − YES? 10 Internal OIU logic lockup.

11


12 OIU 1(2) BIA failure.

Yes

No

Yes

No

13

S62 PDI DECOM FAIL, block 5(SODF: ASSY OPS: MALFUNCTION)

133

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23 JUN 006299.doc

13 Swap to OIU 2(1)

(SSP1)• OIU PWR − OIU 2(1) ON• √OIU tb – DN(UP)

12

14 Switch to PSP2(1)

(A1L)•√S-BD PL CNTL − CMD•√S-BD PL PSP OUTPUT − PL UMB• S-BD PL PWR SYS − 2(1)•√S-BD PL PWR SEL − PSP• S-BD PL CNTL − PNL,CMD


S62 PCMMU/PL COMM• I/O RESET PSP 2(1) − ITEM 7(6) EXEC

15 Configure PDI for OIU2(1)


• sel INPUT − ITEM 12+2(1) EXEC

• LOAD − ITEM 13 EXEC

16 Load OIU Fmt

• For Node MDM, performLOAD OIU FMT/CONF(FDF, ORB OPS FS,COMM/INST) , then:

17

SM 212 OIU•√OIU SYNC

Active Device Lock = YES?

19


18

•√MCC

No

Yes

134

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23 JUN 006297.doc

1

'S212 OIU AD1,2,3,4 NOLK’indicates OIU activedevice lock = NO.

2.4e ‘S62 BCE BYP PDI’(FDF, MAL, COMM)

1

S212 OIU AD 1,2,3,4 NOLK/LOSS OF NODE MDM TELEMETRY,all (SODF: ASSY OPS: MALFUNCTION)

SMALERT

S62 PDIDECOM FAIL

Nominal Config:(A1L)PL DATA INTLVRPWR − ON

DECOM FDAENA – ITEM 14(15,16,17) = ENA(*)

(A1L)S-BD PLPWR SYS – 1PWR SEL – PSPPSP CMD OUTPUT − UMB

(R1)PL PRI MNC − ON(tb-bp)

OIU(R1)PLCAB −MNB(MNA)

PLAUX − ON

(SSP1)OIU PWR – OIU 1(2)ON

OIU tb – UP(DN)

1

Message accompanied by‘S62 BCE BYP PDI’?

2

SM 62 PCMMU/PLCOMM

Any DECOM indicating fail?No

Yes

3

SM 212 OIU•√OIU SYNC

AD 1 LOCK = YES? 4 Transient PDI Decomfailure.

5

• Go to S212 OIU AD1,2,3,4 NOLK/LOSS OFNODE MDMTELEMETRY, block 5(SODF: ASSY OPS)

6


7 Reload DECOM Indicating Fail

SM 62 PCMMU/PL COMM• sel DECOM − ITEM 9 + X EXEC• sel FMT − ITEM 10 + X X X EXEC• Load − ITEM 11 EXEC

Load − CPLT? 8 PDI Decom failure.No

Yes

Yes

No

9

DECOM still indicating fail(↑)?

10 Transient PDI Decommemory failure.

No

Yes

11 Select B/U DECOMConfig if Required

• For alt PDI config,perform LOAD PDIDECOM FORMAT, all(FDF, ORB OPS FS,COMM/INST), then:


12 Select B/U DECOMConfig if Required

• For alt PDI config,perform LOAD PDIDECOM FORMAT, all(FDF, ORB OPS FS,COMM/INST), then:

B/U DECOM indicating fail(↑)?

13


14 PDI Decom failure. 15 Load ALT PDI andPCMMU Config

• For alt PDI config,complete LOAD PDIDECOM FORMAT(FDF, ORB OPS FS,COMM/INST), then

• For alt TFL, performLOAD PCMMUFORMAT, all (FDF ORBOPS FS, COMM/INST)

18

16 PL TLM system toPDI I/F failure or PL TLMsystem failure.

17

No

Yes

Yes

No

SM 62PCMMU/PLCOMM

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23 JUN 006297.doc

2

TCS not addressedin malfunction; it isnot enabled.

3

MCC may directcrew to confirm PLPRI receivingpower.

4

Alternate (OIU 2)requires PSP 2.

3

4

3

2

17 If Required Config toNominal PDI DECOMFORMATS

• Perform LOAD PDIDECOM FORMAT (FDF,ORB OPS FS,COMM/INST), then:

16

18 Zero Out OriginalDECOM Source

SM 62 PCMMU/PLCOMM


• sel INPUT − ITEM 12 +0EXEC

• LOAD − ITEMN 13 EXEC

• Notify MCC.• Continue nominal

operations.

15

19

• Determine affected PL.

OIU (INPUT 1,2)

20 Cycle OIU 1(2) Power

SSPI)• OIU PWR − ctr (tb-pb)• OIU PWR − OIU 1(2) ON

(tb-UP(DN))

• Perform LOAD OIUFMT/CONFIG, all (FDF,ORB OPS FS,COMM/INST), then:

PDI DECOM lock? 21 OIU power transient. 22


23 Switch to OIU 2(1)

(SSP1)• OIU PWR − OIU 2(1) ON (tb-DN(UP))

Switch to PSP 2(1)(A1L)•√S-BD PL CNTL − CMD•√S-BD PL PSP OUTPUT − PL UMB• S-BD PL PWR SYS − 2(1)•√S-BD PL SEL − PSP• S-BD PL CNTL − PNL,CMD


S62 PCMMU/PL COMM• I/O RESET PSP 2(1) − ITEM 7(6) EXEC (*)

Config PDI for OIU 2(1)• sel DECOM − ITEM 9 +X EXEC• sel INPUT − ITEM 12 +2(1) EXEC• LOAD − ITEM 13 EXEC

• Perform LOAD OIU FMT/CONFIG, all (FDF,ORB OPS FS, COMM/INST), then:

PDI DECOM lock? 24 PDI failure.

Yes

No

27

•√MCC

No

Yes

25 OIU 1(2) to PDIinterface failed.

26


136

21 SEP 00

REFERENCE PROCEDURE

REFERENCE

137

21 SEP 00


REFERENCE

138

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RESISTIVE THERMAL DEVICE (RTD)The RTDs are the temperature sensors for the Shuttle-based WirelessInstrumentation System (SWIS). Each RTD is a 1 inch square piece ofresistive thermal material with a resistance related to temperature. EachRTU has a cable attached that is routed to a Remote Sensing Unit (RSU).The RTD designations and locations shown below.

RTDDesignation

Location

Z1-1A Inner PMA bulkhead inside accumulator housing (lower side)Z1-1B CMG bulkhead, mounting post for CMG 3Z1-1C Ku Boom SGTRC (under coldplate)Z1-1D CBM pressure domeZ1-1E Zenith bulkhead near P6 interface, PMA sideZ1-1F Port trunion bulkhead, front side of RPCM coldplateZ1-1G Zenith bulkhead, attached to SGANT RIRS plateZ1-1H Cable tray, attached to NH3 line bracketZ1-1I* Starboard trunion bulkhead, front side of BSP coldplateZ1-1J* Starboard bulkhead, on SASA mounting bracketZ1-2A Inner PMA bulkhead inside accumulator housing (upper side)Z1-2B CMG bulkhead, mounting post for CMG 1Z1-2C Ku Boom SGTRC (under coldplate)Z1-2D Cable tray, attached to NH3 line bracketZ1-2E Zenith bulkhead near P6 interface, CMG sideZ1-2F Starboard bulkhead, near SASA mounting bracketZ1-2G Zenith bulkhead, attached to SGANT RIRS plateZ1-2H Port bulkhead near Plasma Contactor mountingZ1-2I* Starboard trunion bulkhead, front side of BSP coldplateZ1-2J* Ku Boom, mounting flange for Ku antenna

*RTD attached to structure and cable routed, but not connected to RSU

REMOTE SENSING UNITS (RSU)The RSUs collect temperature data from the RTDs connected to it and storeit until the Network Control Unit (NCU) sends a request for the data. Thereare two RSUs, RSU 1 and RSU 2 integrated on Z1. They are located onthe CMG bulkhead along the zenith edge. The RSU 1 antenna is locatedon the nadir bulkhead, the starboard CMG side, at the tip of the poolhandle. The RSU 2 antenna is located on the nadir bulkhead, starboardPMA side. RTDs Z1-1A through Z1-1H are connected to RSU 1, andsimilarly, TRDs Z1-2A through Z1-2H are connected to RSU 2.

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There are two other RSUs, one on the orbiter port sill and one on thestarboard sill, that are used to relay radio signals between the RSUs on Z1and the NCU. Each one is also connected to an RTD on each DDCUsidewall carrier so that each sill RSU has a temperature sensor on eachsidewall carrier.

NETWORK CONTROL UNIT (NCU)The NCU is the only component of SWIS located within the orbiter.Two NCUs are flown, with one being used and the other as a backup.The NCU is attached near the aft windows, behind the CRTs, so that theantenna is in the window. It is connected to a PGSC and communicates viaradio frequency to the RSUs. The data it receives from the RSUs is storedon the PGSC for eventual downlink via OCA.

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23 JUN 006304.doc

S16

SSP-1

STANDARD SWITCH PANEL

UP

5 5

5

DS4 DS6 DS13

CB3

CB4

S5 S7S3 S15 S17 S18 S19

S11 S12

S6S4

5

CB2

CB1

S1 S2 S13 S14

S20 S21 S24S22 S23S8 S9 S10

UP - OIU1 ON

S17S5

PDIP

PDIPPWR 1

PWR 2 /KuBAND RLY

S13 S14

ON

OFF

SECC/L CAM

PWR

ON

OFF

OIU PWR

OIU 1 ON

OIU 2 ONS21

S2S1

OUTPUTRLY

CLOSE

OPEN

ODS CONNMATE X1TLM PWR

OFF

ON

SW PWR 2SW PWR 1

CB2

CB1

CB4

CB3

SSP-1

ON

OFF

TCSPWR

DS15DS3 DS7

APCU 1

CONV

ON

OFF

PRIC/L CAM

PWR

ODS CONNMATE X2TLM PWR

OFF

ON

DN - OIU2 ON

OUTPUTRLY

CLOSE

OPEN

APCU 2

CONV

ON

OFF

S23

CLOSECLOSE

S16

OFF

S8 S9 S11S10 S12

141

20 SEP 00


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12 SEP 006305.doc

143

20 SEP 00


144

MULTIFUNCTION CRT DISPLAY SYSTEM(ASSY OPS/3A/FIN A) Page 1 of 69 pages

20 SEP 006306.doc

The MCDS provides another crew interface to the ISS in addition to the EPCS. The OIUconverts ISS telemetry into a format that can be processed by the orbiter. It is displayedto the crew onboard and sent to the MCC. Likewise, the OIU converts the MCDScommands into a format that the ISS can understand. The assembly related crewdisplays and their descriptions for Mission 3A are provided in this section for reference.For more detailed information on crew displays, refer to the 3A Annex 4.

1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/204/XXX FGB XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 4 VOLTS AMPS 5 MAIN BUS XXXX.X 6 V1 XXX.X 7 V2 XXX.X BC SYNC XXXS 8 SOLAR ARRAY XXX.X FRM CTR XXX 910 RACU 5 INP XXX.X COMMANDING XXX11 OUT XXX.XS XX.XS CMD DIR XXX12 MU RDY CH 1 XXX13 RACU 6 INP XXX.X 2 XXX14 OUT XXX.XS XX.XS 3 XXX15 OCS RDY 1 XXX16 ON OFF 2 XXX17 RACU 5 PWR X X AMP - HRS18 VIA FGB 1 5 BATT VOLTS CHG 1 CHG 219 NCS 2 6 1 XX.X XX.X XX.X20 2 XX.X XX.X XX.X21 RACU 6 PWR X X 3 XX.X XX.X XX.X22 VIA FGB 3 7 4 XX.X XX.X XX.X23 NCS 4 8 5 XX.X XX.X XX.X24 6 XX.X XX.X XX.X2526

Figure 1.- 204 FGB Display.

TITLE: FGBTYPE: SPEC 204AVAILABILITY: SM OPS 2

NOTEThis display is to be used with NCS Release 1.1. For NCS R2,the equivalent display is SPEC 224. The displays are identical;however, the PUIs and MSIDs are different.

PURPOSE, OPERATION, AND ORGANIZATIONThis display is used for monitoring pertinent FGB telemetry and controls power toRACUs. Refer to Figure 1.

The parameter status field for all parameters either displays a blank for normal operationor it displays an “M” for missing data. For analog parameters, this field also displays an“H” or “L” for off-scale data. Some parameters displayed are limit-sensed for SM alerts

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20 SEP 006306.doc

or C&W alarms. For discretes that are limit-sensed, a “↓” is displayed in this field whenthe parameter is out of limits. For analogs that are limit-sensed, an “↑” or a “↓” isdisplayed when the parameter exceeds either an upper or lower limit. The symbolsdriven in the parameter status field have the following display priority from highest tolowest: M, H, L, “↑”, “↓”. All symbols driven in the parameter status column aredisplayed four times normal intensity.

The following paragraphs describe the function of each section of the display.

TOP LEFTThe main bus current (amps), two voltage (volts) values (V1 and V2), and the solararray current are displayed. The input (INP) current for the two RACUs is alsodisplayed. The RACU 5 and RACU 6 output (OUT) voltage and current are limit-sensed. When the voltage reaches its high or low limit and the current reaches it highlimit, the crew receives an alert tone, light, and fault message.

BOTTOM LEFT SECTIONRACU 5 and RACU 6 can be powered two ways via this display. If the OIU is the buscontroller to the FGB MDM, the crew uses the PWR VIA FGB commands. If the NodeMDM is the bus controller to the FGB MDM, the crew uses the PWR VIA NCScommands. When RACUs are powered ON using either method (items 1 - 4), anasterisk is displayed under the ON column. When the RACUs are powered OFF (items5 --- 8), an asterisk is displayed under the OFF column.

RIGHT TOP SECTIONIn the BC SYNC field, either “YES” or “NO” is displayed to indicate whether the FGBMDM is communicating with the bus controller (either the OIU or Node MDM). Whenthe FGB MDM loses sync with the BC, this field reads “NO” and the crew receives analert light, tone, and fault message.

By checking to see if the frame counter (FRM CTR) is incrementing, the crew candetermine whether data is being received from the FGB MDM.

MIDDLE RIGHT SECTIONThe COMMANDING field indicates whether or not the relay command matrix has beenEnabled (ENA) or Inhibited (INH). The relay command matrix is controlled by theMCC-M. When this command matrix is enabled, the MCC-H or the crew can commandthe FGB. This field must read “ENA” before either MCC-H or the crew has the capability toissue the RACU power ON and OFF commands.

The CMD DIR field indicates the direction of a command sent to a FGB element. Thisfield reads either “MU” (to indicate that the command was originated from the matchingunit) or “DIO” (to indicate that the command was originated from the FGB MDM).

The MU RDY CH 1, 2, 3 fields display either “YES” or “NO” to indicate the readiness ofthe matching unit.

The OCS RDY 1, 2 fields display either “YES” or “NO” to indicate the readiness of theonboard computer system, which consists of the matching unit and the FGB MDM.

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BOTTOM RIGHT SECTIONThe BATT section displays the voltage and two charge readings for the six FBGbatteries. The BATT CHG parameters measure the state of charge in A-hr of thebatteries. The range is 0 to 60 A-hr, 0 being a completely drained battery and 60 beinga fully charged battery. There are two sensors that measure the charge. The Russiansare able to select and deselect the sensors depending on their telemetry needs.Therefore, both sets of battery charge data may not be available.

1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/210/XXX NODE 1 XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 PRI MDM SEC MDM 4 PHY ID XXXX XXXX CABIN PRESS XX.XXS 5 STATE XXXX XXXX 6 STBY 1 2 BUS CONFIG 7 N1-1 TO SEC 3 CH A CH B 8 CONFIG XXX XXX N1-1 MDM 9 UB ORB N1-1 XX 19X 20X10 FRM CTR XX XX CB GNC-1 XX 21X 22X11 SYNC XXXS LB LAB SYS-1 XX 23X 24X1213 TEMP N1-1 XXXX N1-2 MDM14 N1-2 XXXX UB ORB N1-2 XX 25X 26X15 LOAD SHED CB GNC-2 XX 27X 28X16 VIA NCS 4+ LB LAB SYS-2 XX 29X 30X17 FGB XXXS18 POWER ON OFF TRIP PRI MDM19 N1-1 MDM 7X 8X S UB EPS N1-14 XX 31X 32X20 SDO A 9X 10X S N1-23 XX 33X 34X21 B 11X 12X S22 N1-2 MDM 13X 14X S ISS C&W TONE STATUS23 SDO A 15X 16X S FIRE S24 B 17X 18X S WARN S CAUT S2526

Figure 2.- 210 NODE 1 Display.

TITLE: NODE 1TYPE: SPEC 210AVAILABILITY: SM OPS 2

NOTEThis display is to be used with NCS Release 1.1. For NCS R2,the equivalent display would be SPEC 220. The displays areidentical; however, the PUIs and MSIDs are different.

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20 SEP 006306.doc

PURPOSE, OPERATION, AND ORGANIZATIONThis display is used to control and monitor Node 1 MDMs and monitor pertinent nodetelemetry. Refer to Figure 2.

The parameter status field for all parameters either displays a blank for normaloperation or displays an “M” for missing data. For analog parameters, this field alsodisplays an “H” or “L” for off-scale data. Some parameters displayed are limit-sensedfor SM alerts or C&W alarms. For discretes that are limit-sensed, a “↓” is displayed inthis field when the parameter is out of limits. For analogs that are limit-sensed, and an“↑” or a “↓” is displayed when the parameter exceeds either an upper or lower limit. Thesymbols driven in the parameter status field have the following display priority fromhighest to lowest: M, H, L, “↑”, “↓”. All symbols driven in the parameter status columnare displayed four times normal intensity.


TOP LEFT SECTIONThe PHY ID field displays “N1-1” or “N1-2” to indicate which ISS Node 1 MDM is thePrimary (PRI) and Secondary (SEC) NCS MDM. For nominal operations, N1-2 is thePRI MDM and N1-1 is the SEC MDM.

The STATE field indicates the operational state of the primary and secondary MDMs.This field reads “PRI” for primary, “SEC” for secondary, and “STBY” for standby. Thediagnostic “DIA” state is not displayed because of the way the Node MDMs function.Items 1 and 2 allow the crew to command either the primary or secondary MDM to thestandby state. Item 3 commands N1-1 to the secondary state.

The CONFIG field indicates the configuration number (C01-16) of the NCS running inthe primary and secondary MDMs.

By checking to see if the FRM CTRs for the PRI and SEC MDMs are incrementing, thecrew can determine whether data are being received from the MDMs.

The SYNC field displays either “YES” or “NO” to indicate whether or not the SEC MDMis communicating with the PRI MDM. This field only applies to the secondary MDM.When the SEC MDM has lost sync with the PRI MDM, “NO” is displayed in the SYNCfield and the crew receives an alert light, tone, and fault message.

The TEMP fields display the internal temperature of the N1-1 and N1-2 MDMs in °F.

LEFT MIDDLE SECTIONItem 4 (LOAD SHED VIA NCS) activates the Node 1 load shed table, which powers offeverything in the Node 1 except the MDMs. This command is used by the crew inresponse to a fire in the Node. This command is protected to prevent inadvertentexecution; therefore, an ITEM 4 + 99 entry is required. Currently, there is no telemetryfrom the NCS to indicate the status of the load shed. The load shed table can also beactivated without crew or ground intervention. If any three or more FGB batteries read25 volts or less, the FGB sends a C&W to the Node 1 MDMs, which activates the loadshed table. If this occurs, the LOAD SHED VIA FGB field displays “YES” and a downarrow is displayed in the status field. The crew also receives an alert light, tone, andfault message. Otherwise the field displays “NO.”

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20 SEP 006306.doc

BOTTOM LEFT SECTIONThe POWER section allows the crew to close (power on) and open (power off) theRemote Power Controllers (RPCs) associated with the MDM power supplies andSolenoid Driver Output (SDO) cards (items 7 - 18). An asterisk is displayed next to theappropriate item number to indicate the power status. A down arrow is displayed in theTrip Status field when an RPC has tripped. The crew also receives an alert light, tone,and fault message.

TOP RIGHT SECTIONThe CABIN PRESS field displays the Node 1 cabin pressure. When this parameterexceeds its lower/upper FDA limits, a down or an up arrow is displayed in the statusfield. The crew also receives a master alarm light and tone, B/U C/W light on panel F7,and a fault message.

MIDDLE RIGHT SECTIONThe BUS CONFIG section displays information on the space station 1553B buses. Thefield to the right of the bus name displays the configuration of the buses connected tothe specified MDM. This field reads either “BC” for bus controller, “RT” for remoteterminals or “NA” for not available. Items 19 - 34 allow the crew to select either Channel Aor B on each of the buses. An asterisk is displayed next to the appropriate item numberto indicate the selected channel.

BOTTOM RIGHT SECTIONISS C&W TONE STATUS: Because the EPCS does not have the capability toannunciate alarm tones, the tone status flag from the NCS is used to trigger the orbiterC&W system. When the tone status flag is set for any fire (FIRE), warning (WARN) orcaution (CAUT) event, a down arrow is displayed in the appropriate status field. For aFIRE event the crew receives a master alarm light and tone, B/U C/W light on panel F7,and a fault message. For WARN and CAUT events the crew receives an alert light, atone, and a fault message. The crew then has to refer to the PCS for details on the faultcondition.

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20 SEP 006306.doc

1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/203/XXX EARLY COMM XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 CL OP 4 N1RS1C RPC 5 1X 2X PTG MODE 5 6 3X 4X MANUAL 22X 6 12 5X 6X AUTO 23X 7 13 7X 8X 8 N1RS2A RPC 5 9X 10X ANT SEL 9 6 11X 12X PORT OMNI 24X10 10 13X 14X STBD OMNI 25X11 11 15X 16X12 PORT ARRAY BEAM X13 ON OFF STBD ARRAY BEAM X14 XMIT 17X 18X15 DECRYPT X 19X BEAM SEL XX16 KEY XXX17 POST XXXX SIG STR XXX18 CPT POST XXXX19 HI LO20 SYS MODE 20X 21X TEMP I/F21 LOCK PORT ANT XXX XXX22 PORTCOM XXX STBD ANT XXX XXX23 CTP FRM XXX PORTCOM XXX XXX24 R-S RJCT XXX CTP XXX2526

Figure 3.- 203 EARLY COMM Display.

TITLE: EARLY COMMTYPE: SPEC 203AVAILABILITY: SM OPS 2

NOTEThis display is to be used with NCS Release 1.1. For NCS R2,the equivalent display is SPEC 223. The displays are identical;however, the PUIs and MSIDs are different.

PURPOSE, OPERATION, AND ORGANIZATIONThis display is used to provide the JSC Mission Control Center (MCC) with the capabilityto uplink commands to and receive telemetry from the Node 1 MDM via the TDRSS.Refer to Figure 3.

The parameter status field for all parameters is blank for normal operation or displays an“M” for missing data. For analog parameters, this field also displays an “H” or “L” for off-scale data. Some parameters displayed are limit-sensed for SM alerts or C&W alarms.For discretes that are limit-sensed, a “↓” are displayed in this field when the parameteris out of limits. For analogs that are limit-sensed, an “↑” or a “↓” is displayed when theparameter exceeds either an upper or lower limit. The symbols driven in the parameterstatus field have the following display priority from highest to lowest: M, H, L, “↑”, “↓”.

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20 SEP 006306.doc

All symbols driven in the parameter status column are displayed four times normalintensity.


TOP LEFT SECTIONItems 1 through 16 allow the crew to power on (close (CL)) and power off (open (OP))the RPCs associated with the early communication system. An asterisk is displayednext to the appropriate item number to indicate the open/closed status of each RPC.

BOTTOM LEFT SECTIONItems 17 and 18 power ON and OFF the early communication system transmitter,respectively. An asterisk is displayed next to the appropriate item number to indicatetransmitter status.

Item 19 turns OFF the decryption function. An asterisk is displayed next to item 19 toindicate that the decryption function is OFF; otherwise, an asterisk is displayed underthe ON column. The KEY field displays the index number of the decryption keycurrently in use. This value is displayed in hex. The POST field displays either “PASS”or “FAIL” to indicate whether the decryption POST was successful.

The CTP POST field displays either “PASS” or FAIL” to indicate whether the CTP POSTwas successful.

Items 20 and 21 allow the crew to select either the HI or LO system mode, respectively.An asterisk is displayed next to the appropriate item entry to indicate the current systemmode. HI mode is used for video teleconferencing and LO mode is used forcommand/telemetry transmission.

The LOCK section indicates whether or not the PORTCOM transceiver has forwarderror correction code lock and whether the CTP has frame lock. Either “ERR” or“NORM” is displayed.

The R-S RJCT field displays either “YES” or “NO” to indicate if forward link packets arebeing discarded because of Reed-Solomon rejects.

TOP RIGHT SECTIONItems 22 and 23 allow the crew to select either manual or automatic pointing modes,respectively. An asterisk is displayed next to the appropriate item entry to indicate thecurrent mode. Normal operation of the system is in automatic pointing mode.

Items 24 and 25 allow the crew to select either the PORT or Starboard (STBD) OMNIantenna, respectively. These commands are used only when in low data rate andmanual pointing mode. An asterisk is displayed next to the appropriate item entry toindicate the antenna selected regardless of pointing mode.

Items 26 and 27 allow the crew to select either the PORT or STBD ARRAY BEAM.These commands are used in conjunction with automatic pointing mode to give theantenna pointing algorithm an initial beam reference for signal acquisition. Thesecommands are also used for full manual control of the arrays when in manual pointing

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20 SEP 006306.doc

mode. These are indexed commands with 64 beam selection. An asterisk is displayedto the right of the command feedback field to indicate PORT or STBD in use.

The BEAM SEL field displays the last ground commanded beam selection or the currentantenna beam used during the search mode for the acquisition phase. Once the systemacquires and begins tracking the satellite in the dither mode, this beam number is nolonger valid.

The SIG STR field displays the strength of the forward link signal.

BOTTOM RIGHT SECTIONThe temperatures for the PORT ANT, STBD ANT, PORTCOM and CTP are displayed incounts.

The I/F section indicates whether or not the control/status data interfaces between thePORT ANT, STBD ANT, PORTCOM and the CTP are good. The field reads either“ERR” or “OK.”

Nonstandard display implementation.

Two sign columns for the hex data are overlaid by two background characters. The twosigns can never be negative and the plus signs are never driven.

1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/212/XXX OIU XX X DDD/HH:MM:SS 2 DDD/HH:MM:SS 3 OIU 1 TEMP ±XXXXS OIU STATUS CTR XX 4 OIU 2 TEMP ±XXXXS ISS BC TIME XX-XX-XX/XX:XX:XX 5 6 STATUS 1 FORMAT XXX 7 ACTIVE DEVICES PDI 8 DCM SYNC BUS 1 RT 2X 9 AD PD BUS LOCK B W F BC 3X10 1 XXXX X XXXXS 1 XSXSXS A 4X11 2 XXXX X XXXXS 2 XSXSXS B 5X12 3 XXXX X XXXXS 3 XSXSXS BUS 2 RT 6X13 4 XXXX X XXXXS 4 XSXSXS BC 7X14 A 8X15 OIU CMD CTR XXX B 9X16 PSP I/F XXX BUS 3 RT 10X17 FLOAT POINT XXXS LAST CMD BC 11X18 PSP XXX A 12X19 OIU XXX B 13X20 SSOR BUS 4 RT 14X21 PRI FRM SYNC XXXS BC 15X22 PRI STATUS XXXS 18 SPARE CMD A 16X23 B/U FRM SYNC XXXS XXX B 17X24 B/U STATUS XXXS2526

Figure 4.- 212 OIU Display.

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TITLE: OIUTYPE: SPEC 212AVAILABILITY: SM OPS 2

PURPOSE, OPERATION, AND ORGANIZATIONThis display is used to configure the OIU for cargo element operations through the OIUsMS 1553 B data buses (ISS MDMs, SSOR, MPLM MDM, etc.), monitor OIU status, andmonitor relevant PDI, PSP, and SSOR statuses. The OIU display is divided into threeareas: upper, lower left, and lower right. The upper area contains the shuttle standarddisplay header information, the OIU 1 and 2 temperatures, and the OIU and ISS BCtime. The lower left section has status information from the OIU, the PDI, the PSP, andthe SSOR. The lower right section contains the OIU command items and OIU busstatus information (BC/RT, side A/B). Refer to Figure 4.

The parameter status field for all parameters is blank for normal operation. For thoseparameters acquired by the SM GPC through the Pulse Code Modulation Master Unit(PCMMU) (OIU temperatures, PDI status, SSOR status), an “M” is displayed for missingdata. For the rest of the parameters displayed on this SPEC, there is no status availablefor missing data. Some of the statused data on this display (OIU temperatures, physicaldevice lock status, floating point error) are also limit-sensed for SM alerts. An “↑” isdisplayed when either OIU temperature exceeds the upper FDA limit. A discreteparameter shows a “↓” if its FDA limit is reached, whether that limit is high or low. Thesymbols driven in the parameter status field have the following display priority fromhighest to lowest: M, H, L, “↑”, “↓”. All symbols driven in the parameter status columnare displayed four times normal intensity.

There are no “index +99” commands on this display.

Each major functional area of the display is described below.

UPPER SECTIONOIU 1(2) Temp. On the left side of the upper section are temperatures for both OIUs.These parameters read 140° F when the OIU associated with that measurement is OFF.Note that the only sure method to determine which OIU is powered up from this displayalone (without referring to the OIU SSP power talkback) is to look for the “OFF”temperature noted above. An “↑” is displayed when the temperature FDA limit isreached, and an “M” is displayed when the associated data are missing.

All of the following OIU measurements are not specific to an OIU (OIU 1 or 2), but aredisplayed from whichever OIU is powered.

OIU Status Counter and ISS BC Times. On the right side of the upper section, the OIUStatus Counter and ISS BC times are displayed. The ISS BC time follows the formatMM-DD-YY/HH:MM:SS. The OIU Status Counter displays the OIU time parameter forseconds, reading from 00 to 59 and resetting to 00 again. This display item is intendedto indicate OIU health by constantly counting from 00 to 59 and recycling when OIUtelemetry is being processed by the PDI. The ISS BC time comes from whicheverdevice is BC to the OIU on one of its MS 1553B buses. This parameter reads all zerosat powerup, shows the correct BC time when the BC comes up and starts sending

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telemetry to the OIU, and remains static at the last good sample when the incoming MS1553B telemetry from that BC goes away.

LOWER LEFT SECTIONActive Devices. The Active Devices Status section provides current OIU processingstatus on the external telemetry sources with which the OIU can interface. Each activedevice is numbered 1 to 4, in the leftmost column. Each row has three columnsdisplaying the Physical Device (PD) currently assigned to that Active Device (AD), theMS 1553B bus being used to acquire that active device’s telemetry, and a lock statusindication for that AD. The PD and bus information is changed by the OIU Formatcommand and the LOCK information is actual status. Following are the allowed statesof the PD, BUS, and LOCK columns.

PD: OIU (default when no active device assigned, also displayed when in a format that supports an OIU error log dump)CC1 (CC2) ISS Command and Control MDM 1 or 2SR1 (SR2) Space to Space Orbiter Radio (SSOR) 1 or 2MP1 (MP2) ISS Mini Pressurized Logistics Module (MPLM) MDM 1 or 2N1-1 (N1-2) ISS Node 1 MDM 1 or 2FG1 (FG2) ISS FGB MDM 1 or 2

BUS: OIU MS 1553B bus 1 to 7, with 8 reading “0”(Note - Current OIU hardware supports only buses 1 to 4)

LOCK: NONE if the current OIU format does not have an AD for this display locationYES if the OIU is RT and in sync with the AD (AD is an ISS BC or SSOR)YES if the AD is OIU in error log dump format (OIU must be in sync with itself)NO if the OIU is RT and was in sync with the AD but has lost lock on the AD(ISS BC or SSOR)N/A if the OIU is BC to the AD, except if the AD is SSOR

Note that if LOCK goes from YES to NO, the OIU stops attempting to acquire sync withthat AD. To force the OIU to attempt to resync with an AD (ISS bc THROUGH MS 1553bus direct or through the SSOR), the appropriate OIU format must be reloaded, thusforcing a resync attempt.

OIU Command Counter. The OIU Command Counter starts at “000” at powerup andincrements by one whenever the OIU receives a valid command from the PSP. Thecounter reads in decimal, counts from “000” to “255,” and rolls over to “000”. Allcommands, whether from the MCC or the MCDS, cause the counter to increment ifreceived and processed by the OIU.

PSP I/F. The PSP I/F parameter indicates whether the OIU is receiving the 16-kHzcommand carrier from either PSP 1 or 2. This parameter reads as follows:

“OK” if the OIU is receiving the PSP command carrier“ERR” if the OIU is not receiving the PSP command carrier

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Float Point. The OIU can convert one ISS floating point parameter value per PDI minorframe (maximum of 100 per major frame) into a shuttle PDI-compatible parametervalue. If an ISS floating point value is invalid or results in an invalid floating pointvalue/operation during the conversion process, the OIU annunicates an error. Theassociated display parameter reads as follows:

“OK” if no floating point error“ERR” if an invalid floating point value/operation is detected

SSORPRI (Backup (B/U)) FRM SYNC. These parameters give the status of the ISS commlink frame synchronizer in the prime (B/U) SSOR, as follows:

YES if the SSOR is in frame sync with the SSSR on the ISSNO if no frame sync, or the SSOR is off or not manifested

PRI (B/U) Status. These parameters give the overall SSOR status for the prime(backup) SSOR as follows:

OK if the SSOR is operating normallyBAD if the SSOR BITE has sensed a failure in the SSOR

PDIDCM and SYNC section. This section is a matrix giving the PDI decommutator bit,word, and frame synchronizer statuses for all four decoms, as follows:

For each decom row (1-4): The “B”, “W”, and “F” columns are blank if the decom isnot in bit, word, or frame sync (respectively). If the decom is in bit sync, the “B”column displays an “∗”, if in word sync the “W” column displays an “∗”, and if inmaster frame sync, the “F” column displays an “∗”. Note that the decom actuallyprocessing the OIU PDI stream is dependent on shuttle recon and may change frommission to mission and with different PDI/PCMMU configs.

PSP Last Command. This status point indicates the PSP command acceptance state,as follows:

“OK” if the PSP has not rejected a PSP-destined crew spec command

“REJ” if the PSP has rejected the last PSP-destined crew spec command, or

“INC” if the PSP was not able to complete transfer of the last PSP-destined crewspec command

The REJ and INC indications are cleared by the next successfully processed PSP-destined command by either the crew or the MCC.

OIU Last Command. This status point indicates the OIU command acceptance state, asfollows:

“OK” if the OIU has not received a command from the PSP that had parity errors orincorrect byte count

“REJ” if the OIU has received a command from the PSP which had either a parityerror, or had an incorrect byte count

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LOWER RIGHT SECTIONFormat. This is an indexed command item entry, with OIU actual telemetry status. Thisitem allows changing the OIU’s PDI format (ITEM 1 + xxx EXEC). The range ofallowable format numbers is 001 to 255, in decimal format. The status feedback is thecurrently loaded OIU PDI format.

Bus 1 (2-4) RT (BC) A (B) 2 (3-17). This section allows changing the OIU’s current MS1553 B bus processing state (Bus Controller or Remote Terminal) and prime buschannel (A or B) for any of the currently implemented four OIU MS 1553 B buses. Thestatus feedback is the actual IOU state for each bus and parameters, with an “∗”displayed to indicate the currently selected state. For example, if bus 3 is BC and usingchannel A, there is an “∗” next to items 11 and 12. To change bus 3 to RT, an “ITEM 10EXEC” is performed. In the case of the bus channelization (“A” or “B”), the displayedtelemetry indicates which channel is prime for command and telemetry transactions onthat bus, if the OIU is BC on that bus. If the OIU is BC on a bus, it tries to send acommand for an AD associated with that bus using the prime channel. If the OIUreceives no MS1553B status message from that AD, it tries again on the prime channel,then the alternate channel; if the AD has not responded, it declares it failed and stopstrying to send that command to that AD. When the OIU is RT on a bus, it responds oneither channel, depending on which channel received a MS1553B transaction from theBC; therefore, the channel priority has no meaning when the OIU is RT on a bus.

18 Spare Cmd. This item entry has command entry feedback only, no actual OIUfeedback. This item entry is an indexed command that allows performing the followinginternal OIU function mapping.

Item 18 + 1: Change FGB MDM Active Device to FGB-2 MDM Physical DeviceItem 18 + 2: Change FGB MDM Active Device to FGB-1 MDM Physical DeviceItem 18 + 3: Change Node 1 MDM Active Device to N1-2 MDM Physical DeviceItem 18 + 4: Change Node 1 MDM Active Device to N1-1 MDM Physical DeviceItem 18 + 5: Move FGB-2 MDM Physical Device to OIU bus 4 (UB ORB N1-2)Item 18 + 6: Move FGB-2 MDM Physical Device to OIU bus 3 (UB ORB N1-1)Item 18 + 7: Move FGB-1 MDM Physical Device to OIU bus 4 (UB ORB N1-2)Item 18 + 8: Move FGB-1 MDM Physical Device to OIU bus 3 (UB ORB N1-1)

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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/202/XXX CBM POWER XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 4 PRI SEC PRI SEC 5 ON/OFF TRIP ON/OFF TRIP ON/OFF TRIP ON/OFF TRIP 6 FORWARD AFT 7 1 1X 2X S 25X 26X S 8 2 3X 4X S 27X 28X S 9 3 5X 6X S 29X 30X S10 4 7X 8X S 31X 32X S1112 PORT STARBOARD13 1 9X 10X S 33X 34X S 1 49X 50X S 65X 66X S14 2 11X 12X S 35X 36X S 2 51X 52X S 67X 68X S15 3 13X 14X S 37X 38X S 3 53X 54X S 69X 70X S16 4 15X 16X S 39X 40X S 4 55X 56X S 71X 72X S1718 ZENITH NADIR19 1 17X 18X S 41X 42X S 1 57X 58X S 73X 74X S20 2 19X 20X S 43X 44X S 2 59X 60X S 75X 76X S21 3 21X 22X S 45X 46X S 3 61X 62X S 77X 78X S22 4 23X 24X S 47X 48X S 4 63X 64X S 79X 80X S23242526

Figure 5.- 202 CBM Power Display.

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PARAMETER CHARACTERISTICS: SM 202 CBM POWER DISPLAY

CRT NAME MSID DISPLAY RANGE STATUS INDICATORSH L M ↑ ↓

FORWARD PRI 1 ON/OFF P79X0320E 1 = ON, 0 = OFF




FORWARD PRI 1 TRIP P79X0427E 1 = YES, 0 = NO ↓




PORT PRI 1 ON/OFF P79X0367E 1 = ON, 0 = OFF




PORT PRI 1 TRIP P79X0468E 1 = YES, 0 = NO ↓




ZENITH PRI 1 ON/OFF P79X0315E 1 = ON, 0 = OFF




ZENITH PRI 1 TRIP P79X0422E 1 = YES, 0 = NO ↓




FORWARD SEC 1 ON/OFF P79X0325E 1 = ON, 0 = OFF




FORWARD SEC 1 TRIP P79X0432E 1 = YES, 0 = NO ↓

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PORT SEC 1 ON/OFF P79X0349E 1 = ON, 0 = OFF




PORT SEC 1 TRIP P79X0456E 1 = YES, 0 = NO ↓




ZENITH SEC 1 ON/OFF P79X0331E 1 = ON, 0 = OFF




ZENITH SEC 1 TRIP P79X0438E 1 = YES, 0 = NO ↓




STARBOARD PRI 1 ON/OFF P79X0361E 1 = ON, 0 = OFF




STARBOARD PRI 1 TRIP P79X0462E 1 = YES, 0 = NO ↓




NADIR PRI 1 ON/OFF P79X0310E 1 = ON, 0 = OFF


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NADIR PRI 1 TRIP P79X0520E 1 = YES, 0 = NO ↓




STARBOARD SEC 1 ON/OFF P79X0355E 1 = ON, 0 = OFF




STARBOARD SEC 1 TRIP P79X0474E 1 = YES, 0 = NO ↓




NADIR SEC 1 ON/OFF P79X0336E 1 = ON, 0 = OFF




NADIR SEC 1 TRIP P79X0443E 1 = YES, 0 = NO ↓




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ITEM ENTRY CHARACTERISTICS: SM 202 CBM POWER DISPLAY

Items 1 and 2: FORWARD PRI RPC 3 ON (OFF) - applies power to and powers offthe Forward Primary circuit 1. Items 1 and 2 are power up andpower down commands of the RPC 3 circuit. Those bolts andlatches would lose power if the circuit were tripped (see the CBMControl display for the specific bolts and latch). Upon completion ofeach command, an asterisk is driven adjacent to the item number.The corresponding trip field will indicate a tripped circuit and willcause an asterisk and a down arrow to be driven in the parameterstatus column if the appropriate discrete is set high. Accompanyingthe tripped indication, a fault message is driven on the messageline indicating the source of the tripped circuit.

The power primary and secondary parameter fields are in partitionedgroups of four. There are groups of bolts and latches that arepowered by each group under the header of primary andsecondary. Each of the groups have a dedicated RPC for thatgroup. (A check of the specific components powered by the RPCsand RPCMs is found in the Electrical Power ArchitectureWorkbook.)

Items 25 and 26: The Secondary circuit fields are displayed similarly to the Primarycircuits.

Items 3 and 4: FORWARD PRI RPC 4 ON (OFF) - similarly power the bolts andlatch tied to the RPC 4 circuit.


Items 5 and 6: FORWARD PRI RPC 5 ON (OFF) - similarly be powered by RPC 5.




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Items 9 and 10: PORT PRI RPC 3 ON (OFF) - applies power to and powers off thePort Primary circuit 1. Items 9 and 10 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.



Items 11 and 12: PORT PRI RPC 4 ON (OFF) - similarly be powered by RPC 4.






Items 17 and 18: ZENITH PRI RPC 3 ON (OFF) - applies power to and powers off theZenith Primary circuit 1. Items 17 and 18 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.

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The power primary and secondary parameter fields are in partitionedgroups of four. There are groups of bolts and latches that arepowered by each group under the header of primary andsecondary. Each of the groups have a dedicated RPC for thatgroup. (A check of the specific components powered by the RPCsand RPCMs is found in the Electrical Power ArchitectureWorkbook).


Items 19 and 20: ZENITH PRI RPC 4 ON (OFF) - similarly power the bolts and latchtied to the RPC 4 circuit.


Items 21 and 22: ZENITH PRI RPC 5 ON (OFF) - similarly be powered by RPC 5.




Items 49 and 50: STARBOARD PRI RPC 3 ON (OFF) - applies power to and powersoff the Starboard Primary circuit 1. Items 49 and 50 are power upand power down commands of the RPC 3 circuit. Those bolts andlatches would lose power if the circuit were tripped (see the CBMControl display for the specific bolts and latch). Upon completion ofeach command, an asterisk is driven adjacent to the item number.The corresponding trip field will indicate a tripped circuit and willcause an asterisk and a down arrow to be driven in the parameterstatus column if the appropriate discrete is set high. Accompanyingthe tripped indication, a fault message is driven on the messageline indicating the source of the tripped circuit.

The power primary and secondary parameter fields are partitioned ingroups of four. There are groups of bolts and latches that arepowered by each group under the header of primary andsecondary. Each of the groups have a dedicated RPC for thatgroup. (A check of the specific components powered by the RPCsand RPCMs is found in the Electrical Power ArchitectureWorkbook.)


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Items 51 and 52: STARBOARD PRI RPC 4 ON (OFF) - similarly power the bolts andlatch tied to the RPC 4 circuit.


Items 53 and 54: STARBOARD PRI RPC 5 ON (OFF) - similarly be powered by RPC 5.




Items 57 and 58: NADIR PRI RPC 3 ON (OFF) - applies power to and powers off theNadir Primary circuit 1. Items 57 and 58 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.



Items 59 and 60: NADIR PRI RPC 4 ON (OFF) - similarly power the bolts and latchtied to the RPC 4 circuit.


Items 61 and 62: NADIR PRI RPC 5 ON (OFF) - similarly be powered by RPC 5.

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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/222/XXX CBM POWER-2N XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 4 PRI SEC PRI SEC 5 ON/OFF TRIP ON/OFF TRIP ON/OFF TRIP ON/OFF TRIP 6 FORWARD AFT 7 1 1X 2X S 25X 26X S 8 2 3X 4X S 27X 28X S 9 3 5X 6X S 29X 30X S10 4 7X 8X S 31X 32X S1112 PORT STARBOARD13 1 9X 10X S 33X 34X S 1 49X 50X S 65X 66X S14 2 11X 12X S 35X 36X S 2 51X 52X S 67X 68X S15 3 13X 14X S 37X 38X S 3 53X 54X S 69X 70X S16 4 15X 16X S 39X 40X S 4 55X 56X S 71X 72X S1718 ZENITH NADIR19 1 17X 18X S 41X 42X S 1 57X 58X S 73X 74X S20 2 19X 20X S 43X 44X S 2 59X 60X S 75X 76X S21 3 21X 22X S 45X 46X S 3 61X 62X S 77X 78X S22 4 23X 24X S 47X 48X S 4 63X 64X S 79X 80X S2324

Figure 6.- 222 CBM Power - 2N Display.

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PORT SEC 4 ON/OFF P79X0785E 1= ON, 0 = OFF























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ITEM ENTRY CHARACTERISTICS: SM 222 CBM POWER DISPLAY

Items 1 and 2: FORWARD PRI RPC 3 ON (OFF) - applies power to and powers offthe Forward Primary circuit 1. Items 1 and 2 are power up andpower down commands of the RPC 3 circuit. Those bolts andlatches would lose power if the circuit were tripped (see the CBMControl display for the specific bolts and latch). Upon completion ofeach command, an asterisk is driven adjacent to the item number.The corresponding trip field will indicate a tripped circuit and willcause an asterisk and a down arrow to be driven in the parameterstatus column if the appropriate discrete is set high. Accompanyingthe tripped indication, a fault message is driven on the messageline indicating the source of the tripped circuit.



Items 3 and 4: FORWARD PRI RPC 4 ON (OFF) - similarly power the bolts andlatch tied to the RPC 4 circuit.






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Items 9 and 10: PORT PRI RPC 3 ON (OFF) - applies power to and powers off thePort Primary circuit 1. Items 9 and 10 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.









Items 17 and 18: ZENITH PRI RPC 3 ON (OFF) - applies power to and powers off theZenith Primary circuit 1. Items 17 and 18 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.

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The power primary and secondary parameter fields are in partitionedgroups of four. There are groups of bolts and latches that arepowered by each group under the header of primary andsecondary. Each of the groups have a dedicated RPC for thatgroup. (A check of the specific components powered by the RPCsand RPCMs is found in the Electrical Power ArchitectureWorkbook).


Items 19 and 20: ZENITH PRI RPC 4 ON (OFF) - similarly power the bolts and latchtied to the RPC 4 circuit.






Items 49 and 50: STARBOARD PRI RPC 3 ON (OFF) - applies power to and powersoff the Starboard Primary circuit 1. Items 49 and 50 are power upand power down commands of the RPC 3 circuit. Those bolts andlatches would lose power if the circuit were tripped (see the CBMControl display for the specific bolts and latch). Upon completion ofeach command, an asterisk is driven adjacent to the item number.The corresponding trip field will indicate a tripped circuit and willcause an asterisk and a down arrow to be driven in the parameterstatus column if the appropriate discrete is set high. Accompanyingthe tripped indication, a fault message is driven on the messageline indicating the source of the tripped circuit.


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Items 51 and 52: STARBOARD PRI RPC 4 ON (OFF) - similarly power the bolts andlatch tied to the RPC 4 circuit.






Items 57 and 58: NADIR PRI RPC 3 ON (OFF) - applies power to and powers off theNadir Primary circuit 1. Items 57 and 58 are power up and powerdown commands of the RPC 3 circuit. Those bolts and latcheswould lose power if the circuit were tripped (see the CBM Controldisplay for the specific bolts and latch). Upon completion of eachcommand, an asterisk is driven adjacent to the item number. Thecorresponding trip field will indicate a tripped circuit and will cause anasterisk and a down arrow to be driven in the parameter statuscolumn if the appropriate discrete is set high. Accompanying thetripped indication, a fault message is driven on the message lineindicating the source of the tripped circuit.



Items 59 and 60: NADIR PRI RPC 4 ON (OFF) - similarly power the bolts and latchtied to the RPC 4 circuit.


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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/200/XXX APCU STATUS XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 4 APCU 1 APCU 2 5 6 CONV A 7 OUT AMPS XX.X XX.X 8 TEMP XXX.X XXX.X 9 CONV B10 OUT AMPS XX.X XX.X11 TEMP XXX.X XXX.X1213 OUT VOLTS14 RES LOW XXX.X XXX.X15 RES HIGH XXX.X XXX.X1617 TRIP X.XX X.XX181920212223242526

Figure 7.- 200 APCU Status Display.

The APCU STATUS display is an SM display (DISP 200) available in SM OPS 2 and 4which provides output power, thermal, and trip data on the Assembly Power ConverterUnit.

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PARAMETER CHARACTERISTICS: SM 200 APCU STATUS DISPLAY

CRT NAME MSID UNITS DISPLAYRANGE

STATUSINDICATORS

FDA LIMITS

M H L ↑ ↓ Lower Upper

APCU 1CONV A

OUTAMPS

P50C9003V Amps 0 to 12 M H ↑ 0SL 7.5 A TMBUto 8.5A

OUTTEMP

P50T9002V °F 0 to 212 M H ↑ 0SL TMBUto 20 °F

120 °FTMBU to130°F

CONV BOUTAMPS


OUTTEMP



OUT VOLTSLOW RES P50V9001V volts 0 to 180 MHIGH RES P50V9000V volts 110 to 160 M H L ↑ ↓ 122 V 130 V

TMBU to126.5V

TRIP [1] P50V9006V volts see remarks M H ↑ 0SL TMBUto -99998

-4.60 VTMBU to-4.40 V

APCU 2CONV A

OUTAMPS


OUTTEMP



CONV BOUTAMPS

P50C9011V Amps 0 to 12 M H ↑ 0SL 7.5 ATMBU to8.5A

OUTTEMP



OUT VOLTSLOW RES P50V9007V volts 0 to 180 MHIGH RES P50V9008V volts 110 to 160 M H L ↑ ↓ 122 V 130 V

TMBU to126.5V

TRIP [1] P50V9013V volts see remarks M H ↑ 0SL TMBUto -99998

-4.60 VTMBU to-4.40 V

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REMARKS

[1] The TRIP status voltage can be interpreted using the following table.

TRIP TRIP CAUSE(S)(STATUS

VOLTAGE)OV OUV OC IUV

+4.88 X X X X+4.23 X X X+3.59 X X X+2.95 X X+2.27 X X X+1.62 X X+0.98 X X+0.34 X-0.30 X X X-0.95 X X-1.59 X X-2.23 X-2.91 X X-3.56 X-4.20 X

-4.86 (NO TRIP)NOTES:

OV: Output OvervoltageOUV: Output UndervoltageOC: Output OvercurrentIUV: Input Undervoltage

The tolerance for all reported voltages is ± 0.2 volts.

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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/XXX/216 FGB/SM C&W XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 EMERGENCY SM THERMAL AVIONICS 4 FGB FIRE S COOLING LOOP 1 2 REDUND LOSS 5 SM FIRE S OPS FAIL S SM CC S 6 DP/DT S OFF-NOM TC S 7 TOX ATM S SHUTDOWN S S BUS FAIL A B 8 CABIN REG CNTL RS 1 S S 9 FGB SMOKE S FAIL S S 2 S S10 SM SMOKE S 3 S S11 PRESS HI S 4 S S12 LO S HEATING LOOP 1 2 MU FAIL13 PPO2 HI S OPS FAIL S SM 1 S 4 S14 LO S 2 S 5 S15 PPCO2 HI S 3 S 6 S16 FGB S17 PPH2 HI S181920 SM POWER SM MCS21 TOT BATT CHG XXXXXX.XS GNC FAIL S22 PWR LO S SV DGRD S23 LOAD SHED S2425 (XX)26

Figure 8.- 216 FGB/SM C&W Display.

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PARAMETER CHARACTERISTICS: SM 216 FGB/SM C&W DISPLAY


STATUSINDICATORS

FDA(Limits)

H L M ↑ ↓ HI LOFGB FIRE P79X0700E ----------- ----------------- M ↓ ----------- 1SM FIRE P79X0832E ----------- ----------------- M ↓ ----------- 1SM DP/DT P79X0702E ----------- ----------------- M ↓ ----------- 1SM TOX ATM P79X0703E ----------- ----------------- M ↓ ----------- 1FGB SMOKE P79X0704E ----------- ----------------- M ↓ ----------- 1SM SMOKE P79X0705E ----------- ----------------- M ↓ ----------- 1SM PRESS HI P79X0706E ----------- ----------------- M ↓ ----------- 1SM PRESS LO P79X0707E ----------- ----------------- M ↓ ----------- 1

SM PPO2 HI P79X0708E ----------- ----------------- M ↓ ----------- 1

SM PPO2 LO P79X0709E ----------- ----------------- M ↓ ----------- 1SM PPCO2 HI P79X0710E ----------- ----------------- M ↓ ----------- 1

SM PPH2 HI P79X0712E ----------- ----------------- M ↓ ----------- 1SM COOLING LOOP 1 OPS FAIL P79X0717E ----------- ----------------- M ↓ ----------- 1SM COOLING LOOP 1 OFF-NOM SHUTDOWN P79X0833E ----------- ----------------- M ↓ ----------- 1SM COOLING LOOP 1 REG CNTL FAIL P79X0722E ----------- ----------------- M ↓ ----------- 1SM COOLING LOOP 2 OFF-NOM SHUTDOWN P79X0834E ----------- ----------------- M ↓ ----------- 1SM COOLING LOOP 2 REG CNTL FAIL P79X0723E ----------- ----------------- M ↓ ----------- 1SM HEATING LOOP 1 OPS FAIL P79X0716E ----------- ----------------- M ↓ ----------- 1AVIONICS REDUND LOSS SM CC P79X0733E ----------- ----------------- M ↓ ----------- 1AVIONICS REDUND LOSS SM TC P79X0734E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 1 A P79X0739E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 1 B P79X0740E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 2 A P79X0741E ----------- ----------------- M ↓ ----------- 1

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PARAMETER CHARACTERISTICS: SM 216 FGB/SM C&W DISPLAY


STATUSINDICATORS

FDA(Limits)

H L M ↑ ↓ HI LOAVIONICS BUS FAIL RS 2 B P79X0742E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 3 A P79X0735E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 3 B P79X0736E ----------- ----------------- M ↓ ----------- 1

AVIONICS BUS FAIL RS 4 A P79X0737E ----------- ----------------- M ↓ ----------- 1AVIONICS BUS FAIL RS 4 B P79X0738E ----------- ----------------- M ↓ ----------- 1AVIONICS MU FAIL SM 1 P79X0743E ----------- ----------------- M ↓ ----------- 1

AVIONICS MU FAIL SM 2 P79X0744E ----------- ----------------- M ↓ ----------- 1

AVIONICS MU FAIL SM 3 P79X0745E ----------- ----------------- M ↓ ----------- 1AVIONICS MU FAIL SM 4 P79X0746E ----------- ----------------- M ↓ ----------- 1AVIONICS MU FAIL SM 5 P79X0747E ----------- ----------------- M ↓ ----------- 1AVIONICS MU FAIL SM 6 P79X0748E ----------- ----------------- M ↓ ----------- 1AVIONICS MU FAIL FGB P79X0749E ----------- ----------------- M ↓ ----------- 1SM POWER TOT BATT CHG P79E0713D AMPS -9.97 ---

+125877.5H L M N/A N/A

SM POWER PWR LO P79X0714E ----------- ----------------- M ↓ ----------- 1SM POWER LOAD SHED P79X0715E ----------- ----------------- M ↓ ----------- 1SM MCS GNC FAIL P79X0750E ----------- ----------------- M ↓ ----------- 1SM MCS SV DGRD P79X0751E ----------- ----------------- M ↓ ----------- 1

REMARKS

None

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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/220/XXX NODE 1-2N XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 PRI MDM SEC MDM 4 PHY ID XXXX XXXX CABIN PRESS XX.XXS 5 STATE XXXX XXXX 6 STBY 1 2 BUS CONFIG 7 N1-1 TO SEC 3 CH A CH B 8 CONFIG XXX XXX N1-1 MDM 9 UB ORB N1-1 XX 19X 20X10 FRM CTR XX XX CB GNC-1 XX 21X 22X11 SYNC XXXS LB LAB SYS-1 XX 23X 24X1213 TEMP N1-1 XXXX N1-2 MDM14 N1-2 XXXX UB ORB N1-2 XX 25X 26X15 LOAD SHED CB GNC-2 XX 27X 28X16 VIA NCS 4+ LB LAB SYS-2 XX 29X 30X17 FGB XXXS18 POWER ON OFF TRIP PRI MDM19 N1-1 MDM 7X 8X S UB EPS N1-14 XX 31X 32X20 SDO A 9X 10X S N1-23 XX 33X 34X21 B 11X 12X S22 N1-2 MDM 13X 14X S ISS C&W TONE STATUS23 SDO A 15X 16X S FIRE S24 B 17X 18X S WARN S CAUT S2526

Figure 9.- 220 Node 1 - 2N Display.

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PARAMETER CHARACTERISTICS: SM 220 NODE 1-2N DISPLAY

CRT NAME MSID UNITS DISPLAY RANGE STATUSINDICATORS

FDA(Limits)

H L M ↑ ↓ HI LOPHY ID PRI MDM [1] P79X0484E ----------- 1 = N1-2,

0 = N1-1----------- ---------

PHY ID SEC MDM [1] P79X0486E ----------- 1 = N1-2,0 = N1-1

----------- ---------

STATE PRI MDM BIT 5/6/7 [2] P79X0120E,P79X0487E,P79X0488E

----------- 001 = STBY010 = PRI011 = SEC111 = DIA

----------- ---------

STATE SEC MDM BIT 5/6/7 [2] P79X0111E,P79X0489E,P79X0490E

----------- 001 = STBY010 = PRI011 = SEC111 = DIA

----------- ---------

LOAD SHED VIA FGB [6] P79X0058E,P79X0066E,P79X0072E

----------- 100 or 001= NO010 or 110 = YES

↓ N/A 1

CONFIG PRI MDM BIT 3-6 [3] P79X0118E,P79X0500E →P79X0502E

----------- C01 --- C16 ----------- ---------

CONFIG SEC MDM BIT 3-6 [3] P79X0109E,P79X0503E →P79X0505E

----------- C01 --- C16 ----------- ---------

FRM CTR PRI MDM [4] P79U0509D ----------- INCREMENT ----------- ---------

FRM CTR SEC MDM [4] P79U0114D ----------- INCREMENT ----------- ---------

SYNC - SEC MDM [5] P79X0112E ----------- 1 = NO,0 = YES

↓ N/A 1

TEMP N1-1 P79T0106A °F -428 --- 470

TEMP N1-2 P79T0107A °F -428 --- 470

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FDA(Limits)

H L M ↑ ↓ HI LON1-1 MDM POWER ON P79X0781E ----------- 1 = *

0 = blank----------- ---------

N1-1 MDM POWER OFF P79X0781E ----------- 1 = blank0 = *

----------- ---------

N1-1 MDM POWER TRIP P79X0453E ----------- ----------------- ↓ N/A 1N1-1 SDO A POWER ON P79X0779E ----------- 1 = *

0 = blank----------- ---------

N1-1 SDO A POWER OFF P79X0779E ----------- 1 = blank0 = *

----------- ---------

N1-1 SDO A POWER TRIP P79X0450E ----------- ----------------- ↓ N/A 1N1-1 SDO B POWER ON P79X0780E ----------- 1 = *

0 = blank----------- ---------

N1-1 SDO B POWER OFF P79X0780E ----------- 1 = blank0 = *

----------- ---------

N1-1 SDO B POWER TRIP P79X0451E ----------- ----------------- ↓ N/A 1N1-2 MDM POWER ON P79X0800E ----------- 1 = *

0 = blank----------- ---------

N1-2 MDM POWER OFF P79X0800E ----------- 1 = blank0 = *

----------- ---------

N1-2 MDM POWER TRIP P79X0300E ----------- ----------------- ↓ N/A 1N1-2 SDO A POWER ON P79X0794E ----------- 1 = *

0 = blank----------- ---------

N1-2 SDO A POWER OFF P79X0794E ----------- 1 = blank0 = *

----------- ---------

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FDA(Limits)

H L M ↑ ↓ HI LON1-2 SDO A POWER TRIP P79X0298E ----------- ----------------- ↓ N/A 1

N1-2 SDO B POWER ON P79X0795E ----------- 1 = *0 = blank

----------- ---------

N1-2 SDO B POWER OFF P79X0795E ----------- 1 = blank0 = *

----------- ---------

N1-2 SDO B POWER TRIP P79X0299E ----------- ----------------- ↓ N/A 1

CABIN PRESS [7] P79P0493A PSIA -0.08 --- 20 ↑ ↓ 15 13.9

UB ORB N1-1 BUS CONFIG [8] P79X0128E,P79X0491E

----------- 00 = NA01 = RT10 = BC

----------- ---------

UB ORB N1-1 BUS CONFIG CH A P79X0230E ----------- 1 = blank0 = *

----------- ---------

UB ORB N1-1 BUS CONFIG CH B P79X0230E ----------- 1 = *0 = blank

----------- ---------

CB GNC-1 BUS CONFIG BIT 6/7 [8] P79X0126E,P79X0492E

----------- 00 = NA01 = RT10 = BC

----------- ---------

CB GNC-1 BUS CONFIG CH A P79X0229E ----------- 1 = blank0 = *

----------- ---------

CB GNC-1 BUS CONFIG CH B P79X0229E ----------- 1 = *0 = blank

----------- ---------

LB LAB SYS-1 BUS CONFIG BIT 6/7[8]

P79X0124E,P79X0494E

----------- 00 = NA01 = RT10 = BC

----------- ---------

LB LAB SYS-1 BUS CONFIG CH A P79X0228E ----------- 1 = blank0 = *

----------- ---------

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FDA(Limits)

H L M ↑ ↓ HI LOLB LAB SYS-1 BUS CONFIG CH B P79X0228E ----------- 1 = *

0 = blank----------- ---------

UB ORB N1-2 BUS CONFIG BIT 6/7[8]

P79X0134E,P79X0495E

----------- 00 = NA01 = RT10 = BC

----------- ---------

UB ORB N1-2 BUS CONFIG CH A P79X0233E ----------- 1 = blank0 = *

----------- ---------

UB ORB N1-2 BUS CONFIG CH B P79X0233E ----------- 1 = *0 = blank

----------- ---------

CB GNC-2 BUS CONFIG BIT 6/7 [8] P79X0132E,P79X0496E

----------- 00 = NA01 = RT10 = BC

----------- ---------

CB GNC-2 BUS CONFIG CH A P79X0232E ----------- 1 = blank0 = *

----------- ---------

CB GNC-2 BUS CONFIG CH B P79X0232E ----------- 1 = *0 = blank

----------- ---------

LB LAB SYS-2 BUS CONFIG BIT 6/7[8]

P79X0130E,P79X0497E

----------- 00 = NA01 = RT10 = BC

----------- ---------

LB LAB SYS-2 BUS CONFIG CH A P79X0231E ----------- 1 = blank0 = *

----------- ---------

LB LAB SYS-2 BUS CONFIG CH B P79X0231E ----------- 1 = *0 = blank

----------- ---------

UB EPS N1-14 BUS CONFIG BIT 6/7[8]

P79X0140E,P79X0498E

----------- 00 = NA01 = RT10 = BC

----------- ---------

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FDA(Limits)

H L M ↑ ↓ HI LOUB EPS N1-14 BUS CONFIG CH A P79X0234E ----------- 1 = blank

0 = *----------- ---------

UB EPS N1-14 BUS CONFIG CH B P79X0234E ----------- 1 = *0 = blank

----------- ---------

UB EPS N1-23 BUS CONFIG BIT 6/7[8]

P79X0122E,P79X0499E

----------- 00 = NA01 = RT10 = BC

----------- ---------

UB EPS N1-23 BUS CONFIG CH A P79X0227E ----------- 1 = blank0 = *

----------- ---------

UB EPS N1-23 BUS CONFIG CH B P79X0227E ----------- 1 = *0 = blank

----------- ---------

FIRE [9] P79X0161E ----------- ----------------- ↓ N/A 1

WARN [9] P79X0158E ----------- ----------------- ↓ N/A 1

CAUT [9] P79X0157E ----------- ----------------- ↓ N/A 1

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REMARKS

[1] The PHY ID field will display ‘N1-1’ or ‘N1-2’ to indicate which ISS Node 1Multiplexer/ Demultiplexer (MDM) is the primary (PRI) and secondary (SEC) NodeControl Software (NCS) MDM. For nominal operations, N1-2 will be the PRI MDMand N1-1 will be the SEC MDM.

[2] The STATE field indicates the operational state of the primary and secondaryMDMs. This field will read ‘PRI’ for primary, ‘SEC’ for secondary, ‘STBY’ forstandby and ‘DIA’ for diagnostics.

[3] The CONFIG field indicates the configuration number (C01 - C16) of the NCSrunning in the primary and secondary MDMs.

[4] By checking to see if the frame counters (FRM CTR) for the PRI and SEC MDMsare incrementing, the crew can determine whether data is being received fromthe MDMs.

[5] The SYNC field will display either ‘YES’ or ‘NO’ to indicate whether or not the SECMDM is communicating with the PRI MDM. This field applies to the secondaryMDM only. When the SEC MDM has lost sync with the PRI MDM, ‘NO’ will bedisplayed in the SYNC field and the crew will receive an alert light, tone, and faultmessage.

[6] If any three or more FGB batteries read 25 volts or less, the FGB will send a C&Wto the Node 1 MDMs, which will activate the load shed table. If this occurs, theLOAD SHED VIA FGB field will display ‘YES’ and a down-arrow will be displayedin the status field. The crew will also receive an alert light, tone, and faultmessage. Otherwise, the field will display ‘NO’.

[7] The CABIN PRESS field displays the Node 1 cabin pressure. When thisparameter exceeds its lower/upper FDA limits, a down or an up arrow will bedisplayed in the status field. The crew will also receive a master alarm light andtone, a B/U C/W light on panel F7, and a fault message.

[8] BUS CONFIG displays information on the ISS 1553B buses. The field to the rightof the bus name displays the configuration of the buses connected to thespecified MDM. This field will read either ‘BC’ for bus controller, ‘RT’ for remoteterminal, or ‘NA’ for not available.

[9] ISS C&W TONE STATUS: Since the Early Portable Computer System (PCS)does not have the capability to annunciate alarm tones, the tone status flag fromthe NCS will be used to trigger the orbiter C&W system. When the tone statusflag is set for any FIRE, WARNING, or CAUTION event, a down-arrow will bedisplayed in the appropriate status field. For a ‘FIRE’ event, the crew will receivea master alarm light and tone, a B/U C/W light on panel F7, and a fault message.For ‘WARN’ and ‘CAUT’ events, the crew will receive an alert light, tone, andfault message. The crew will then have to refer to the PCS for details on the faultcondition.

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ITEM ENTRY CHARACTERISTICS: SM 220 NODE 1-2N DISPLAY

Items 1 and 2: STBY - allows the crew to command either the primary or secondaryMDM to the Standby state.

Item 3: N1-1 TO SEC - commands N1-1 to the secondary state.

Item 4: LOAD SHED VIA NCS - activates the Node 1 Load Shed Table,which will power off everything in the Node 1, except the MDMs.This command will be used by the crew in response to a fire in theNode. This command is protected to prevent inadvertent execution;therefore, an ITEM 4 + 99 entry is required. Currently, there is notelemetry from the NCS to indicate the status of the load shed. Theload shed table can also be activated without crew or groundintervention.

Items 7 --- 12: N1-1 POWER ON/OFF - allows the crew to close (Power On) andopen (Power Off) the RPCs associated with the MDM power suppliesand Solenoid Driver Output (SDO) A and B cards. An asterisk willbe displayed next to the appropriate item number to indicate thepower status. A down-arrow will be displayed in the Trip Statusfield when an RPC has tripped. The crew will also receive an alertlight, tone, and fault message.

Items 13 --- 18: N1-2 POWER ON/OFF - allows the crew to close (Power On) andopen (Power Off) the RPCs associated with the MDM powersupplies SDO A and B cards. An asterisk will be displayed next tothe appropriate item number to indicate the power status. A down-arrow will be displayed in the Trip Status field when an RPC hastripped. The crew will also receive an alert light, tone, and faultmessage.

Items 19 --- 34: BUS CONFIG CH A/CH B - allows the crew to select either ChannelA or B on each of the buses. An asterisk will be displayed next tothe appropriate item number to indicate the selected channel.

Items 19 and 20: UB ORB N1-1 CH A/CH B - allows the crew to select which channel(A, B) the N1-1 MDM will communicate on the UB ORB N1-1 bus.

Item 21 and 22: CB GNC-1 CH A/CH B - allows the crew to select which channel (A, B)the N1-1 MDM will communicate on the CB GNC-1 bus.

Items 23 and 24: LB LAB SYS-1 CH A/CH B - allows the crew to select which channel(A, B) the N1-1 MDM will communicate on the LB LAB SYS-1 bus.

Items 25 and 26: UB ORB N1-2 CH A/CH B - allows the crew to select which channel(A, B) the N1-2 MDM will communicate on the UB ORB N1-2 bus.

Items 27 and 28: CB GNC-2 CH A/CH B - allows the crew to select which channel (A, B)the N1-2 MDM will communicate on the CB GNC-2 bus.

Items 29 and 30: LB LAB SYS-2 CH A/CH B - allows the crew to select which channel(A, B) the N1-2 MDM will communicate on the LB LAB SYS-2 bus.

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ITEM ENTRY CHARACTERISTICS: SM 220 NODE 1-2N DISPLAY (cont)

Items 31 and 32: UB EPS N1-14 CH A/CH B - allows the crew to select which channel(A, B) the PRI MDM will communicate on the UB EPS N1-14 bus.

Items 33 and 34: UB EPS N1-23 CH A/CH B - allows the crew to select which channel(A, B) the PRI MDM will communicate on the UB EPS N1-23 bus.

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1 2 3 4 5123456789012345678901234567890123456789012345678901 XXXX/221/XXX CBM CONTROL-2N XX X DDD/HH:MM:SS DDD/HH:MM:SS ALL STOP 1 BOLT CMDST POS LOAD XXXX COND CMD 1-1 XXXX XXX.X XXXXX.XX CBM CONF 2 R SAFE 19 2 XXXX XXX.X XXXXX.XX XXX 3 XXXX XXX.X XXXXX.XX M/S SAFVAL 20 4 XXXX XXX.X XXXXX.XX3 ZEN X X/XS RESET 21 1-2 XXXX XXX.X XXXXX.XX4 NAD X X/XS MSTR STAT 2 XXXX XXX.X XXXXX.XX5 FWD X X/XS XXXX 3 XXXX XXX.X XXXXX.XX6 PRT X X/XS 22 MASK XX 4 XXXX XXX.X XXXXX.XX 12345 1-3 XXXX XXX.X XXXXX.XXBBOLTCK 7 1XXXXX 2 XXXX XXX.X XXXXX.XXCLOSE 8 2XXXXX 3 XXXX XXX.X XXXXX.XXABOLT 9 3XXXXX 4 XXXX XXX.X XXXXX.XXIBOLT 1ST 10 4XXXXX 1-4 XXXX XXX.X XXXXX.XX 2ND 11 RTL 2 XXXX XXX.X XXXXX.XX 3RD 12 1 XX SS 3 XXXX XXX.X XXXXX.XX 4TH 13 2 XX SS 4 XXXX XXX.X XXXXX.XX 5TH 14 3 XX SS LAT CMDST ANG CAPSWFBOLT 15 4 XX SS 1 XXXX XXX XX SSLAT DEPLOY 16 BITALL 23 2 XXXX XXX XX SSCAPTURE-1 17 SET0 A 24 3 XXXX XXX XX SSCAPTURE-2 18 B 25 4 XXXX XXX XX SS

Figure 10.- 221 CBM Control - 2N Display.

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PARAMETER CHARACTERISTICS: SM 221 CBM CONTROL-2N DISPLAY


FDA(Limits)

H L M ↑ ↓ HI LO‘CONFIRMATION REQUEST’ [1] P79X0626E,

P79X0627E,P79X0628E,P79X0629E,P79X0630E,P79X0631E

-------------NONE, RSAF,UBLT, STOP,BIT, CAPT,BBLT, DBLT,ABLT, MASK,RSET, DPLY,CLOS, FBLT,IBLT, LBLT,RBLT, INIT

------ -------

ZEN M (MONITOR FIELD) P79X0606E,P79X0607E -------------

D = DEACTIVATEDA = ACTIVATEDM = MONITOR

------ -------

ZEN S P79U0616D-------------

0 = NOCONTROLLERSELECTED,1 = PRIME(MASTER) CNTLR2 = SECONDARYCONTROLLER

------ -------

NAD M (MONITOR FIELD) P79X0608E,P79X0609E -------------


------ -------

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FDA(Limits)

H L M ↑ ↓ HI LONAD S P79U0618D

-------------0 = NOCONTROLLERSELECTED,1 = PRIME(MASTER) CNTLR2 = SECONDARYCONTROLLER

------ -------

FWD M (MONITOR FIELD) P79X0610E,P79X0611E -------------


------ -------

FWD S P79U0620D-------------


------ -------

STB M (MONITOR FIELD) P79X0612E,P79X0613E -------------


------ -------

STB S P79U0622D-------------


------ -------

(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOPORT M (MONITOR FIELD) P79X0614E,

P79X0615E -------------D = DEACTIVATEDA = ACTIVATEDM = MONITOR

------ -------

PORT S P79U0624D-------------


------ -------

MSTR STAT P79X0091E,P79X0524E,P79X0525E,P79X0526E

------------- CPLT, PROG,PEND, ABRT,FAIL, TIME

------ -------

RTL 1 P79X0167E,P79X0168E -------------

O = OPENEDC = CLOSED

↓ ------ -------

RTL 2 P79X0176E,P79X0177E -------------


↓ ------ -------

RTL 3 P79X0185E,P79X0186E -------------


↓ ------ -------

RTL 4 P79X0194E,P79X0195E

------------- O = OPENEDC = CLOSED

↓ ------ -------

BOLT CMD STAT 1-1 [2] P79X0059E,P79X0527E,P79X0528E,P79X0529E

-------------CPLT, PROG, FAIL,BIND, INTF, STRP,NOEN, NOAD,MALF, MISS, JAMD,MSBD, ABRT

------ -------

(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOBOLT CMD STAT 2-1 P79X0061E,

P79X0539E,P79X0540E,P79X0541E


------ -------

BOLT CMD STAT 3-1 P79X0071E,P79X0551E,P79X0552E,P79X0553E


------ -------



------ -------



------ -------



------ -------

(Cont)

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FDA(Limits)


P79X0554E,P79X0555E,P79X0556E


------ -------



------ -------



------ -------



------ -------



------ -------

(Cont)

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FDA(Limits)


P79X0569E,P79X0570E,P79X0571E


------ -------



------ -------



------ -------



------ -------



------ -------

POSITION BOLT 1-1 P79H0034A Revs 0 --- 51 ------ -------


(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOPOSITION BOLT 1-3 P79H0037A Revs 0 --- 51 ------ -------














BOLT LOAD 1-1 P79G0002A POUNDS -1 to 25,000 ------ -------






(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOBOLT LOAD 2-3 P79G0012A POUNDS -1 to 25,000 ------ -------










LAT CMD STAT 1 P79X0093E,P79X0575E,P79X0576E,P79X0577E


------ -------



------ -------

(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOLAT CMD STAT 3 P79X0101E,

P79X0581E,P79X0582E,P79X0583E


------ -------



------ -------

LATCH SHAFT POSITION 1 (ANG) P79H0051A Revs 0 --- 51 ------ -------




CAP SW -1 (left) P79X0169E EVENT 1 = O (OPEN)/0 = blank

↓ ------ -------

-1 (right) P79X0170E EVENT 1 = C (CLOSED)/0 = blank

↓ ------ -------

-2 (left) P79X0178E EVENT 1 = O (OPEN)/0 = blank

↓ ------ -------


↓ ------ -------

(Cont)

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FDA(Limits)

H L M ↑ ↓ HI LOCAP SW -3 (left) P79X0187E EVENT 1 = O (OPEN)/

0 = blank↓ ------ -------


↓ ------ -------

-4 (left) P79X0196E EVENT 1 = O (OPEN)/0 = blank

↓ ------ -------


↓ ------ -------

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REMARKS

[1] The four-character field below displays ‘CONF’. It is the ‘confirmation request’field where the commanded process in work is displayed upon execution of an‘ITEM 2 EXEC’.

[2] Bolt Command Status, Position, and Loads are to the right of each bolt. For theCommand Status, each controller has a particular four-character field to denote ifthe command is: in progress, failed, if binding is detected, if interference isdetected, if missed capture is detected, if stripping is detected, if there is a noengaged condition, if there is a not adjusted condition, if a malfunction isdetected, if missing capture is detected, if a jam is detected, if a commandmissed a broadcast, and if a command was aborted. The user is cued from thisfield in the event a command has to be masked or if ground intervention isrequired.

Bolt position is identified to the right of the Command Stat field, and shows theprogress of bolt rotation for each once commands are issued. The user can usethis cue to determine if a slowdown or jam can be anticipated. This is a good boltprogress column for the user.

Bolt Load is displayed at the right of the display. With each bolt force commandincreasing as the sequence progresses, the crew can use this cue to determine ifan I_Bolt or F_Bolt command needs to be present.

[3] For each of the four capture latches at the bottom right, similar columns providethe user with latch insight as with the bolts above. Latch command status issimilar to the range of four-character fields for the bolt commands above. Latchangle shows the range of full latch extension to the retracted position.

The Capture Switch, along with the position switch, shows whether a particularlatch missed the incoming passive segment. An ‘O’ or ‘C’ under the ‘CA’ of theheader ‘CAPSW’ will indicate when a latch switch is open or closed. Under ‘SW’of the header a status field will indicate if an open circuit or switch short is evidentwith a down arrow displayed.

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ITEM ENTRY CHARACTERISTICS: SM 221 CBM CONTROL-2N DISPLAY

Items 1 and 2: Item 1 is an all stop command to be used in the event the crewneeds to stop any controller activity that could be considered aproblem. This is boxed on top as to allow rapid identification andexecution. The four-character field below displays ‘CONF.’ It is the‘confirmation request’ field where the commanded process in workis displayed upon execution of an ‘ITEM 2 EXEC’. The command isa two-step MDM software process to override the firmwarecommand validation step or to send a command which the firmwareconsiders non-default (nominally sent during the ABOLTcommand).

Below the CBM Confirm Item 2 are the CBM activation hex entriesfor powering up the opening desired.

Items 3 --- 6: These will be mission unique and will represent Node 1 for earlyassembly flights and Node 2 for the later flights. These commandswill be given to the “active” side of the CBM desired usually at thenode interface. ‘ITEM 3 +1 EXEC’ will select a primary (master)controller. ‘ITEM 3 +2 EXEC’ will select a secondary controller. Ineach case the index number is displayed in the hex field as a crewcue as to which was selected. This is the beginning of the nominalprocedures after the power up steps. Item 3 will select the ZenithCBM items 4, 5, 6, and 7 work similarly if procedures require theseto be activated.

The ‘M/S’ fields adjacent to the index field shows the user whetherthe CBM is activated, deactivated, or in the Monitor state. An ‘A’ isdisplayed if activated, a ‘D’ is displayed if deactivated, and an ‘M’ isdisplayed if in the monitor state. The ‘S’ field displays a 0, 1, 2, or 3and shows the user if the CBM selected is using no controller, aprime controller, or a backup controller. These correspond to theactivate and deactivate command.

Items 7 --- 9: The ‘BBOLTCK’ command ‘ITEM 7 EXEC’ drives all 16 bolts out 2turns and in 3 turns. This is a test of the bolt and motor operationto ensure they work as desired prior to the mating operation. TheITEM 8 EXEC draws all latches from the extended position towardthe retracted position, thus bringing the passive CBM toward theactive CBM in preparation for the ABOLT command. The ‘ITEM 9EXEC’ drives out all 16 bolts to acquire the passive correspondingnuts.

Item 10-14: IBOLT - command continues the bolting process but takes all bolts toa higher or interim load (torquing all bolts 5 times).

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ITEM ENTRY CHARACTERISTICS: SM 221 CBM CONTROL-2N DISPLAY (Cont)

Item 15: FBOLT - command continues the bolt torque until the bolts are takento their final load. This command is sent several times to ensure thebolts reach their final load.

Item 16: LAT DEPLOY - command sends out the latches (four) from theretracted position in preparation to grapple the passive portion ofthe CBM of the component to be berthed.

Item 17: CAPTURE-1 - command moves all four capture to the closedposition from the capture position. This is the end of the nominalmating operation.

Item 18: CAPTURE-2 - command moves all four capture latches to catch theincoming passive CBM ring (or to close a cover if there is nomodule in the capture envelope.

Item 21: RESET - a reset command similar to that on a home computer. Itallows a restart if the software sequences lock up.

Item 19: R SAFE - the Contingency Command ‘ITEM 19 EXEC’ which starts asequence of three commands to start the process of CBM supportof the 20 minute separation requirement for a fast getaway of theorbiter should that become necessary. Note: the second commandin this sequence is the CBM_Confirmation_Command. Uponsuccessful completion of this event, a ‘VAL’ appears below item 19prompting the operator to be sure they really want to initiate RapidSafing.

Item 20: SAFVAL - ‘ITEM 20 EXEC’ is the third of three commands that arerequired to start the process of mating the CBM automatically tosupport the shuttle 20 minute sep requirement (the secondcommand is the CBM_Confirmation_Command).

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ITEM ENTRY CHARACTERISTICS: SM 221 CBM CONTROL-2N DISPLAY (Cont)

Items 22: Above item 22 is the field for the Master Stat Code. This four-character telemetry field tells the user the status of the MasterController assigned (i.e., whether a command is in complete, inprogress, pending, aborted, failed, or has timed out.)

MASK - ‘ITEM 21 +X X’, the Mask Bolt commands, are indexed itementries. The XX are integers that are: 11, 12, 13, 14, 15, 21, 22,23, 24, 25, 31, 32, 33, 34, 35, 41, 42, 43, 44, and 45, eachcorrespond to the bolt groups. All other hex entries will result in an‘ILLEGAL ENTRY’ message.

These are grouped in a matrix to mask a single or multiple controllerfailure should that malfunction happen. This is a contingency areaon the display which, when a certain actuator is masked, anasterisk is driven at the appropriate X,Y coordinate of thecontroller/actuator being masked. For example, if an ‘ITEM 21 +2 2EXEC’ is entered, an asterisk is driven adjacent the vertical columnat 2 and under the horizontal column at 2. This command deselectsthe actuator/controller 2-2. There is a group 5 listed there and theseare the latch controller/actuators that can be masked similarly aswith the bolts.

The Ready To Latch (RTL) area below is a discrete feedback field onthe display to provide the RMS operator with a series of alphacharacters ‘O’ for an Open or ‘C’ for a Closed indication for each offour latches. The characters indicate whether the CBM is in thecapture envelope for the latch that corresponds to that specific RTL.Adjacent to each latch is a pair of stand alone status that (left to right)provide insight to a switch short or an open circuit respectively, ineither case if a down arrow is displayed if the event has occurred.

The BITALL A and B commands, Items 23-25, are associatedcommands that show on PCS the last run active bit. Thesecommands would be executed in conjunction with an X displayedon the Built-In-Test pop-up display.

Telemetry parameters are displayed on the right half of the spec.Bolt information is displayed at right adjacent to the bolt location.Under the column labeled BOLT the first group of bolts is: 1-1, 2-1,3-1, and 4-1. These bolt actuation sequences occur together;because these bolts are 90 degrees apart from each other, thisgrouping specifically allows the active and passive CBM segmentsto be drawn together while ensuring that they remain parallel toeach other. Bolt groups 1-2, 2-2, 3-2, and 4-2 follow along with 1-3,2-3, 3-3, and 4-3 followed by 1-4, 2-4, 3-4, and 4-4 descending thecolumn from top to bottom.

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Bolt Command Status, Position, and Loads are to the right of eachbolt. For the command status, each controller can have a particularfour-character field denote if: (1) the command is in progress or hasfailed, (2) binding is detected, (3) interference is detected, (4) misscapture is detected, (5) stripping is detected, (6) there is a noengaged condition, (7) there is a not adjusted condition, (8) amalfunction is detected, (9) a jam is detected, (10) a commandmissed a broadcast, or (11) a command was aborted.

Bolt position is identified to the right of the Command Stat field toshow the progress of bolt rotation for each command issued.

For each of the four capture latches at the bottom right, similarcolumns provide latch insight as with the bolts above. Latchcommand status is similar to the range of four-character fields forthe bolt commands above. Latch angle shows the range of fulllatch extension to the retracted position.

The Capture Switch area is a discrete feedback field on the displayto provide the RMS operator with a series of alpha characters, O forOpen and C for Closed, indication for each of four capture latches.Adjacent to each latch is a pair of stand-alone statuses that provideinsight to a switch short or open circuit, respectively. In either casea down arrow is displayed if the event has occurred.

CBM Control has a nonstandard display implementation. The signfield for four hex parameters overlaps the background slashes,separating the mode and status fields. This deviation fromstandard requirements will be completely invisible to all usersbecause the parameters can never be negative and the plus signwill never be driven.

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1 2 3 4 5 123456789012345678901234567890123456789012345678901 1 XXXX/223/XXX EARLY COMM-2N XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 CL OP 4 N1RS1C RPC 5 1X 2X PTG MODE 5 6 3X 4X MANUAL 22X 6 12 5X 6X AUTO 23X 7 13 7X 8X 8 N1RS2A RPC 5 9X 10X ANT SEL 9 6 11X 12X PORT OMNI 24X10 10 13X 14X STBD OMNI 25X11 11 15X 16X12 PORT ARRAY BEAM X13 ON OFF STBD ARRAY BEAM X14 XMIT 17X 18X15 DECRYPT X 19X BEAM SEL XX16 KEY XXX17 POST XXXX SIG STR XXX18 CPT POST XXXX19 HI LO20 SYS MODE 20X 21X TEMP I/F21 LOCK PORT ANT XXX XXX22 PORTCOM XXX STBD ANT XXX XXX23 CTP FRM XXX PORTCOM XXX XXX24 R-S RJCT XXX CTP XXX2526

Figure 11.- 223 Early Comm - 2N Display.

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PARAMETER CHARACTERISTICS: SM 223 EARLY COMM-2N DISPLAY

CRT NAME MSID UNITS DISPLAY RANGEOPS FUNCTION PAGE V93X0040X ---------------------- XXXXSPEC FUNCTION PAGE V93X0042X ---------------------- XXXDISPLAY FUNCTION PAGE V93X0044X ---------------------- XXXUPLINK ACTIVITY IND V93X5032X ---------------------- ULGPC DRIVER V93X0048X ---------------------- XMET V91W1990C DDD/HH/MM/SS DDD/HH/MM/SSDISPLAY CRT TIME, SM V91W1988C DDD/HH/MM/SS DDD/HH/MM/SSN1RS1C RPC 5 CL P79X0786E ---------------------- ‘∗’ = 1, blank = 0N1RS1C RPC 5 OP P79X0786E ---------------------- blank = 1, ‘∗’ = 0N1RS1C RPC 6 CL P79X0787E ---------------------- ‘∗’ = 1, blank = 0N1RS1C RPC 6 OP P79X0787E ---------------------- blank = 1, ‘∗’ = 0N1RS1C RPC 12 CL P79X0788E ---------------------- ‘∗’ = 1, blank = 0N1RS1C RPC 12 OP P79X0788E ---------------------- blank = 1, ‘∗’ = 0N1RS1C RPC 13 CL P79X0789E ---------------------- ‘∗’ = 1, blank = 0N1RS1C RPC 13 OP P79X0789E ---------------------- blank = 1, ‘∗’ = 0N1RS2A RPC 5 CL P79X0790E ---------------------- ‘∗’ = 1, blank = 0N1RS2A RPC 5 OP P79X0790E ---------------------- blank = 1, ‘∗’ = 0N1RS2A RPC 6 CL P79X0791E ---------------------- ‘∗’ = 1, blank = 0N1RS2A RPC 6 OP P79X0791E ---------------------- blank = 1, ‘∗’ = 0N1RS2A RPC 10 CL P79X0792E ---------------------- ‘∗’ = 1, blank = 0N1RS2A RPC 10 OP P79X0792E ---------------------- blank = 1, ‘∗’ = 0N1RS2A RPC 11 CL P79X0793E ---------------------- ‘∗’ = 1, blank = 0N1RS2A RPC 11 OP P79X0793E ---------------------- blank = 1, ‘∗’ = 0XMIT ON P79X0588E ---------------------- ‘∗’ = 1, blank = 0XMIT OFF P79X0588E ---------------------- blank = 1, ‘∗’ = 0DECRYPT ON P79X0592E ---------------------- ‘∗’ = 1, blank = 0DECRYPT OFF P79X0592E ---------------------- blank = 1, ‘∗’ = 0DECRYPT KEY BIT 0/4/8 P79U0594D/

P79U0327D/P79U0330D

---------------------- 000-FFF

DECRYPT POST P79X0595E ---------------------- FAIL = 1, PASS = 0CPT POST P79X0372E ---------------------- FAIL = 0, PASS = 1SYS MODE HI P79X0589E ---------------------- ‘∗’ = 1, blank = 0SYS MODE LO P79X0589E ---------------------- blank = 1, ‘∗’ = 0FRM LOCK PORTCOM P79X0591E ---------------------- YES = 1, NO = 0FRM LOCK CTP P79X0605E ---------------------- NO = 1, YES = 0R-S RJCT [1] P79X0590E ---------------------- ERR = 1,

NORM = 0PTG MODE MANUAL P79X0596E ---------------------- ‘∗’ = 1, blank = 0PTG MODE AUTO P79X0596E ---------------------- blank = 1, ‘∗’ = 0ANT SEL PORT OMNI P79X0597E ---------------------- ‘∗’ = 1, blank = 0ANT SEL STBD OMNI P79X0597E ---------------------- blank = 1, ‘∗’ = 0

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PARAMETER CHARACTERISTICS: SM 223 EARLY COMM-2N DISPLAY

CRT NAME MSID UNITS DISPLAY RANGEPORT ARRAY BEAM P79X0597E ---------------------- ‘∗’ = 1, blank = 0STBD ARRAY BEAM P79X0597E ---------------------- blank = 1, ‘∗’ = 0BEAM SEL P79U0599D ---------------------- 0 --- 255SIG STR P79U0600A CNT 0 --- 255PORT ANT TEMP P79U0601A CNT 0 --- 255STBD ANT TEMP P79U0602A CNT 0 --- 255PORTCOM TEMP P79U0603A CNT 0 --- 255CTP TEMP P79U0604A CNT 0 --- 255PORT ANT I/F P79X0373E ---------------------- ERR = 1, OK = 0STBD ANT I/F P79X0374E ---------------------- ERR = 1, OK = 0PORTCOM I/F P79X0375E ---------------------- ERR = 1, OK = 0

REMARKS

[1] This parameter displays ‘ERR’ or ‘NORM’ to indicate if forward link packets arebeing discarded due to Reed-Solomon rejects.

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ITEM ENTRY CHARACTERISTICS: SM 223 EARLY COMM-2N DISPLAY

Items 1 --- 16: N1RS1C RPC (5,6,12,13) and N1RS2A RPC (5,6,10,11) - powers on(CL) and powers off (OP) the Remote Power Controllers (RPCs)associated with the Early Communication System. An asterisk willbe displayed next to the appropriate item number to indicate theopen/closed status of each RPC.

Items 17 and 18: XMIT - powers ON and OFF the Early Communication Systemtransmitter, respectively. An asterisk will be displayed next to theappropriate item number to indicate transmitter status.

Item 19: DECRYPT - turns OFF the Decryption function. An asterisk will bedisplayed next to item 19 to indicate that the decryption function isOFF; otherwise, an asterisk will be displayed under the ON column.The KEY field displays the index number of the decryption keycurrently in use. This value is displayed in hex. The POST fielddisplays either ‘PASS’ or ‘FAIL’ to indicate whether or not thedecryption Power On Self-Test (POST) was successful.

The Command/Telemetry Processor (CTP) POST field displayseither ‘PASS’ or ‘FAIL’ to indicate whether or not the CTP POSTwas successful.

Items 20 and 21: SYS MODE - selects either the HI or LO system mode, respectively.An asterisk will be displayed next to the appropriate item entry toindicate the current system mode. HI mode is used for video-teleconferencing and LO mode is used for command/telemetrytransmission.

Items 22 and 23: PTG MODE - allow the crew to select either the MANUAL or AUTOpointing modes, respectively. An asterisk will be displayed next tothe appropriate item entry to indicate the current mode. Normaloperation of the system will be in automatic pointing mode.

Items 24 and 25: ANT SEL - selects either the PORT or STBD OMNI antennarespectively. These commands are used when in Low Data Rateand Manual Pointing Mode only. An asterisk will be displayed nextto the appropriate item entry to indicate the antenna selectedregardless of pointing mode.

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1 2 3 4 5123456789012345678901234567890123456789012345678901 1 XXXX/224/XXX FGB-2N XX X DDD/HH/MM/SS 2 DDD/HH/MM/SS 3 4 VOLTS AMPS 5 MAIN BUS XXXX.X 6 V1 XXX.X 7 V2 XXX.X BC SYNC XXXS 8 SOLAR ARRAY XXX.X FRM CTR XXX 910 RACU 5 INP XXX.X COMMANDING XXX11 OUT XXX.XS XX.XS CMD DIR XXX12 MU RDY CH 1 XXX13 RACU 6 INP XXX.X 2 XXX14 OUT XXX.XS XX.XS 3 XXX15 OCS RDY 1 XXX16 ON OFF 2 XXX17 RACU 5 PWR X X AMP - HRS18 VIA FGB 1 5 BATT VOLTS CHG 1 CHG 219 NCS 2 6 1 XX.X XX.X XX.X20 2 XX.X XX.X XX.X21 RACU 6 PWR X X 3 XX.X XX.X XX.X22 VIA FGB 3 7 4 XX.X XX.X XX.X23 NCS 4 8 5 XX.X XX.X XX.X24 6 XX.X XX.X XX.X2526

Figure 12.- 224 FGB - 2N Display.

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PARAMETER CHARACTERISTICS: SM 224 FGB-2N DISPLAY


STATUSINDICATORS

FDA(Limits)

M H L ↑ ↓ HI LOMAIN BUS AMPS P79C0236A AMP 0 --- 600 N/A N/A

MAIN BUS V1 VOLTS P79V0270A VDC 0 --- 40

MAIN BUS V2 VOLTS P79V0272A VDC 0 --- 40

SOLAR ARRAY AMPS P79C0510A AMP 0 --- 600 N/A N/A

RACU 5 INPUT AMPS P79C0242A AMP 0 --- 35 N/A N/A

RACU 5 OUTPUT VOLTS P79V0274A VDC 0 – 150 ↑ ↓ 130V 118V

RACU 5 OUTPUT AMPS P79C0238A AMP 0 --- 80 ↑ 16A N/A

RACU 6 INPUT AMPS P79C0244A AMP 0 --- 35 N/A N/A

RACU 6 OUTPUT VOLTS P79V0276A VDC 0 --- 150 ↑ ↓ 130V 118V

RACU 6 OUTPUT AMPS P79C0240A AMP 0 --- 80 ↑ 16A N/A

RACU 5 POWER ON P79X0383E --------------- ‘∗’ = 0,blank = 1

--------- ---------

RACU 5 POWER OFF --------------- blank = 0,‘∗’ = 1

--------- ---------

RACU 6 POWER ON P79X0384E --------------- ‘∗’ = 0,blank = 1

--------- ---------

RACU 6 POWER OFF --------------- blank = 0,‘∗’ = 1

--------- ---------

BC SYNC [1] P79X0211E --------------- YES = 0,NO = 1

↓ N/A 1

FRM CTR [2] P79U0116D --------------- INCREMENT --------- ---------COMMANDING [3] P79X0511E --------------- ENA = 1,

INH = 0--------- ---------

CMD DIRECTION [4] P79X0512E --------------- MU = 1,DIO = 0

--------- ---------

MU READY CH 1 P79X0513E --------------- YES = 1,NO = 0

--------- ---------

MU READY CH 2 P79X0514E --------------- YES = 1, --------- ---------

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PARAMETER CHARACTERISTICS: SM 224 FGB-2N DISPLAY


STATUSINDICATORS

FDA(Limits)

M H L ↑ ↓ HI LONO = 0

MU READY CH 3 P79X0515E --------------- YES = 1,NO = 0

--------- ---------

OCS READY 1 P79X0518E --------------- YES = 1,NO = 0

--------- ---------

OCS READY 2 P79X0519E --------------- YES = 1,NO = 0

--------- ---------

BATT 1 VOLTS [5] P79V0278A VDC 0 --- 35BATT 1 CHG 1 [5] P79E0246A AMP-HRS 0 --- 60BATT 1 CHG 2 [5] P79E0248A AMP-HRS 0 --- 60BATT 2 VOLTS [5] P79V0280A VDC 0 --- 35BATT 2 CHG 1 [5] P79E0250A AMP-HRS 0 --- 60BATT 2 CHG 2 [5] P79E0252A AMP-HRS 0 --- 60BATT 3 VOLTS [5] P79V0282A VDC 0 --- 35BATT 3 CHG 1 [5] P79E0254A AMP-HRS 0 --- 60BATT 3 CHG 2 [5] P79E0256A AMP-HRS 0 --- 60BATT 4 VOLTS [5] P79V0284A VDC 0 --- 35BATT 4 CHG 1 [5] P79E0258A AMP-HRS 0 --- 60BATT 4 CHG 2 [5] P79E0260A AMP-HRS 0 --- 60BATT 5 VOLTS [5] P79V0286A VDC 0 --- 35BATT 5 CHG 1 [5] P79E0262A AMP-HRS 0 --- 60BATT 5 CHG 2 [5] P79E0264A AMP-HRS 0 --- 60BATT 6 VOLTS [5] P79V0288A VDC 0 --- 35

BATT 6 CHG 1 [5] P79E0266A AMP-HRS 0 --- 60

BATT 6 CHG 2 [5] P79E0268A AMP-HRS 0 --- 60

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REMARKS

[1] In the BC SYNC field, either ‘YES’ or ‘NO’ will be displayed to indicate whether ornot the FGB MDM is communicating with the bus controller (either the OIU orNode MDM). When the FGB MDM loses sync with the bus controller, this fieldwill read ‘NO’ and the crew will receive an alert light, tone and fault message.

[2] By checking to see if the frame counter (FRM CTR) is incrementing, the crew candetermine whether data is being received from the FGB MDM.

[3] The COMMANDING field indicates whether or not the relay command matrix hasbeen enabled (ENA) or inhibited (INH). The relay command matrix is controlledby the Mission Control Center in Moscow (MCC-M). When this command matrixis enabled, the Mission Control Center in Houston (MCC-H) or the crew cancommand the FGB. This field must read ‘ENA’ before either MCC-H or the crewhas the capability to issue the RACU power ON and OFF commands.

[4] The CDM DIR field indicates the direction of a command sent to a FGB element.This field will read either ‘MU’ to indicate that the command was originated fromthe Matching Unit or ‘DIO’ to indicate that the command was originated from theFGB MDM.

[5] The BATT section displays the voltage and two charge readings for the six FGBbatteries. The BATT CHG parameters measure the state of charge in Amp-hrsof the batteries. The range is 0 to 60 Amp-hrs, 0 being a completely drainedbattery and 60 being a fully charged battery. There are two sensors thatmeasure the charge. The Russians are able to select and deselect the sensorsdepending on their telemetry needs. Therefore, both sets of battery charge datamay not be available.

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ITEM ENTRY CHARACTERISTICS: SM 224 FGB-2N DISPLAY

Items 1 --- 5: RACU 5 PWR VIA FGB ON/OFF - enables the crew to commandRACU 5 power On/Off via the FGB MDM when the OIU is the buscontroller. An asterisk will be displayed under the ON/OFF column.

Items 3 --- 7: RACU 6 PWR VIA FGB ON/OFF - enables the crew to commandRACU 6 power On/Off via the FGB MDM when the OIU is the buscontroller. An asterisk will be displayed under the ON/OFF column.

Items 2 --- 6: RACU 5 PWR VIA NCS ON/OFF - enables the crew to commandRACU 5 power On/Off via Node MDM when the Node MDM is thebus controller. An asterisk will be displayed under the ON/OFFcolumn.

Items 4 --- 8: RACU 6 PWR VIA NCS ON/OFF - enables the crew to commandRACU 6 power On/Off via Node MDM when the Node MDM is thebus controller. An asterisk will be displayed under the ON/OFFcolumn.

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System Message TextALRM CLS

MSID Event DriverAnalog Limit Low

Analog Limit High

Discrete in Alarm Value

Filter

ECLSS 210 ISS C&W FIRE 15 P79X0161E NCS_CW_FIRE_TONE_STATE 1 = Tripped 1ECLSS 210 NODE 1 CAB PRES 15 P79P0493A NODE_1_CAB_PRESS 13.9 15 5ECLSS 206 FGB FIRE - 15 P79X0700E FGB_CW_FIRE_VIA_SM 1 = Tripped 5ECLSS 206 SM DEPRESS - 15 P79X0702E SM_CW_RPD_DEPRESS 1 = Tripped 5ECLSS 206 SM TOX ATM - 15 P79X0703E SM_CW_TOXIC_AIR 1 = Tripped 5ECLSS 206 SM FIRE - 15 P79X0832E SM_FIRE-RS 1 = Tripped 5

C&DH 210 LOAD SHED N1 3 P79X0072E LOAD_SHED_DETECTION_STA BIT 13

0 = Tripped if P79X0066E = 1

and P79X0058E = 1

5C&DH 210 N1SEC SYNC FAIL 3 P79X0112E SEC_NCS_DAP_LOSS_SYNC_STAT 1 = Tripped 5C&DH 210 ISS C&W CAUT 3 P79X0157E NCS_CW_CAUTN_TONE_STATE 1 = Tripped 1C&DH 210 ISS C&W WARN 3 P79X0158E NCS_CW_WARN_TONE_STATE 1 = Tripped 1EPS 0 P79X0163E CBM_ACT_LATCH_1_RTL_SHORT 1 = Tripped 5EPS 0 P79X0164E CBM_ACT_LATCH_1_RTL_OPEN_CIRCUIT 1 = Tripped 5EPS 0 P79X0165E CBM_ACT_LATCH_1_CAPTURE_SWITCH_SHO 1 = Tripped 5EPS 0 P79X0166E CBM_ACT_LATCH_1_CAPTURE_SWITCH_OPE 1 = Tripped 5EPS 0 P79X0172E CBM_ACT_LATCH_2_RTL_SHORT 1 = Tripped 5EPS 0 P79X0173E CBM_ACT_LATCH_2_RTL_OPEN_CIRCUIT 1 = Tripped 5EPS 0 P79X0174E CBM_ACT_LATCH_2_CAPTURE_SWITCH_SHO 1 = Tripped 5EPS 0 P79X0175E CBM_ACT_LATCH_2_CAPTURE_SWITCH_OPE 1 = Tripped 5EPS 0 P79X0181E CBM_ACT_LATCH_3_RTL_SHORT 1 = Tripped 5EPS 0 P79X0182E CBM_ACT_LATCH_3_RTL_OPEN_CIRCUIT 1 = Tripped 5EPS 0 P79X0183E CBM_ACT_LATCH_3_CAPTURE_SWITCH_SHO 1 = Tripped 5EPS 0 P79X0184E CBM_ACT_LATCH_3_CAPTURE_SWITCH_OPE 1 = Tripped 5EPS 0 P79X0190E CBM_ACT_LATCH_4_RTL_SHORT 1 = Tripped 5EPS 0 P79X0191E CBM_ACT_LATCH_4_RTL_OPEN_CIRCUIT 1 = Tripped 5EPS 0 P79X0192E CBM_ACT_LATCH_4_CAPTURE_SWITCH_SHO 1 = Tripped 5EPS 0 P79X0193E CBM_ACT_LATCH_4_CAPTURE_SWITCH_OPE 1 = Tripped 5EPS 204 FGB SYNC FAIL 3 P79X0211E FGB_MDM_LOSS_OF_SYNC 1 = Tripped 5EPS 204 RACU5 AMP LMT 3 P79C0238A FGB_RACU5_IOUT 16 5EPS 204 RACU6 AMP LMT 3 P79C0240A FGB_RACU6_IOUT 16 5

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Filter

EPS 204 RACU5 VOLT LMT 3 P79V0274A FGB_RACU5_VOUT 118 130 5EPS 204 RACU6 VOLT LMT 3 P79V0276A FGB_RACU6_VOUT 118 130 5EPS 210 N1-2 CARD TRIP 3 P79X0298E RPCM_N1RS2_C_RPC_03_N1_2_SDO_CARD_ 1 = Tripped 5EPS 210 N1-2 CARD TRIP 3 P79X0299E RPCM_N1RS2_C_RPC_04_N1_2_SDO_CARD_ 1 = Tripped 5EPS 210 N1-2 CARD TRIP 3 P79X0300E RPCM_N1RS2_C_RPC_13_N1_2_MDM_TRIP_ 1 = Tripped 5EPS 202 CBM ZEN P1 TRIP 3 P79X0422E RPCM_N13B_B_RPC_11_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN P2 TRIP 3 P79X0423E RPCM_N13B_B_RPC_12_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN P3 TRIP 3 P79X0424E RPCM_N13B_B_RPC_13_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN P4 TRIP 3 P79X0425E RPCM_N13B_B_RPC_14_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM FWD P1 TRIP 3 P79X0427E RPCM_N13B_C_RPC_03_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD P2 TRIP 3 P79X0428E RPCM_N13B_C_RPC_04_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD P3 TRIP 3 P79X0429E RPCM_N13B_C_RPC_05_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD P4 TRIP 3 P79X0430E RPCM_N13B_C_RPC_06_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD S1 TRIP 3 P79X0432E RPCM_N14B_A_RPC_02_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD S2 TRIP 3 P79X0433E RPCM_N14B_A_RPC_03_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD S3 TRIP 3 P79X0435E RPCM_N14B_A_RPC_14_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM FWD S4 TRIP 3 P79X0436E RPCM_N14B_A_RPC_15_NODE_1_FWD_CBM_ 1 = Tripped 5EPS 202 CBM ZEN S1 TRIP 3 P79X0438E RPCM_N14B_B_RPC_03_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN S2 TRIP 3 P79X0439E RPCM_N14B_B_RPC_04_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN S3 TRIP 3 P79X0440E RPCM_N14B_B_RPC_05_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM ZEN S4 TRIP 3 P79X0441E RPCM_N14B_B_RPC_06_NODE_1_ZEN_CBM_ 1 = Tripped 5EPS 202 CBM NAD S1 TRIP 3 P79X0443E RPCM_N14B_B_RPC_11_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD S2 TRIP 3 P79X0444E RPCM_N14B_B_RPC_12_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD S3 TRIP 3 P79X0445E RPCM_N14B_B_RPC_13_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD S4 TRIP 3 P79X0446E RPCM_N14B_B_RPC_14_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 210 N1-1 CARD TRIP 3 P79X0450E RPCM_N1RS1_A_RPC_05_N1_1_SDO_CARD_ 1 = Tripped 5EPS 210 N1-1 CARD TRIP 3 P79X0451E RPCM_N1RS1_A_RPC_06_N1_1_SDO_CARD_ 1 = Tripped 5EPS 210 N1-1 MDM TRIP 3 P79X0453E RPCM_N1RS1_A_RPC_11_N1_1_MDM_TRIP_ 1 = Tripped 5EPS 202 CBM POR S1 TRIP 3 P79X0456E RPCM_N1RS1_B_RPC_05_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR S2 TRIP 3 P79X0457E RPCM_N1RS1_B_RPC_06_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR S3 TRIP 3 P79X0459E RPCM_N1RS1_B_RPC_13_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR S4 TRIP 3 P79X0460E RPCM_N1RS1_B_RPC_14_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM STB P1 TRIP 3 P79X0462E RPCM_N1RS2_A_RPC_05_ECOMM_XCVR_TRI 1 = Tripped 5

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Analog Limit High


Filter

EPS 202 CBM STB P2 TRIP 3 P79X0463E RPCM_N1RS2_A_RPC_06_ECOMM_RFPDB_TR 1 = Tripped 5EPS 202 CBM STB P3 TRIP 3 P79X0465E RPCM_N1RS2_A_RPC_10_ECOMM_CTP_TRIP 1 = Tripped 5EPS 202 CBM STB P4 TRIP 3 P79X0466E RPCM_N1RS2_A_RPC_11_ECOMM_RFPDB_TR 1 = Tripped 5EPS 202 CBM POR P1 TRIP 3 P79X0468E RPCM_N1RS2_C_RPC_07_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR P2 TRIP 3 P79X0469E RPCM_N1RS2_C_RPC_08_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR P3 TRIP 3 P79X0471E RPCM_N1RS2_C_RPC_10_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM POR P4 TRIP 3 P79X0472E RPCM_N1RS2_C_RPC_11_NODE_1_PORT_CB 1 = Tripped 5EPS 202 CBM STB S1 TRIP 3 P79X0474E RPCM_N1RS1_C_RPC_05_ECOMM_PORT_ANT 1 = Tripped 5EPS 202 CBM STB S2 TRIP 3 P79X0475E RPCM_N1RS1_C_RPC_06_ECOMM_PORT_ANT 1 = Tripped 5EPS 202 CBM STB S3 TRIP 3 P79X0477E RPCM_N1RS1_C_RPC_12_ECOMM_STBD_ANT 1 = Tripped 5EPS 202 CBM STB S4 TRIP 3 P79X0478E RPCM_N1RS1_C_RPC_13_ECOMM_STBD_ANT 1 = Tripped 5EPS 202 CBM NAD P1 TRIP 3 P79X0520E RPCM_N13B_B_RPC_03_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD P2 TRIP 3 P79X0521E RPCM_N13B_B_RPC_04_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD P3 TRIP 3 P79X0522E RPCM_N13B_B_RPC_05_NODE_1_NAD_CBM_ 1 = Tripped 5EPS 202 CBM NAD P4 TRIP 3 P79X0523E RPCM_N13B_B_RPC_06_NODE_1_NAD_CBM_ 1 = Tripped 5ECLSS 206 FGB SMOKE 3 P79X0704E FGB_CW_SMOKE_VIA_SM 1 = Tripped 5ECLSS 206 SM SMOKE 3 P79X0705E SM_CW_SMOKE 1 = Tripped 5ECLSS 206 SM PRESS HIGH 3 P79X0706E SM_CW_CAB_PRESS_HIGH 1 = Tripped 5ECLSS 206 SM PRESS LOW 3 P79X0707E SM_CW_CAB_PRESS_LOW 1 = Tripped 5ECLSS 206 SM PPO2 HIGH 3 P79X0708E SM_CW_PPO2_HIGH 1 = Tripped 5ECLSS 206 SM PPO2 LOW 3 P79X0709E SM_CW_PPO2_LOW 1 = Tripped 5ECLSS 206 SM PPCO2 HIGH 3 P79X0710E SM_CW_PPCO2_HIGH 1 = Tripped 5ECLSS 206 SMPPH2 HIGH 3 P79X0712E SM_CW_PPH2_HIGH 1 = Tripped 5EPS 206 SM POWER LOW 3 P79X0714E SM_INSUFFICIENT_PWR 1 = Tripped 5C&DH 206 SM LD SHED 3 P79X0715E SM_PWR_GEN_REDUCED 1 = Tripped 5C&DH 206 SM HL1 OPS FAIL 3 P79X0716E SM_CW_EXT_LOOP1_FAIL 1 = Tripped 5C&DH 206 SM CL1 OPS FAIL 3 P79X0717E SM_CW_EXT_LOOP2_FAIL 1 = Tripped 5C&DH 206 SM CL1 REG FAIL 3 P79X0722E SM_CW_EXT_LOOP1_FCV_FAIL 1 = Tripped 5C&DH 206 SM CL2 REG FAIL 3 P79X0723E SM_CW_EXT_LOOP2_FCV_FAIL 1 = Tripped 5C&DH 206 SM CC REDN LOST 3 P79X0733E SM_CW_CC_LOSS_OF_REDUN 1 = Tripped 5C&DH 206 SM TC REDN LOST 3 P79X0734E SM_CW_TC_LOSS_OF_REDUN 1 = Tripped 5EPS 206 SM BUS 3A FAIL 3 P79X0735E SM_CW_BUS_3A_FAULT 1 = Tripped 5EPS 206 SM BUS 3B FAIL 3 P79X0736E SM_CW_BUS_3B_FAULT 1 = Tripped 5

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Analog Limit High


Filter

EPS 206 SM BUS 4A FAIL 3 P79X0737E SM_CW_BUS_4A_FAULT 1 = Tripped 5EPS 206 SM BUS 4B FAIL 3 P79X0738E SM_CW_BUS_4B_FAULT 1 = Tripped 5EPS 206 SM BUS 1A FAIL 3 P79X0739E SM_CW_BUS_1A_FAULT 1 = Tripped 5EPS 206 SM BUS 1B FAIL 3 P79X0740E SM_CW_BUS_1B_FAULT 1 = Tripped 5EPS 206 SM BUS 2A FAIL 3 P79X0741E SM_CW_BUS_2A_FAULT 1 = Tripped 5EPS 206 SM BUS 2A FAIL 3 P79X0742E SM_CW_BUS_2B_FAULT 1 = Tripped 5C&DH 206 SM MU 1 FAIL 3 P79X0743E SM_CW_MU_1_FAULT 1 = Tripped 5C&DH 206 SM MU 2 FAIL 3 P79X0744E SM_CW_MU_2_FAULT 1 = Tripped 5C&DH 206 SM MU 3 FAIL 3 P79X0745E SM_CW_MU_3_FAULT 1 = Tripped 5C&DH 206 SM MU 4 FAIL 3 P79X0746E SM_CW_MU_1_FAULT 1 = Tripped 5C&DH 206 SM MU 5 FAIL 3 P79X0747E SM_CW_MU_2_FAULT 1 = Tripped 5C&DH 206 SM MU 6 FAIL 3 P79X0748E SM_CW_MU_3_FAULT 1 = Tripped 5C&DH 206 FGB MU FAIL 3 P79X0749E FGB_CW_MU_FAULT 1 = Tripped 5C&DH 206 SM GNC FAIL 3 P79X0750E CW_RSMCS_SM_SYSTEM_FAIL 1 = Tripped 5C&DH 206 SM SV DGRD 3 P79X0751E CW_RSMCS_SM_STATE_VECTOR_DEGRADING 1 = Tripped 5C&DH 206 SM CL1SHDN 3 P79X0833E SM_CW_EXT_LOOP1_SW_SHUTDOWN 1 = Tripped 5C&DH 206 SM CL2SHDN 3 P79X0834E SM_CW_EXT_LOOP2_SW_SHUTDOWN 1 = Tripped 5C&DH 221 ZENITH COM ERR 3 P79X0835E CBM_COMM_ERROR_N1_ZEN 1 = Tripped 1C&DH 221 NADIR COM ERR 3 P79X0836E CBM_COMM_ERROR_N1_NAD 1 = Tripped 1C&DH 221 PORT COM ERR 3 P79X0837E CBM_COMM_ERROR_N1_PORT 1 = Tripped 1C&DH 221 FORWRD COM ERR 3 P79X0838E CBM_COMM_ERROR_N1_FWD 1 = Tripped 1INCO 212 OIU TEMP 1 3 P50T4000V OIU POWER SUPPLY TEMPERATURE-PF01 212 0INCO 212 OIU TEMP 1 3 P50T4001V OIU POWER SUPPLY TEMPERATURE-PF02 212 0INCO 212 OIU CONV ERR 1 3 P50X4288E OIU FLOATING POINT CONVERSION ERR 1 = Tripped 0

INCO 212 OIU AD1 NOLK 1 3 P50X4440E OIU ACTIVE DEV 1 SYNC STATUS BIT 01 = Tripped if

P50X4441E = 1 0


P50X4451E = 1 0


P50X4461E = 1 0

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Analog Limit High


Filter


P50X4471E = 1 0

EGIL 200 APCU1 VOLT LMT 3 P50V9000V APCU 1 OUTPUT VOLTS (HIGH RES)

122 130 TMBU

to 126.5 5

EGIL 200 APCU1 TEMP HIGH 3 P50T9002V APCU 1 CONVERTER A TEMP

none TMBU to 20

120 TMBU to 130 5

EGIL 200 APCU1 AMP HIGH 3 P50C9003V APCU 1 CONVERTER A OUTPUT CURRENT

7.5 TMBU to 8.5 5

EGIL 200 APCU1 AMP HIGH 3 P50C9004V APCU 1 CONVERTER B OUTPUT CURRENT

7.5 TMBU to 8.5 5

EGIL 200 APCU1 TEMP HIGH 3 P50T9005V APCU 1 CONVERTER B TEMP

none TMBU to 20

120 TMBU to 130 5

EGIL 200 APCU1 TRIP 3 P50V9006V APCU 1 TRIP STATUS

-4.6 TMBU to -4.4 5

EGIL 200 APCU2 VOLT LMT 3 P50V9008V APCU 2 OUTPUT VOLTS (HIGH RES)

122 130 TMBU

to 126.5 5

EGIL 200 APCU2 AMP HIGH 3 P50C9009V APCU 2 CONVERTER A OUTPUT CURRENT

7.5 TMBU to 8.5 5

EGIL 200 APCU2 TEMP HIGH 3 P50T9010V APCU 2 CONVERTER A TEMP

none TMBU to 20

120 TMBU to 130 5

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Analog Limit High


Filter

EGIL 200 APCU2 AMP HIGH 3 P50C9011V APCU 2 CONVERTER B OUTPUT CURRENT

7.5 TMBU to 8.5 5

EGIL 200 APCU2 TEMP HIGH 3 P50T9012V APCU 2 CONVERTER B TEMP

none TMBU to 20

120 TMBU to 130 5

EGIL 200 APCU2 TRIP 3 P50V9013V APCU 2 TRIP STATUS

-4.6 TMBU to -4.4 5

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International Space Station Assembly Operations … space station assembly operations book - 3a ......

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