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INSTRUMENTATION - Central States Bus Sales, Inc.

1. 110715 F 02 19 09 Page 61 69 14 4 1939 Table of Messages Frame PGN Name Byte TX RX English Source Metric Units Address Engine H ours 65 253 00FEE5 Total engine hours 1 2 3 4 RQ H 0 Component ID 65 259 OOFEEB Component ID Multipacket RQ 0 Cruise Control V ehicle Speed 65 265 OOFEF1 Wheel based vehicle speed 2 3 RX M PH km h 0 Cruise Control V ehicle Speed 65 265 O0FEF 1 Service Brake 4 b6 amp 5 TX 17 Cruise Control V ehicle Speed 65 265 OOFEF 1 Park Brake 10463 TX 17 PTO 65 264 OOFEFO Throttle Interlock CAT 6 b2 amp 1 TX 17 PTO 65 264 Engine PTO Governor 6 b2 amp 1 TX 17 enable switch PTO 65 264 Engine Remote PTO 6 b4 amp 3 TX 17 Governor Programmed Speed Control Switch 1 61 441 00 001 Throttle Interlock 4 b2 amp 1 TX 17 Cummins 1 61 441 00 001 ABS 6 b6 amp 5 RX 0B EBCI 61 441 00 001 ATC 6 b8 amp 7 RX 0B Shutdown 65 252 OOFEE4 Wait to Start 4b 2 amp 1 RX 0 DM1 65 226 OOFECA Active DTC 3 6 RX 0 DM1 65 226 OOFECA Protect lamp 10261 0 DM1 65 226 OOFECA Amber warning lamp 1 b 4 amp 3 RX 0 DM1 65 226 0OFECA Red Stop lamp 1 b6 amp 5 RX 0 Shutdown 65 252 OOFEE4 Idle Shutdown Active SPN 1 b4 amp 3 RX 0 594 EECI 61 444 00F 004 Engine speed 4 5 RX RPM 0 EEC2 61 443 00F 003 Percent load 3 RX
2. Gees 4 1 2 LIN Devices CER RUNE APAE BN OND a A E E A E E E 4 2 1 Display Odometer amp Clock in LCD 422 Hazard warhing lights in t imet rtt o n pe en KEKEE cH EL ede Ee 13 4 2 3 Brake InterlockReguesti s oie ada ose tes i UR RR Ree Fea EEUU CH Ld Leg aed Ey Da EY EOD 13 4 3 START UP MODE s 43 11 Star p up test t 13 rco Luo 14 4 5 SLEEP MODE e 4 6 SELF DIAGNOSTIG MODE M 14 TESEBANELIM ODE DU E UD neces oon eee 15 5 IGNITION MODE E 16 5 1 GAUGE DISPLAY 16 DCCA OMELET sivas Ges sat PE 16 5 1 2 Tachomet t H M 16 SLI Fuel 16 5 1 4 Oil Pressure Gauge Coolant Temperature Gauge RN SE D TU dc E 5 1 6 Rear Air 5 2 Ye quic cM Di 2A GAUGES DEED 18 5 2 2 LCD 5 2 3 IIIA MERERI 18 5 3 WARNING BANK INDICATORS E 19 5 4 LAMP GENERAL DETAIL EU NA TNI NI H ALARM eccL 23 6 1 TONE DEFINITION as
3. 51 11 1 BUZZER TIME OUT ENABLE cccscsssscessssestesescsseseesesstseeseesecasseseeaesaesasseseeseeseseseeseesauseseesensassesecaesaesassesersaeseesanseraeeeeateatsaeans 52 gud G 52 11 3 TURN SIGNAL CLICK ecce neret inr riter Hr sag v x RS aud 52 AMMETERIDISPILA Y RR Ru 52 11 5 IBRAK ESY STEM E 52 J1 6 APPEIED SUSPENSION AIR eed ie ver ate evertere docere d e NU RON NR GRE RA TRA RA NR 52 11 7 BUS CONFIGURATION TY PE i3 iius cic enira roi rds cactus eorr edv 53 11 8 ENGINE CONFIGURATION M4 REM 53 SEU Um 53 TIT JO BATTERY CONTROLLED LIET Eae ac Exc eric perc crac RIVA FRA CN M RN T ERR EE TS 53 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 615 e BLUE BIRD D3 FE SERVICE MANUAL e BLUE BIRD 110715 F 02 19 09 Page 10 69 12 FEATURE PROGRAMM ING eese entente entes tntn tnn 54 12
4. Indicatio Nominal PSI n Empty 260 1 8 665 1 4 1070 3 8 1475 1 2 1880 5 8 2285 3 4 2690 7 8 3095 Full 3500 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden Se 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 59 69 14 2 Air Pressure Sensors 14 2 1 174 PSI Kavlico P2000 5192 Kavlico 0 50 050 L 174 090 69 6 230 Vout 0 10 20 30 40 50 60 70 380 90 100 110 120 130 140 150 160 170 180 190 PSI 665 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 60 69 14 3 Ammeter Type Ammeter Hall Effect Sensor Manufacturer Sure Power Mftr parte DCCS45S 200 pO 1 1580 16 1660 80 1680 i7 17170 66 1880 19 19 40 20790 21 2120 0 2450 25 250 40 2 8710 2 9290 60 3090 3130 326700 3333 90 3360 34 3430 150 39600 4 4040 150 120 90 60 30 0 30 60 90 120 15 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden e 1 BLUE BIRD APPENDIX INSTRUMENTATION
5. Tripl 11939 XXXX X PGN62265 SPN 84 9999 9 EARUM 5 1579F Trans 15zoAM Trip2 J 1939 XXXX X mp2 NRE PGN62265 SPN 84 9999 9 Pp AIr R 150 PSI 150 PSI 1579F 9 2 1 1 Odometer Logic 640 All odometers have a resolution of 0 1 mi km Leading zeros are only displayed in the 1 s position The vehicle distance is calculated every 80 msec and stored within the cluster in kilometers It can be displayed in miles or kilometers The odometer reading will be displayed when the ignition switch is off by activating the headlights or pressing either button on the cluster 9 2 1 2 Odometer A ccuracy A ccuracy of the odometer value is dependant on two 2 main variables 1 The algorithm in the speedometer for calculating distance and 2 the speed value transmitted by the ECM The algorithm has been designed and written to calculate the distance with the accuracy and resolution necessary to exceed SAE recommendations The distance is calculated every 80 msec to reduce error during any rapid speed change the vehicle might make The speed data is dependant on the calibration parameters for tire size and axle ratio being properly entered into the ECM These are the same parameters necessary to have the ECM properly calculate the vehicle speed and distance value Testing has indicated that the algorithm will calculate mileage within 0 07 of actual based on the speed
6. 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 16 69 5 IGNITION MODE 5 1 Gauge Display 5 1 1 SPEEDOMETER J1939 PGN 65265 s ud MPH D426 GMLAN TBD x K mh 0427 Note Scale units M PH K m h scale will be noted though dead front indications on the speedometer 5 1 2 TACHOMETER Stepper i dge M 401 Linear J1939 PGN 61444 187 CW 0 O None None None N A GMLAN TBD 187 5000 RPM 5 1 3 FUEL GAUGE Stepper Alarm NA per dge M 403 Amber FMVSS On if fuel lt 571 101 12 5 Diesel Table 2 pe CL Pin 34 Fuel Level ONG n Gas CL Pin 34 D428 Linear Diesel cw 0 Empty Fuel Y es 5 min Pressure Reoccur 90 Full 0429 On if fuel lt CNG ow Fuel 1 6V dc CL Pin 10 Then off if fuel D429 gt 1 7V dc CNG O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 622 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 17 69 5 1 4 PRESSURE GAUGE Stepper Alarm M 402 Linear 11939 11939 PGN 65263 CCW 20PSI i pmispnioo Continuo es 5 min GMLAN TBD 90 100 PSI GMLAN COOLANT TEMPERATURE GAUGE
7. C PRG 12 2 BYTE 1 12 3 DIAGNOSTIC COMMANDS 13 RELATED STANDARDS TE Sas 55 14 5 T Y 56 RESISTIVE FUEL SENDER 2 dede 14 1 VOLTAGE FUEL SENDER 14 2 AIR PRESSURE SENSORS LEA NL TEILE 14 3 AMMETER rennes 14 4 1939 TABLE OF MESSAGES YS OM AN 14 6 CUSTER CONNECTOR ever tme ence c ea ern nn Na v Rn SCR eu vi 14 7 CLUSTER MATING 14 8 WARNING MODULE BINARY INPUT CONNECTOR 15 APPENDIX Hi 67 15 1 SERVICE SET ODOMETER FEATURE sssssssssssssestesesssseesesstsecsesecsecaesecseseesasseaeseseusesseseesaeseseesavsesasseeersansassesonsesatsesensateatenee 67 15 2 LIMITED FUNCTION 15 3 SETTING THE UNITS 154 SETTING THE ODOMETER BUE occisione n era n na Y n e EY REY SNR ERN KUNA SEA ER RSEN NY EN 68 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 11 69 1 PURPOSE This document is the design specifications for the development of a corporate cluster for Bluebird Bus Co
8. This screen displays the J2012 DTC Display as received from the engine for active faults via 1939 Converted from 1850 GM LAN Active faults shown below as examples L L GM Engine Diagnostics E P0230 Fuel Pump Relay Control Circuit P0315 Crankshaft pos sys var not learned P0354 Ignition Coil 4 control circuit Prev P0641 5v Reference 1 Circuit D Press on both buttons to Exit Next D 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX BLUE BIRD 0 SERVICE MANUAL 02 19 09 Page 50 69 10 11 Trans Diagnostic Item 11 This screen displays J2012 DTC Display as received from the transmission for active faults via 1939 Active faults shown below as examples Transmission type and number of active DTC sis located in upper right corner Press both buttons to exit to previous screen Transmission Diagnostics Allison P0218 TBO P0733 P1482 Prev Press on both buttons to Exit Next D 10 12 ABS Diagnostic Item 12 A BS Diagnostics This screen displays the Suspect Parameter Number SPN and Failure mode Identifier as received from the ABS for active faults via 1939 Two active faults shown below as an example Brake system type and number of active DTC s is located in upper right corner Press both buttons to exit to previous screen ABS Diagnostics 254 12 Main controler saftey controler 656 100 06 Pw
9. intervals Data Link Historical List of NR Missin M essage Flashing None Warning connected devices 9999999 9 16 9V 155A des ce hak to As Shown Data Link Warning 112 55 Was present video at msec intervals Vehicle 11939 N R j1939data Message Flashing Beep 1 Speed Error PGN65265 SPN 84 9999999 9 16 9 155A either N A ann to i As Shown Vehicle Speed 15 55 nq or in reverse video at GMLAN TBD Error error data 500msec range intervals EngineDoor CL_Pin 28 NR M essage Flashing Continuous Ds 9999999 9 16 9V 155A to j Until Fault As Shown ngine Door Active Low reverse video at is gone Open pem 500msec intervals Brake N R 8 Interlock See Section 9 4 2 1 bel See Section 9999999 9 16 9V 155A SeeSection SeeSection 9 4 2 1 SeeSection 9 5 4 2 DEIOW 9 4 2 1 below Brake Interlock 42 55AM 9 4 2 1 below below 9 4 2 1 below Retarder 11939 ing None essage Flashing A pplied PGN61440 SPN 1667 9999999 9 N R 8 forward to As Shown 189V 155A Value 201 reverse video at GMLAN TBD Retarder Applied 12 55AM 500msec intervals 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX e 646 e BLUE BIRD SFE SERVICE MANUAL 110715 F 02 19 09 Page 40
10. Stepper Warning WL Alarm M 405 11939 PGN 65262 cw 0 He R J1939 PGN65262 Continuo Y es 5 min GMLAN E GMLAN Reoccur 90 260 F 5 1 5 FRONT AIR GAUGE Stepper Warning WL Alarm M 407 CL Pin 11 lt 65 PSI Continuo E Then off when2 us1 90 150 PSI 72 PSI 5 1 6 REAR AIR GAUGE Stepper Warning Alarm CL Pin 12 0 2098 lt 65 PSI Continuo Th ff when gt 90 150 PSI 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 18 69 5 2 Backlighting The gauge backlighting will be turned on when the backlight CL Pin 19 input is active Dimming of the backlight is done using an internal dimmer which is controlled using the buttons on the cluster If the park brake is setthe dimmer can be accessed through the diagnostic menu If the park brake is not set and the Headlight input is active then the up an down buttons will automatically become the dimmer adjustment In this state if Trip or Odometer access or access to any other quadrant is needed both buttons must be pressed and they will temporarily return to normal operation Once adjusted the setting is stored inthe EEPROM 5 2 1 GAUGES The gauge backlight can be selected by the end user The selected color is controlled through the
11. 0 Engine Fluid evel Pressure 65 263 00FEEF Engine oil pressure 4 RX PSI KPa 0 Engine Temperature 65 262 00FEEE Engine coolant temp 1 RX kd 0 ERC1 61 440 00F 000 Retarder 4 b4 amp 3 RX OF or 10 1 61 442 00 002 Electronic Trans Controller N A RX 3 ETC7 65 098 OOFE4A Shift inhibit 2 b8 amp 7 RX 3 Fuel Economy 65 266 OOF EF 2 Instantaneous fuel econ 3 4 RX MPG 0 L 100K m Fuel Economy 65 266 OOFEF2 Average fuel economy 5 6 RX MPG 0 L 100K m Inlet Exhaust Conditions 65 270 OOFEF6 Boost pressure 2 RX PSI KPa 0 Inlet Exhaust Conditions 65 270 OOFEF6 Intake manifold temperature 3 RX oF 0 Transmission Fluids 65 272 OOFEF8 Transmission oil temp 5 6 RX oF C 3 ETC2 61 445 00F 005 Transmission Current G ear 4 RX 3 7Dh neutral lt 7Ch reverse 7Eh though 84h drive Vehicle Electrical Power 65 271 OOFEF7 Electrical potential volts 56 RX V 0 Vehicle Electrical Power 65 271 OOFEF7 Battery potential volts 7 8 RX V 0 Switched Dash Display 65 276 OOFEFC Fuel Level 2 RX 96 0 WFI 65 279 OOFEFF Water in fuel 10261 0 1 64 892 00 07 Particulate Trap Lamp 1b1 3 RX 0 Command 1 64 892 00 07 Exhaust System High Temp 7b3 5 RX 0 Cruise Control V ehicle Speed 65 265 Cruise Control State 7B 8 7 6 RX 0 OOFEF1 SPN 527 Defined Faults PGN Name Byte SPN FMI Source Address DM1 65 226 OOFECA High Coolant Temp 3 6 110 0 11 and 16 0 DM1 65 226 OOFECA Low Oi
12. 4 Per previous documentation received from BB on how the engine should react to PTC messages updated Stop engine and Engine Warning lamps to work with the DPF message Section 9 4 2 1 1 added Scenario numbers to each row of the Brake Interlock display table for clarity Section 12 2 A located another bit to the Engine Type config setting to allow for future unknown CAT or Cummins Engines to register with Engine ID message 9 5 08 1939 Table changed the SA for retarder message to OF 10 and 29 based on engine and transmission specifications Section 11 3 Removed the requirement for Beep 2 to sound for turn signal If turn signal click config is disabled Section 7 1 Reconstructed Speed Detect output flow chart and added notes for clarity corrected Ignition on decision outcome 9 8 08 Section 7 3 Reconstructed L ift A uthorization output flow chart and added notes for clarity Section 8 6 2 Slightly modified the verbiage in Throttle interlock message 6 12 description logic to clarify that itis sent during L ift A uthorization output active 10 14 08 A dded comment about fuel gauge initial position in section 4 3 C SMyers 10 27 08 110940v01 17 Section 11 amp 12 added detail to make certain configurable feature only accessible by diagnostic tool after 25 mi Per Jim Halpin Section 11 7 A dded function to the Bus Type Config to invert the Park Brake and Fast Idle binary input logic for BBCV per Jim Halpin Added PIN 36
13. 9 4 2 Changed WIF alarm to be acknowledgeable Section 9 4 2 Removed the ignition of portion of the headlight reminder logic per John Williams also added the 2 min duration as this is how it currently works Section 9 4 2 Changed duration of alarm for ATC DPF and High exhaust temp to 5 sec per John Williams 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 611 e BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 6 69 Section 9 4 2 Change alarm for Range Inhibit Trans oil life filter and service to NONE per John Williams Section 9 4 2 1 changed alarm durations for several of the alarms per John Williams 7 30 08 Section 12 2 2 Corrected Engine Type bit values and descriptions to match software 8 15 08 Removed Hydraulic designation from D404 and added comment to trigger to only use this if configured as English Added D405 for Metric brake fail function Corrected Air gauge warning lamps to text instead of symbol All of which to satisfy the changes made to the dial per J ohn Williams 8 25 08 Section 9 4 2 1 A dded note that brake interlock is NOT acknowledgeable per J ohn Williams Section 6 1 A dded details of general acknowledgement and reoccurrence of alarms per John Williams 9 4 08 Section 5
14. 9 RE forward to GMLAN TBD As Shown Value 01 reverse video at Fk Range Inhibit 12 55AM 500msec intervals Trans Oil J 1939 DM1SA 03 SPN Symbol flashing None Life GMLAN TBD 9999999 9 RE 4177 FMI forward to 7 As Shown Transmission 17 reverse video at 648 Oil Life 12 55AM 500msec intervals Trans Oil 11939 DM1SA 03 SPN Symbol flashing None Filter GMLAN TBD 9999999 9 RE 3359 forward to E As Shown Transmission 7 31 reverse video at AM oil Filter 12 55AM 500msec intervals Trans Oil 11939 DM1SA 03 SPN Symbol flashing None Service 9999999 9 RE 4178 FMI forward to As Shown Transmission 31 reverse video at Oil Service 12 55AM 500msec intervals 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden e 1 BLUE BIRD APPENDIX 9 4 2 1 Brake Interlock Display M essage Detail 110715 F INSTRUMENTATION 02 19 09 Page 43 69 The brake interlock Priority Interrupt Display message will function per logic below This message is NOT acknowledgeable Air Brakes Systems w Brake interlock 40051 02 Scenario Vehicle Brake Brake Brake Cluster Behavior Speed Interlock Interlock Interlock Alarm Request Set Input Input CL Input CL CL PIN 35 PIN 27 PIN 26 1 lt 3MPH N A ACTIVE ACTIVE PIM BRAKE INTERLOCK SET ALARM NONE 2 lt 3MPH N A ACTIVE INACTIVE PIM BRAKE IN
15. ACTIA is forbidden 1 BLUE BIRD APPENDIX 0 INSTRUMENTATION 110715 F 02 19 09 14 7 Cluster Mating Connectors 16 positions 2 X 8 Actia P N 102130 Tyco US Part Number 175966 2 20 positions 2 X 10 Actia P N 102131 Tyco US Part Number 175967 2 1 4 14 8 Warning Module Binary Input connector 8 positions 2 X 4 ActiaP N 100950 Tyco US Part Number 1411001 1 LIN ID 20x92 Terminal Designation Description 1 Spare Binary Input Active low 2 Spare Binary Input Active low 3 Spare Binary Input Active low 4 Spare Binary Input Active low 5 Spare Binary Input Active low 6 j TestPanel w Air System Binary Input Active low 7 Test Panel w A pplied A ir Binary Input Active low 8 Spare Binary Input Active low Signal low Chassis Ground 0 0V 1 5V Signal high 4 0V up to Ignition V oltage Page 65 69 671 so 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 66 69 14 9 1850 Gateway Module Tyco GET64 series sealed connector 8 positions 2 X 4 Actia P N 100950 Tyco US Part Number 1411001 1 Terminal Designation Description Battery Unswitched positive Ground Chassis ground SAE J 1939 Data bus Switched Battery Ignition input
16. Alarm Format Logic Display Notes Duration Trans Temp 1939 PGN65272 SPN 177 XXX X 9999999 9 NRB MLAN TBD Trans 1579F Trans 12 55AM Intake 1939 XXX X Not M anifold PGN65270 SPN 105 IMT NR available Mai 9999999 9 availab GMLAN TBD 150 12 55AM 1850 Engine 11939 PGN65253 Hrs Hourmeter SPN 247 9999999 9 eRe GMLAN 8977 4 Hrs 12 55AM Boost J 1939 XXXX Not Pressure PGN65270 SPN102 Boost 9999999 9 AR available for GM MLAN TBD 5PSI Boost 12 55AM 1850 Instantaneo J 1939 XXXX NRD Not us Fuel PGN65266 SPN 184 XXX Inst 9999999 9 available Econ 12 5MPG Inst 12 55 for GM GMLAN TBD 1850 Average See section 9 4 11 XXXX Not NR Fuel Econ XXX Avg 9999999 9 URB ne GMLAN TED 12 5MPG Avg 12 55 1850 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 643 BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 38 69 9 4 1 1 Average Fuel Consumption Detail Total Distance TD This is an independent trip odometer dedicated to A verage Fuel Consumption calculations and will not be displayed This distance is calculated using the wheel based vehicle speed CCV S in K mh multiplied by the time traveled For the trip distance it simply logs this distance from the time of A verage Fuel Consumption reset to the current time giving you
17. Level 1500 WB2 GkiILkReq HIGH WB 6 Tet W Air HIGH CL 35 Spare WA W683 Lift DrOpen HIGH Prev 7 Tet WApp Air HIGH Prev CL 36 Spare WB MIL HIGH WE 8 Spare NIA Press on both buttons to Exit Next D Press on both buttons to Exit Next D 654 Note The value high and low refers to the voltage level at the connector pin for binary inputs Warning bank information will only be shown if warning bank is detected on the LIN data bus This information will be continuously updated to assist in troubleshooting 10 7 5 STATUS Item E Exits from this menu to the previous screen 10 8 Data Link Item 8 The LIN will be checked and each device found on that data bus would be displayed If the device is saved automatically in this list and is disconnected from the system a warning will be displayed Y ou can delete the device from this list to avoid this warning by scrolling to the device in the list and pressing both buttons Once removed the cluster will not display a warning unless the device is reconnected and auto saved back to the list Press the Exit button to exit to the previous screen DATA LINK LIN ID 92 Optional Input Mod LIN ID Frt Applied Air Ga Press both buttons to Delete Exit D 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 10 9 Read Parameters I
18. Link 11 Trans Diag Prev 3 Contrast 6 Set Clock 9 Read Parameters 12 ABS Dia D Press on both buttons to select Next D Press on both buttons to select Next D The item highlighted in will be selected when both of the buttons are pressed together Pressing either button separately will move the highlight through the list as indicated by the arrow so other items can be selected This menu will auto exit to the drive screen after 10 sec timeout with no activity 10 1 Air Brake PSI Selecting menu item 1 brings up the following screen that is used to perform Pre trip Brake Inspections It will show Front and Rear brake system PSI Pressing the down button will exit to the previous screen FRONT AIR REAR AIR 72 1 PSI 72 5 PSI oggle O E Exit amp 10 2 Set Units Selecting menu item 2 brings up the following screen that is used to select if values are to be displayed in Metric units or English units This will change the Speedo reading and units lamp display menu items except Air which will always be displayed as PSI and change which brake System fail lamp is used Pressing the down button will exit to the previous screen UNITS ENGLISH pe amp Exit amp 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 46 69 10 3 Contrast Selecting menu item 3 displays a scree
19. RearAir Pressure Sender S VAI 0 5 4 5V Software Configurable VAI 0 7V 13 C25105 Applied Front A ir Pressure Sender S VAI 0 5 4 5V Software Configurable VAI 0 7V 670 14 C25106 Applied Rear Air Pressure Sender S VAI 0 5 4 5V Software Configurable VAI 0 7V 15 C25107 Ammeter 5 VAI 1 4 Software Configurable VAI 0 7V 16 C25108 Spare VAI 0 18V Software Configurable VAI 0 18V LT C25109 Hydraulic BrakeFailure S BIN AL Software Configurable RAI 18 C25110 Ignition 5 Binary Input Active High C25111 Brake Interlock Alarm BIN AL Software Configurable RAI 28 C25112 Rear Engine Door 5 BIN AL Software Configurable RAI 29 C25113 LiftAuthorize BINOUT 1 Active Low 1A max current draw Sink 30 C25114 Shutter Solenoid BINOUT 2 Active Low 1A max current draw Sink 31 C25115 Speed Detect Out BINOUT 3 Active Low 1A max current draw Sink 32 C25116 Seat Belt S BIN AL Software Configurable RAI FREQ 33 C25117 LiftDoorO pen Not stowed S BIN AL Software Configurable RAVFREQ 34 C25118 Fuel Level Sender Binary Input Active Low RAI 0 400 Ohms See Chart 35 C25119 Brake Interlock Set A IR Lock Hyd Binary Input Active Low RAI 0 400 Ohms 36 C25120 Waitto Start Binary Input Active Low RAI 0 400 Ohms Signal low Chassis Ground 0 0V 1 5V Signal high 4 0V up to Ignition V oltage 2009 Any reproduction of this document whether total or partial without the written consent of
20. SPN 97 A Wal 16 9 1554 forward to Acknowledg As Shown ater Value 01 video at In Fuel 12 55AM 500msec intervals Headlight CL Pin 19 9999999 9 19 Iignitionis Symbol flashing Beep 1 for 2 Alert 18 9 155 OFF and forward to min AsShown Z D Headlights On 12 55AM Headlights reverse video at input is 500msec Active intervals O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 647 e BLUE BIRD 3 FE SERVICE MANUAL 110715 F 02 19 09 Page 42 69 Function Data Source Text Display Example Trigger Alarm Format Logic Display Notes Duration ATC J 1939 PGN61441 SPN N R Symbol flashin Beep 1 for 5 1793 9999999 9 169v 155A to Sec f GMLAN TBD AsShown TC ATC Active 12 55AM Value 01 G e intervals DPF J 1939 N R 8 Symbol flashing Beep 1 for 5 PGN 64892_SPN 3697 9999999 9 16 9 155A 000 OFF fiat to f sec i As Shown 2 Regen 001 EON reverse video at 5 Needed 12 55AM 100 Fast SO0msec blink intervals Hi Exhaust J1939 N R 8 Symbol flashing Beep 1 for 5 Temp PGN 64892_SPN 3698 9999999 9 16 9 155A aN aa to Sec i High Exhaust E i See enn Temperature 12 55AM 100 i Fast Dm at Blink intervals Range Inhibit 1939 Symbol flashing None PGN65098 SPN 1851 9999999
21. Setting and diagnostics menu using the buttons on the cluster Once adjusted the setting is stored in the EEPROM Colors R G B 624 Blue 0 0 100 Light Blue 0 47 100 White 62 100 91 Red 100 0 0 Green 0 100 0 5 2 2 LCD TheLCD backlight is not selectable by the end user Color W hite 5 2 3 POINTER The pointer backlight is not selectable by the end user Color Amber 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX 110715 F 5 3 Warning Bank Indicators 5 4 Lamp General Detail INSTRUMENTATION 02 19 09 Page 19 69 The lamps detailed below are either indicator lights activated to show the engagement of some chassis function or warning lights to show a fault in a particular chassis function Some warning lights have an alarm associated with them This alarm will be one of several preset Speaker profiles See alarm section for profile details Alarm and duration are referenced for each lamp If no duration is listed the alarm will continue until the fault is gone Some warnings have an associated LCD Warning message that will be displayed along with the warning light See the message display section for specifics on those messages All warnings with associated alarms display messages can be acknowledged If acknowledges the warning by pressing the op b
22. as described in section 7 of this document or go back to sleep 4 3 Start Up Mode Cl The ignition binary input is used to sense if the key switch is on or off The cluster enters start up mode when the ignition is on If the start up self test option is enabled the system will go through the functional diagnostic tests described in the start up self test option section If the self test option is disabled the gauges should drive to zero with the exception of fuel which remains at its last commanded position then default to actual values received by data buss messages senders at startup All warning lights will perform lamp check by turning on for 5 seconds and then go out After lamp check active warning lights will turn The cluster will determine which data buses are connected and which devices are present Error messages will display if a data bus is missing or a device that had been previously found is now missing If the data bus should fail a communications error should be displayed on the LCD and the gauges will wag to flag the communication failure 4 3 1 START UP UP SELF TEST OPTION The start up self test is an option enabled through the setup menu The factory setting for this option is enabled 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 14 69 4 3 1 1 Gauges Gauge po
23. received This far exceeds the SAE recommended 0 3 found in SAE J 1226 9 2 1 3 Normal Shutdown The odometer value is stored to the EEPROM at each 1 kilometer increment 0 62 mi and when the ignition switch is turned off The value is stored to 1 100 of a kilometer resolution 33 ft using a 4 byte memory location within an array Each store is made sequentially to one 1 of eight 8 locations in the array so at any point in time the last eight 8 values are maintained Each value stored is verified at the time it is saved Multiple store attempts to a location will be made if necessary and if not successful the memory location will be tagged as bad The precount that is used to increment the odometer every 1 100th km is also saved The precount value is 115200 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 35 69 Therefore our internal resolution is 1 11520000th of km or 0 003385827 inches This valueis stored on power down and recovered on power up 9 2 1 4 Abnormal shutdown If there is battery power loss at the speedometer prior to turning the ignition off an abnormal shut down will occur The odometer value when power is restored will return to the last kilometer increment value saved i e the last XX X 0 kilometer rollover Therefore the maximum distance lost by an abnormal shutd
24. responses expected will be as follows 633 ASCII ISB ISC ISLG 1 2 3 M M M 4 N N N 5 S S S 6 7 6 6 6 8 B C L 9 10 u U 11 0 0 0 12 7 7 7 13 D D G 14 0 0 0 15 6 8 8 16 7 3 9 17 18 19 O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 28 69 Engine Caterpillar ID Byte ASCII CAT C7 CAT C9 1 C 2 T 3 R R 4 P P 5 L L 6 7 8 9 7 9 10 11 12 13 14 15 16 17 18 19 634 Engine GM 8 1L 1850 ASCII ISB 1 G 2 Y 3 X 4 last digit 1 X 5 last digit 1 6 7 8 GM 8 1L LTG propane engine will communicate on 1850 and for this application the Gateway module will be used so if the Gateway is present on the 1939 data bus the cluster will assume the GM propane engine is used See 111702 specification for general Gateway message support details O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION e 110715 F 02 19 09 Page 29 69 ASCII 2000 2500 3000 1 A A A 2 L
25. same frequency as B eep 2 per John Williams Section 8 6 Removed water in fuel from messages sent per J ohn Williams Section 9 4 2 corrected brake interlock display function reference to reference the correct table in section 9 4 2 1 Section 9 4 2 Changed retarder applied audible alarm to NONE per John Williams Section 10 6 4 dded reference only comment to screen shots for 1 0 status 18 S M yers 7 10 08 Section 9 4 2 Updated headlight alert logic to closer match function per M ichel s notes Section 6 1 Updated tone definition to change beep to freq and both beep 1 and beep 2 repetition to 2Hz per M ichel s notes on how the software actually works and to closer match A3 S M yers 7 10 08 All changes for this rev are additions original project requirements Section 1 A dded FM V SS CM V SS 101 requirement per John Williams Section 4 A dded Brake interlock request limited mode note per J ohn Williams Section 5 4 Removed triggers and alarms for High Hydraulic Oil temp as it is no longer required per J ohn Williams Section 5 4 Changed Hydraulic Brake Failure international icon to text BRAKE PRESSURE per John Williams was originally specified to be BRAKE SYSTEM but was inadvertently changed to the international symbol after rev 2 of the spec Some time after this was implemented in Alpha it was requested that the symbol be moved down and its place be
26. taken by text BRAKE PRESSURE so that both were available on one dial Section 7 1 M odified Speed Detect output logic per John Williams Added the Brake interlock request and Battery Controlled Lift Config requirements Added section 11 10 for this new config Section 12 2 A dded byte for the above mentioned Battery Controlled Lift Config Section 7 3 A dded Brake Interlock request input and Battery Control L ift Config to Lift A uthorize logic per John Williams Section 8 6 2 1 M odified Brake interlock logic per John Williams Changed PIN 25 from spare to brake interlock alarm BIN AL per John Williams 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 5 69 Changed PIN 36 to brake interlock request BIN AL per John Williams This will be a wakeup Added section 4 2 3 to describe limited mode for Brake interlock request wakeup per John Williams Changed PIN 27 from Alternator to Spare per John Williams Changed PIN 33 from Spare to Lift door not open per J ohn Williams Changed PIN 35 to Brake Interlock Set locked per J ohn Williams Section 8 6 1 Added brake interlock request to service brake message sent trigger per John Williams Section 9 4 2 Changed Alterna
27. their end 110764 Dial face without A ir Gauges If spec change effects graphics updated art must be supplied to the Customer for approval and documentation on their end O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD BLUE BIRD SERVICE MANUAL 02 19 09 Page 12 69 4 MODES OF OPERATION left or right turn headlight button press or Brake Interlock Request if configured and not ignition Limited Mode Sleeping Mode left or right turn headlight button press or Brake Interlock R equest if configured and not ignition Ignition Diagnostic Start up Ignition Diagnost Start up Mode 4 1 Sleep Mode If battery power is applied to the system with no other activity it will bein sleep mode When the System is in Sleep M ode the microprocessor is stopped 4 1 1 POWER SUPPLY The system exits Sleep M ode when one of the wake up inputs becomes active When the cluster wakes up it first begins to control the power supply by activating the power supply maintain output Itthen decides depending on which wake up input is active what mode must be entered When the system goes back to sleep after the deactivation of the wakeup input it simply deactivates the power supply maintain output 4 1 2 LIN DEVICES All LIN devices will remain awake for 10s after loss of wakeup The mast
28. whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 57 69 Resistive Fuel Sender Type Resistive Fuel Sender Mftr part Indication Minimum Nominal Maximum Empysop 0 J 0 Empty 3 6 9 053 Fu 87 2 53 87 663 Empty Empty 1 8 1 4 3 8 1 2 5 8 3 4 7 8 Full Stop N ote If the sender is over 180 ohms the system will assume that it is a out of tolerance sender and the fuel level gauge will display a fault by wagging O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 58 69 14 1 Voltage Fuel Sender Voutput PSI 4 3600 1 Type Pressure Transducer Manufacturer Energy Kinetic Mfg part EK 110 1S 36C 0 3600PS 21 5V Energy Kinetic Pressure Sender Voltage 400 1498 1444 3708 1900 3171 3111 1 925 3400 4810 4778 0 674 700 1 769 1 778 0 49496 2200 3 481 3 444 1 06196 80 1896 1889 0 376 2300 3605 3556 1391 J 9 2056 2000 2800 2400 3725 3667 159 J 1000 2159 2111 2 268 2500 3815 3778 0 985 4 596 error 162 psi for a 3600 psi transducer 664
29. 2 6 09 110940v01 21 Section 8 2 A dded final gateway spec info as well as more definition for device ID 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 7 69 messages Section 11 8 A dded notes to clarify what changes with GM 1850 config Section 9 4 1 Added display info to show which Parameters were not available when configured for GM 1850 Section 9 4 A dded note that Quad 3 defaults back to Trans Temp on ignition cycle This is not a software change but additional info for the spec and confirmed by J ohn Williams 613 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD e BLUE BIRD 3 FE SERVICE MANUAL 110715 F 02 19 09 Page 8 69 Table of Content 1 QU dup 11 2 QUUM 11 3 RELA TED 11 4 MODES H 12 AA hzfo ze 2 TP OWOT SUP DIY EET
30. 69 Function Data Source Text Display Example Trigger Display Notes Alarm Format Logic Duration Alternator Internal Logic RPM gt 400 Symbol flashing Continuous Fail N R E forward to Until As Shown 9999999 9 169v 155A and VBAT reverse video at Acknowledg 12V for Alternator 45 55AM 30 500msec ed Failure intervals Stop Engine 1939 DM1 SA 00 Red Stop Symbol flashing Continuous NR Lam forward to Until Fault GMLAN TBD As Shown 9999999 9 155A i reverse video at is gone Stop Engine 12 55AM R Low Coolant 1939 DM 1 SA 00 9999999 9 NR SPN Symbol flashing Continuous Level 169V 155 111 1 forward to Until GMLAN TBD As Shown Low Coolant 5 55 nq 11 or 18 reverse video at Acknowledg Level 500msec ed intervals Hi Trans 1939 DM1SA 03 9999999 9 NR SPN Symbol flashing Continuous Temp V d869V 155A 177 15 forward to Until GMLAN TBD As Shown 1x M 2 55AM reverse video at Acknowledg 500msec ed intervals Low Oil 1939 DM1 SA 00 9999999 9 SPN Symbol flashing Continuous Pressure GMLAN TBD 2 IB9V 195 100 EMI forward to Until As Shown ur Low Oil 2 55AM 110r 18 reverse video at Acknowledg Pressure 500msec ed intervals Hi Engine 1939 DM 15A 00 9999999 9 NR SPN Symbol flashing Continuous Temp M Hd69V 155A 110 FMI 0 forward to Until GMLAN TBD As Shown High Engine 2 55AM 1 or 16 reverse video at Acknowledg x 500msec e
31. 850 and GM LAN references from Allison transmission in section 2 Section 6 6 Corrected pin references and clarified message broadcast and trigger information for all sent messages Corrected all section referencing pin 25 as service brake to be pin 24 Removed duplicate info on Lift Authorization logic flow chart that referenced sent messages Updated Dial face backlight color descrip with color percentages based on WCC application Section 8 Changed Backlight setting feature to DIM MER and added a backlight color selection feature N eed new screen shot U pdated all pin out references to match table 7 S Myers 4 1 08 U pdated lift authorize flow chart for clarification Updated missing suspension air pin info as it is the same as front air but only in hydraulic busses A dded description to backlight section for clarity M oved brake interlock logic flow chart and modified for clarity 8 S Myers 4 2 08 Modified section 9 to change the way brake system and its option setting are configured Updated section 8 7 5 and 8 7 6 to match the new brake system config and option settings 9 P 4 11 08 Sections 7 1 1 7 1 5 changed all screen shots to reflect change in quadrant 2 English Ammeter if available will now be displayed on line with voltage current gear will now always have its own line and depending on active options quad 2 will adjust from 2 to 3 lines as appropriate 10 SMyers 5 12 08 Finished updating all screen shots for display config
32. AL to Wait to start for BBD3 and BBCV perJim Halpin 11 10 08 Section 5 4 Split D406 Park Brake lamp to double as Brake Fail when configured asMetric Spec only change for clarification software is correct D SMyers 12 11 08 110940v01 18 Added Section 9 4 1 1 to describe calculation and display of the Average Fuel Consumption resettable trip This was to give BB a resettable trip average fuel per J ohn Williams Section 10 6 Changed clock set menu timeout from 5 sec to 15 sec per John Williams Section 5 2 Changed how the dimmer adjustment works Per John W illiams Section 5 4 A dded SPN 65000 as a trigger for ENGINE WARN lamp for Gateway support Section 8 6 1 removed brake interlock request as a requirement for the service brake message to be sent per J ohn Williams 12 16 08 Section 11 11 A dded a configuration to the Config menu to Enable or Disable the seatbelt logic This includes auto detect feature to enable the logic if input becomes active Used Byte 1 bit 7 of config bytes 12 17 08 Section 5 1 1 Swapped M PH and KMH LED designations for dial face art change Software needs updated as well E SMyers 1 9 09 110940v01 18 Section 5 4 Park brake lamp alarm logic changed to shut off after 2 min to match current A3 gauge logic This is a document only change and confirmed by John Williams 1 20 09 Section 9 4 2 Added 30 sec delay to Alternator Fail and Low Voltage Error triggers per John Williams F S Myers
33. Brake interlock req Transmit Throttle Interlock See 6 4 2 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 32 69 8 6 3 PARK BRAKE Input Data Message Trigger Message Sent i BIN AL J 1939 PGN65265 SPN 70 01 8 6 4 FAST IDLE Input Data Message Trigger Message Sent If this input is active AND J 1939 CAT PGN65264_SPN 980 01 Brakeis se AND in Neutral 1939 CAT PGN65264 SPN 979 01 Geer J 1939 CMNS PGN65264 SPN 979 01 GMLAN TBD 638 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden e 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 33 69 9 MESSAGE DISPLAY CENTER 9 1 Drive Mode Screen During normal operation the LCD displays in 4 quadrants The user can activate and navigate between quadrant 3 amp 4 by pressing and release the Jower button to highlight quadrant 3 and then press and release both buttons to select quadrant 4 Quadrant 1 is controlled only by the4 upper button and quadrant 2 has no user configuration so it cannot be selected To toggle though the available selections for the active quadrant press the upper or lower button to toggle up or down respectively Below are examples of the possible drive mode screen configurations
34. D 8 5 GMLAN Communication Errors If a parameter is not received by GMLAN for seconds it will be flagged as missing Missing LCD information will display a and missing gauge information will be signaled by wagging the pointer from dial end to dial end A missing GMLAN data bus will be announced in the LCD If aLIN parameter is missing for 5 seconds the gauge will wag the pointer from dial end to dial end and flash the warning LED 8 6 Messages Sent 8 6 1 SERVICE BRAKE Input Data Message Sent 1939 65265 597 01 Pin 24 BIN AH GMLAN TBD See Lift A uthorize If trigger above is NOT active or lift 1939 PGN65265 SPN 597 00 Logic authorize conditions are met GMLAN TBD 8 6 2 THROTTLE INTERLOCK A 3 D3 ONLY Input Data Message Trigger See Lift A uthorize The throttle interlock message is sent to the engine when the lift J 1939 CAT PGN65264 SPN 980 01 hrottle Interlock authorization output is active section 1939 Cummins PGN61441 SPN 972 01 Logic flow charts 7 3 or Throttle Interlock conditions GMLAN TBD Section 8 6 2 1 are met 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 31 69 8 6 2 1 Throttle Interlock The function of the throttle interlock message is shown in the flow chart below 637 Not Active
35. IA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 23 69 6 AUDIBLE ALARM 6 1 Tone Definition The following table details the available alarms mentioned throughout this document These will be referred to by their Audible Alarm name throughout this document to define audible alarms for specific functions The Frequency of the alarm is detailed below The Period is shown as the ON time repeated tones and then the R epetition describes how often the tone is repeated Continuous and Click alarms cannot be acknowledged unless otherwise stated All Beep Alarms will have a 5 min reoccurrence when acknowledged unless otherwise stated Continuous see section 11 1 for timeout config Continuous 1 Buzzer 2 8KHz N A detail Beep 1 Alarm 2 0KHz 160 ms 2Hz Beep 2 Chime 2 8KHz 160 ms 2Hz Beep 3 Seat Belt 2 0KHz 160 ms Continuous Click 1 Relay See below See below See Below 629 6 1 1 TURN SIGNAL CLICK Turn signal Click On Click Off Click T1 Hz Duration ms Hz Duration ms tl 10 000 160 10 000 160 t2 6 200 80 2 800 80 B 2 400 10 2 400 10 t4 10 000 160 10 000 160 5 6 200 150 6 200 80 6 3 600 80 2 800 40 7 920 40 10 000 160 t8 6 200 150 6 200 80 830 770 500 gt t1 t2 t3 t4 t5 16 17 18 2009 Any reproduction of this document whether total or parti
36. INSTRUMENTATION Overview The Blue Bird All American instrument cluster uses all electronic analog guages with stepper motor technology coupled to a microcontroller that provides the necessary electrical control In addition to gauges this ACTIA manufactured instrument clus ter includes an LCD display panel known as a Message Display Center and gauge warning indicators which provide illuminated visual alerts to the Driver The instrument cluster receives both analog inputs from such components as the fuel tank sender and instrument panel dimmer switch binary inputs from brake and directional signal switches and digital signals from components such as the engine and transmission control modules via the J1939 and J1587 data buses The instrument cluster comes with several modes of operation The system is in Sleep Mode when the battery power is applied to the cluster with no other activity In this mode the microprocessor deactivates the power maintain output resulting in low power draws of less than 3mA to support the clock When the instrument cluster sences a change to an input signal such as turning the iginition key on or turning on the headlights the cluster wakes up and then decides which mode to enter depend ing on which input is active Limited Mode is a stand by mode entered when there is battery power available and the iginition is turned off but other input signals are requiring the system to operate such as hazard
37. L L 3 L L L 4 S S S 5 N N N 6 7 M M M 8 D D D 9 2 2 3 10 0 5 0 11 0 0 0 12 0 0 0 13 14 15 ABS Bendix Air ID Byte ASCII EC60 sta EC60 pre 1 B B 635 2 N N 3 D D 4 W W 5 S 5 6 7 8 9 6 6 10 0 0 11 12 5 13 R 14 A E 15 16 17 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 636 BLUE BIRD 110715 F 02 19 09 Page 30 69 8 3 Plug and Play Function The cluster keeps historical list of slave LIN devices attached and continuously verifies that all devices are present while in Ignition mode When a new device is found itis added to the list If a device is found missing a Data Link Warning message will be sent to the LCD but is NOT removed from the list Devices can only be removed from the list through the diagnostic menu 8 4 J1939 Communication Errors If a parameter is not received by J 1939 for 5 seconds it will be flagged as missing Missing LCD information will display a and missing gauge information will be signaled by wagging the pointer from dial end to dial end A missing J 1939 data bus will be announced in the LCD If aLIN parameter is missing for 5 seconds the gauge will wag the pointer from dial end to dial end and flash the warning LE
38. M ichel 16 S M yers 6 26 08 Section 9 1 Changed how Quad 1 is toggled and how Quad 3 and 4 are navigated between to make the commonly used odometer much easier to toggle and the lesser used Parameter Quad 3 the default selection and the even lesser used clock Quad 4 the only one that requires more that one button push and the only one to require the double button push to get to Section 9 2 U pdated instruction on toggling between quad 1 display options and how to reset trip odo Section 9 3 corrected verbiage in quad descrip for 2A to say PRNDL instead of requested gear Section 9 4 1 A dded more description to how quad 3 is changed by the end user Section 9 5 A dded description on how quad 4 is changed by the end user 17 S M yers 7 1 08 Section 3 A dded note to provide updated drawings of the dials to BB if a spec change effects the dial art Per John Williams request to do so All references to Park Brake input PIN 22 changed from AH to AL Per John Williams request Section 5 4 Changed seat belt audible alarm from beep 1 to beep 3 per John William s request for a unique beep for seatbelt logic Also changed trigger to only reference flow chart in section 5 4 1 Section 5 4 1 Changed seat belt logic to actuate if the input is high unbuckled instead of Low buckled per John Williams Section 6 1 A dded Beep 3 tone definition for seat belt as continuous with
39. Photometric Guidelines for Instrument Panel Displays that Accommodate Older Drivers SAE J1939 Recommended Practice for Truck and Bus Control and Communications Network SAE J1708 Serial Data Communications Between Microcomputer Systems SAE J1587 Joint SAE TMC Electronic Data Interchange Between Microcomputer Systems in Heavy Duty Vehicle Applications SAE J1226 Electric Speedometer Specification On Road SAE J1399 Electric Tachometer Specification SAE J1810 Electrical Indicating System Specification SAE J1048 Symbols for Motor Vehicles Controls Indicators and Tell Tales SAE J1362 Graphical Symbols for Operator Controls and Displays on Off Road Self Propelled Work Machines FMVSS 302 Flammability of interior materials LIN Specification Package Revision 1 2 ELECSP13 Bluebird Engineering Standard Electrical environmental specification FMVSS CMVSS 101 FMVSS CMVSS 105 FMVSS CMVSS 135 GMW3097 GMWS3172 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 56 69 14 GLOSSARY ABBREVIATIONS TBD To be determined EEPROM Electrically Erasable Programmable Read Only M emory SAE Society of Automotive Engineers PGN Parameter Group Number J 1939 SPN Suspect Parameter N umber J 1939 FMI Failure M ode Identifier J 1939 662 2009 Any reproduction of this document
40. TERLOCK FAIL flashing forward to reverse video at 500msec intervals ALARM Continuous 1 until fault is gone 3 gt 3 N A ACTIVE N A PIM BRAKE INTERLOCK REQUESTED flashing forward to reverse video at 500msec intervals ALARM Beep 2 on for 5 sec off for 15 sec until fault is gone Hydraulic Brakes Systems w Brake interlock 40051 01 Scenario Vehicle Brake Brake Brake Cluster Behavior Speed Interlock Interlock Interlock Alarm Request Set Input Input CL Input CL CL PIN 35 PIN 27 PIN 26 1 lt 3MPH INACTIVE ACTIVE INACTIVE PIM BRAKE INTERLOCK SETTING flashing forward to reverse video at 500msec intervals ALARM Beep 1 until fault is gone 2 lt 3MPH INACTIVE ACTIVE ACTIVE PIM BRAKE SET ALARM Beep 2 for 2 sec 3 lt 3MPH ACTIVE ACTIVE INACTIVE PIM BRAKE INTERLOCK FAIL flashing forward to reverse video at 500msec intervals ALARM Continuous 1 until fault is gone 4 gt 3 N A ACTIVE N A PIM BRAKE INTERLOCK REQUESTED flashing forward to reverse video at 500msec intervals ALARM Beep 2 on for 5 sec off for 15 sec until fault is gone 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 649 BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 44 69 9 5 Quadrant 4 Quadrant 4 is dedicated to the clock If Applied Air or Suspension Air feature is active Quad 4 i
41. Total Distance traveled TD This data would be stored in the EEPROM TD 2CCVS T Total Fuel Consumed TFC This is the total fuel used value calculated by using the Total Fuel Used PGN65257 SPN250 SA 00 given inL This calculation is based on total fuel captured at the last A verage fuel reset TFr and every 1s after that TFn TFC is calculated by subtracting the reset value TFr from the current value TFn This data would be stored in the EEPROM TFC TF 644 Average Trip AT This calculation is based on TD recorded since the last AT reset This data would be stored in the EEPROM The AT can be reset if the A verage Fuel consumption display is selected for Quad 3 The user will be given a choice to reset or not using the Top button If theAT is reset the current TFC value will be stored as AFC displayed is set equal to Instantaneous Fuel Economy received from the engine SPN 184 AFCr IFE Average Calc At every 1s after the AT reset the following formula will be used to calculate Average Fuel Consumption AFC TFC TD This process will continue every 1s until the AVG is reset Note Both Instantaneous and A verage Fuel Economy values are stored in EEPROM After power up both previously calculated values are kept until a next valid calculation occurs If no message for the fuel is broadcasted than those values will not change At manufacturing the Fuel Economy values are reset to 0 This can of cours
42. ached Therefore the value will not rollover to zero and continue incrementing but will freeze at 9 999 999 9 9 2 1 8 Service Programming If replacement of the cluster becomes necessary the actual vehicle mileage may be programmed into the odometer using Actia proprietary software The mileage may be incremented but not decremented using this software 9 2 1 9 Service Gauges Replacement clusters will be shipped in a mode that allows the installer to preset actual vehicle distance thus eliminating the need to tag the vehicle Documentation on how this mode works can be found in Actia document 104426 O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 36 69 9 3 Quadrant 2 Quadrant 2 2 2 is configured based on active chassis features Quad 2 is 80 pixels wide independent of the configuration Quad 2A is dedicated to the PRNDL and will always be 20 pixels high Quad 2B is dedicated to V oltmeter and mmeter if configured active Depending on the presence of air configurations 2B will be 17 pixels high no air or 15 pixels high with air Quadrant 2C will display only if A pplied Air or Suspension A ir feature is configured active and will be 20 pixels high if present Function Data Source Text Display Example T
43. al without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 24 69 7 BINARY OUTPUTS 7 1 Speed Detect Speed Detect output will be active according to the logic below The display will be on with ODO and Clock and display the message SPEED DETECT ON while active when ignition is off ACTIVE BCL OUTPUT ENABLED ON AL 630 NO NO PB ACTIVE YES OUTPUT ONAL Note BIR Brake Interrupt Request BCL Battery Control Lift Config PB Brake 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 25 69 7 2 Shutter Solenoid This binary output is a low side drive output and is normally active For the logic listed below this output will become inactive Cummins Engines Inactive output when PGN 65262 Byte 1 has a value of gt 180 F and PGN 65270 Byte 3 has a value gt 100 F or engine is not running CAT Engines Inactive output when PGN 65262 Byte 1 has a value of gt 180 F and PGN 65270 Byte 3 has a value gt 140 F or engine is not running 631 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 26 69 7 3 Lift Authorization Lift A uthorization ou
44. al without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 55 69 12 3 Diagnostic Commands The following table shows the possible feature values for diagnostic commanded features set by manf by specific command or by enabling defaults set in the application code The default value for manf to set will be defined on the family print 111027 per part number Feature Command Application Default User Configurable Configured Value Setting after 25 mi Service Gauge YES NO N A M anf Set per print NO Self Test ON OFF N A M anf Set per print YES Display Units M etric U S M ETRIC US N A M anf Set per print YES Dimmer 0 100 100 YES Contrast 0 100 50 YES Engine Hrs XXXX Hrs 0 hrs NO Trip 1 XXXXXXX X mi Omi YES Trip 2 XXXXXXX X mi Omi YES Odometer Reference 0 NO Active LIN device 0 YES Data link warning 0 YES Backlight Color Blue Lt Blue White Red Green YES Green Device ID NO Wakeup NO 13 RELATED STANDARDS 6 6 1 SAE J1455 Joint SAE TMC Recommended Environmental Practices for Electronic Equipment Design Heavy Duty Trucks SAE 71211 Recommended Environmental Practices for Electronic Equipment Design SAE J1113 Electromagnetic Compatibility Measurement Procedures and Limits for Vehicle Components SAE 71812 Function Performance Status Classification for EMC Immunity Testing SAE J2217
45. and backward through the digits 0 9 Pressing m and together stores the digit and displays the next digit to be set The following Screens show programming 7654 2 into the odometer 1 7 Set Digits V Select 674 1 6 Set Digits ok 0 4 2 V Select 1 5 Set Digits ok ok ox 0 542 V Select 1 4 Set Digits 0654 2 V Select O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 69 69 All digits must be set but since pressing the m and buttons together for select brings up the next digit as zero you can quickly set the remaining digits to zero 1 3 Set Digits n76542 V Select 1 2 Set Digits 07654 2 V Select 1 1 Set Digits 10076542 V Select Once all digits have been set the confirmation screen will be displayed Pressing m will accept the mileage while pressing will take you back to the beginning Service Set Gauge screen to start over Odometer will be set to 7654 2 mi OK BACK 675 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD
46. ansLamp ON for SPN 2003_ D416 CHECK TRANS RED 61onm ext Check FMI3landAMBER Trans GMLAN TBD Lamp D402 ABS YEL 590nm ds No 1939 PGNG1441ABS ON 01 Beep 1 for 5 sec HIGH HY DRAULIC SAE J 1362 No D420 OIL TEMP RED 610nm Not required Not required Not required u ON Active Low D404 RED 610nm po Fugen CL Pin 17 only if configured for Continuous English units Flashing at 1Hz for Continuous LOW COOLANT 1939 DM 1LowCoolantLamp SPN111 FMI 1 11 0418 LEVEL YEL 590nm SAE J 1362 No 9 9 GMLAN TBD 18 and AM BER acknowledged Lamp 11939 Continuous D417 HIGH TRANS TEMP YEL 590nm Text Trans Temp DM 1HighTransT empl amp oN poi luntil GMLAN TBD acknowledged Engine Same as D423 HIG Poesia UST YEL 590nm M anufacturer 11939 PGN64892 SPN3698 ia Display Defined M essage ON for SPN 11939 DM1CheckEngLamp ANY FMIANY GMLAN TBD indicator is illuminated and ELT Text Engine ps ao acknowledged D412 ENGINE WARNING YEL 590nm g when the idle shutdown arn PGN65252Shutdown Idle shutdown becomes active will have priority 1939 over engine warning SPN 65000 FMI M 18 Value 011 lamp PGN 64892 will flashin See DPF PIM sequence with DPF display Flash D408 MIL YEL 590nm Text MIL Not Used Not Used Not Used UC rien J 1939 CruiseA ctive ON Anything D403 CRUISE GRN 527nm Text Cruise GMLAN TBD except 000 or 111 None Modified SAE see
47. ast Idle from 27 to 25 and made ohn Williams 7 22 08 Section 1 Added in writing to criteria for standard deviation by customer per John Williams Section 4 2 3 changed the AH to just Active to avoid duplicate info and any confusion between A ctive and A nalog Corrected spelling in D404 row of lamp table Section 5 4 1 A dded park brake decision to logic of seatbelt per J ohn Williams Section 6 1 A dded a little more description to the Audible alarm section to clarify the numbers in the table Section 7 3 Moved battery control Lift config decision to come after Ignition decision per John Williams Section 8 6 2 1 corrected the verbiage to only refer to throttle interlock Removed reference to A3 as this applies to both A3 and CV per John Williams Also updated 11 7 to say that bus type config has no effect on application any more Section 9 4 2 Changed A Iternator Fail to have acknowledgeable alarm Section 9 4 2 Corrected WIF SPN from 197 to 97 7 24 08 D402 ABS alarm changed to self cancel in 5 sec per John Williams Section 7 3 moved in neutral gear decision above park brake set and changed how it interacts with batter cntrl lift decision per J ohn Williams Section 9 4 2 chanced Lift not Stowed alarm and Battery Voltage alarm to Beep l for 5 sec per John Williams Section 9 4 2 added detail that both turn signals at the same time do not apply to turn signal warning logic per John Williams Section
48. cted some of the menu item numbers as they were off by one Section 5 1 6 Corrected gauge direction M oved and restructured Brake Interlock logic tables Removed No Brake Interlock table Removed Stop lamp as it is not used anymore to show Brake peddle depressed Added a note to Drive mode screen section to show that Quad 2 has no user configuration and will be skipped when navigating between quadrants A dded feature programming section to show config bit 1939 T able to the back 6 SMyers 3 21 08 Changed Test panel binary inputs to work with the Input module spare binaries A dded reference to Bus Type config byte to brake interlock logic tables to show referenceto BBCV Corrected the configuration bytes A dded SA 16 to retarder message detail in 1939 table Corrected the logic of turning odo on with ignition off It is not done by dimmer anymore but by headlights or button push A dded Engine ID feature detail 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 3 69 Renamed section 6 5 5 to throttle interlock instead of brake interlock U pdated Plug and play section description to remove roll call references A dded priority message for data link missing Removed 1
49. d intervals 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 41 69 Function Data Source Text Display Example Trigger Display Notes Alarm Format Logic pay Duration Engine 1939 DM 1 SA 00 NR Amber Symbol flashing Continuous Warning GMLAN TBD 9999999 9 16 9 1155A Warning forward to Until As Shown ngine L reverse video at Acknowledg i C 3 Warning AOSAN p 500msec ed intervals Lift Not CL Pin 33 9999999 9 N R D Symbol flashing Beep 1 for 5 Stowed 16 9 155A forward to sec As Shown Active Low reverse video at amp Lift Not Stowed 12 55AM ace intervals Battery J 1939 9999999 9 NR 0 lt 110 1 for 5 Voltage Error PGN65271_SPN 168 V 16 87 155 for gt 30sec Symbol flashing sec then off at forward to GMLAN TBD AsShown E Voltage Error 12 55AM 12 1V reverse video at gt 15 5 500msec then off at intervals 15 3V Turn Signal CL Pin 210 9999999 9 19 When 1 Warning CL Pin 23 16 9 155 vehicle Symbol flashing Turn Signal On 2 travels 1 forward to AsShown lt gt 1ZS5AM mile with reverse video at either turn 500msec signal on but intervals not both Water in Fuel 1 1939 9999999 9 N R D Symbol flashing Beep 1 Until PGN65279
50. depending on quadrant 2 related chassis features Configured without A mmeter 0375 9999999 9 1579F Trans 12 55AM Quad 3 Quad 4 Configured with A mmeter Quad 1 9999999 9 1579F Trans 12 55AM Quad 3 Quad 4 Configured with A mmeter and A pplied Air Quad 1 B9V 155A 2999999 9 Tue 1579F Trans 5 Quad 3 Quad 4 Configured with A mmeter and Suspension A ir Quad 1 9999999 9 Susp Air 150 PSI Quad 2 C 1579F lIransnssoaw Quad 3 Quad 4 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 34 69 9 2 Quadrant 1 Quadrant 1 is dedicated to the odometer or the trip odometers This quadrant is always 169 pixels wide by 37 pixels tall The user can toggle between the odometer trip 1 and trip 2 by simply pressing and releasing the top button Two trip odometers are available and will be designated T1 amp T2 when displayed To reset T1 or T2 simply press and hold the top button while that trip distance is displayed Function Data Source Text Display Example Trigger Display Notes Alarm Format Logic di Duration Odometer 1939 XXXXXX PGN62265 SPN 84 9999999 9 50 App Air R 150 PSI 150 PSI 1579F Trans 5 oAM
51. e EFE ERE ERE Ra d E ER EFE ER TN LER RR DE Rd EEG 23 6 1 1 Turn Signal Click 23 p BINARY OUTPUTS eccL 24 PANS died 24 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 9 69 7 25 SHUTTER SOLENOID ice te ec a des eee e RR ERR RE ERE GU OR DU E E ua e BE RON RN dst A 25 TSSEIFRAUTHORIZATION iieri GRE 26 8 COMMUNICATION 3 1 1939 AUTO DETECT FUNCTION Pe ort ed eei etre eite 27 SEZ e 27 8 3 PE UGAND PLAY FUNCTION e a ner nba cake cea rea cerea a con e dah dera nera rae Y Ya dav ER EN UR 30 1939 COMMUNICATION ERRORS REPRE RE ERE E KEEN KEEN AER 30 S 55 GMLAN COMMURNICATIONIERRORS iiis vec ue var oe A eL RES TY NUTS EAT NGC TRU NE NEAR ENTERA NER DENN 30 8 6 MESSAGES SENT ati rsen iei rae E E 30 8 0 1 Service Brake 30 8 0 2 Throtile Interlock A3 D3 0nly
52. e be displayed in mpg for English units when converted 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX 110715 F INSTRUMENTATION 02 19 09 Page 39 69 9 4 2 PRIORITY M ESSAGES Quad 3 content will be replaced by these messages in the event of their trigger logic being satisfied Some of these messages can be acknowledged by pressing the bottom button which will return Quad 3 to previous display until the recurrence time next ignition or the trigger logic is not satisfied If multiple triggers are present the associated priority messages will cycle every 2 Seconds Function Data Source Text Display Example Trigger Display Notes Alarm Format Logic Duration Engine J 1939 SA 00 M essage Flashing None Comm Fail NR forward to GMLAN TBD As Shown 9999999 9 16 9 155 Available reverse video at No Engine gt 15 500msec Communication 12 55AM intervals Trans Comm 1939 SA 03 M essage Flashing None Fail NR E Not forward to As Shown 9999999 9 16 9 155A Available reverse video at GMLAN TBD No Transmission 12 55AM gt 15 500msec Communication 2 intervals ABS Comm 1939 SA 0B M essage Flashing None Fail NR forward to As Shown 9999999 9 16 9V 155A Available reverse video at GMLAN TBD No ABS 12 55AM gt 15 500msec Communication
53. e configuration that is built Some of these can be configured through the diag menu as shown above The default value for manf to set will be defined on the family print 111027 per part number 12 1 Byte 0 Feature Bit Value User Configurable Address after 25 mi Buzzer Timeout Enable BitO 0 YES 1 0N Test Panel Enable Bit1 0 NO 1 0N Turn signal click Enable Bit 2 O OFF YES 1 0N Ammeter Enable Bit3 0 5 1 0N Brake System Type Bit 4 lt ir Bendix NO 1 Hydraulic WABCO Applied A ir Suspension A ir Bit5 0 Disabled OFF YES Enable 1 Enabled ON If bit 4 is set to Air this option effects A pplied A ir If it is set to Hydraulic it effects the Suspension air feature Buss Type Bit 6 0 BBD3 NO 1 BBCV Clock Mode Bit7 0 12 hrs mode YES 1 24 hrs mode 12 2 Byte 1 Feature Bit Value User Configurable Address after 25 mi Engine Type Bit0 0001 Cummins 15807 1939 NO Bitl 0010 Cummins 15 07 1939 Bit2 0011 Cummins ISLGO7 1939 0100 CAT Diesel C7 1939 Bit3 0101 2 GM Gas 1850 0110 2 GM Gas GMLAN 0111 Cummins OTHER 1000 OTHER Battery Controlled L ift Option Bit4 0 Disabled OFF NO 1 Enabled ON ABS Type Bit5 0 WABCO NO 1 B endix Trans Type Bit 6 0 A Ilison NO 1 Other Seat Belt Logic Bit7 0 Disabled NO 1 nabled 2009 Any reproduction of this document whether total or parti
54. e faulty If the gauge indicator needle now indicates a reading the original malfunction is probably not due to a faulty instrument panel harness A gauge test can determine if the gauge itself needs to be replaced There are other test and troubleshooting techniques available in Appendix 1 Refer to the manufacturer s service manual for instructions regarding signals originating from the engine ECM or transmission TCU Electrical diagrams can also be found in this manual to aid in troubleshooting the entire circuit 0 BLUE BIRD 0 SERVICE MANUAL 42 A El ll E Instrument Cluster Appendix 1 INSTRUMENTATION 110715 F 02 19 09 Page 1 69 52765BridgerCourt Phone Elkhart IN 46514 Fax USA www actia com MY08 Bluebird Corporate Cluster Functional Specification 607 NOTICE OF PROPRIETARY INFORMATION This document and its contents are proprietary to A ctia This publication and its contents may not be reproduced or distributed for any purposes without the written permission of A ctia By Date ACTIA Ref Revision Written MY08 Reviewed Specifications 110715 F A pproved 2009 Any reproduction of this document whether total or P age 1 Format partial without the written consent of ACTIA is forbidden U S L etter 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is
55. ected seat belt alarm in lamp table Corrected Data sources for MIL and LOW FUEL PRESSURE lamps in lamp table Out dented binary output descriptions for clarity Removed duplicate Brake Interlock flow chart in section 9 1 4 Added only reference to Brake interlock logic flow chart in section 8 6 5 Defined Brake interlock logic in section 9 1 3 3 as the display logic for BBCV only Added Throttle Interlock message reference to lift authorization Flow Chart for clarity M oved Brake Interlock flow chart to message sent section for clarity O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX e BLUE BIRD e BLUE BIRD 110715 F SERVICE MANUAL 02 19 09 Page 4 69 Removed LOW FUEL PRESSURE binary trigger from the warning light table and from the warning bank input table per John Williams statement that CUMMINS ISLG isthe only CNG we support and that is triggered with the voltage on pin 10 of the cluster Corrected audible alarms associated with warnings per M ichel markups Changed byte 0 bit 7 of config table from unused to clock mode 14 S Myers 6 19 08 Corrected connector pinout to show 1939 on pins 3 amp 4 and GM LAN pins 5 amp 6 15 S M yers 6 25 08 Updated Cruise control lamp function to use States instead of Active to match current A 3 functionality that was never documented before per
56. emote dimmer input 10 6 1 Added dimmer adjustment to the LCD menu 5 2 amp 7 2 3 Added scroll description 7 1 Added suspension air screens 7 1 2 5 amp 7 3 7 Added Transmission amp ABS diagnostic screens 7 28 amp 7 29 Added self test screen 7 3 3 5 S Myers 3 6 08 Section 10 6 U pdated the Cluster Connector Pinout table to match the hardware Fuel level moved to pin 34 All designations from pin 11 pin 17 moved down one pin Hi Hydraulic Oil Temp Hyd Brake Fail moved down to pin 17 All designations from pint 22 pin 25 move down one pin Pin 25 changed to spare Seat belt moved to pint 32 Added a little more description to the pins Added wakeup designation column for clarity on Hardware or Software configurable wakeup Also added a column for individual connector pinout for clarity Section 7 27 Corrected the Engine Diag display to show the J2012 information instead of the SPN FMI for GM only Section 7 28 Corrected the Trans Diag display to show the J2012 information instead of the SPN FM I Section 5 1 A dded stepper motor designators to each gauge for clarity on location Section 5 1 4 Changed scale type to linear and max scale to be 100 psi to match the dial Also corrected direction to be CCW to match dial Section 5 1 7 Corrected trigger to be for rear air instead of front air Probably a cut past error Combined all indicator lights into single table in section 5 3 for clarity Section 7 2 corre
57. enu e BLUE BIRD BLUE BIRD 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD SERVICE MANUAL 02 19 09 Page 48 69 10 7 4 1 0 STATUS Item D Displays the module pin number and the status as received by the vehicle s electrical System Scroll through all the status screen by screen using the up and down arrows Press both buttons to exit to the previous screen screens shown for reference only actual inputs may differ VO STATUS I O STATUS CL 1 Battery 138V CL SCAN2 DATA CL 5V PWR SV CL IS App 25V CL 2 Ground GNO CL 6CAN2 DATA CL 10 CNG Press 35V CL 14 App Rear Air 25V CL 3 CAN DATA CL 7LIN DATA Prev CL 11 Frort Air Press 25V CL 15Ammeter 1204 Prev CL 4 CAN DATA CL 876VPWR 78V amp CL 12 Rear Ar Press 25V CL 16 Spare N A amp Press on both buttons to Exit Next Press on both buttons to Exit Next VO STATUS STATUS CL 17 Hi Hyd Oil LOW CL21LeflTun HIGH CL 25 Spare N A CL 28 Lift Auth OFF CL 18 Ignition HIGH CL 22 Park Brake HIGH CL 26 WIF LOW CL 30 Shutter Sol ON CL 19 HL Alert HIGH CL 23RightTum HIGH Prev CL 27 Altemator LOW CL 31SpeedDet OFF Prev CL 20 Hi Beam HIGH CL 24 Service Brk HIGH CL 28 RearEngDr LOW CL 32 Seat Belt HIGH Press on both buttons to Exit Next D Press on both buttons to Exit Next D CL 33 Spare N A WB 1 ILk Aln HIGH W85 Low Fuel Pres HIGH CL 34 Fuel
58. er will stay awake for 4 seconds after loss of IGN and 10 seconds after loss of any other wakeup 4 1 3 CLOCK The clock will remain awake in the background as long as battery power is applied It will only display on LCD when in Limited or Ignition mode 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 13 69 4 2 Limited Mode The system runs in limited mode when battery power is available the ignition input is not active but other input signals are requiring the system to operate The system exits limited mode when the ignition becomes active or the input signals that caused the system to wake up become inactive 4 2 1 DISPLAY ODOMETER amp CLOCK IN LCD The odometer and Clock is readable with the ignition off when the Headlight input is Active or M ode or Trip button is pressed The cluster will go back to sleep mode if the H eadlight input is not active or 15 sec after the mode or trip was pressed 4 2 2 HAZARD WARNING LIGHTS The right and left turn icons are operational with the ignition off when the hazard lights are turned on right and or left turn binary inputs high 4 2 3 BRAKE INTERLOCK REQUEST When this input is A ctive the cluster power supply will wake up only to check the Battery control lift config and depending on the setting will either carry out the logic for the outputs
59. et DIEI E Renee ree eue ires CAA LEGAL 30 IRE BE Ic EEEE SH H 32 80 41 Fast Idle iive er b paa ket eye 32 9 MESSAGE DISPLAY CENTER TN 33 9 T DRIVE MODE SCREEN cde n vec ec ea t are wane an etude ae Eu ut en 33 9 2 QUADRANT 1 9 3 QUADRANT 2 9 4 QUADRANT 3 94 2 Priority MesSQBGSii bos aea PE EE E eph euni buead here ees eus eed 38 5 QUADRANT E PE 44 10 SETTINGS AND DIAGNOSTIC eese esee tees setenta tatnen stata tatus tata tasa tasa tasse tatnen stata 45 BRAKE mE 45 10 2 SET UNITS 10 3 CONTRAST 10 4 DIMMER 10 5 COLOR rev c ie NR NN E MA NOR d NE RO NEAN PEE INR 6 COCK e nc M uc MEE MM 10 7 INSTRUMENT DIAGNOSTICS 10 7 5 I O Status DATA CINK p 10 9 READ PARAMETERS iiri inris ip seas ue riv gerer Ud ud erre ra re un rn viv pre Grave Ur utn var ed 10 10 ENGINE DIAGNOSTIC 10 11 TRANS DIAGNOSTIC 10 12 ABS DIAGNOSTIC is iuste evan ev eher e cara eva exa Era Yr SN c e E NA Nu a NN QNARE NA TRE PN 11 CONFIGURATION MENU a
60. forbidden APPENDIX BLUE BIRD 608 e BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 2 69 Revision Table Rev By Date Software Description 0 RParks 11 26 2007 1110940v00 01 Original Draft Out for comment 1 R Parks 11 29 2007 U pdated per comments from K evin Decker 10 6 1 7 1 2 3 7 1 2 4 7 1 2 5 2 R Parks 01 16 2008 Changed tachometer to 5000 rpm 5 1 2 Removed Stop light warning light 5 3 12 Removed stop light inhibit configuration bit 7 3 6 A dded Brake Interlock priority message 7 1 3 25 Removed retarder warning light 5 3 11 A dded retarder priority message 7 1 3 26 A dded source address to retarder message 6 5 Changed engine shutter solenoid activation level 5 5 2 Removed range inhibit warning light 5 3 8 A dded range inhibit priority message 7 1 3 27 A dded Trans fluid life Trans fluid filter Trans service priority messages 7 1 3 28 7 1 3 29 7 1 30 6 5 3 R Parks 02 12 2008 Added Seat belt warning light amp audible alarm 10 6 1 5 3 18 Added device auto detect feature Assigned LED designators to all warning amp indicator lights 5 1 5 3 Changed symbol references 5 3 1 5 3 2 5 3 4 5 3 10 A dded screen shots to LCD parameters A dded suspension air to the set up menu 7 3 7 4 R Parks 02 27 2008 Replaced the m amp t button references with lower amp upper All Removed the r
61. ges will function normally and buzzer tones associated with the warnings will be allowed Once set the Service Set Gauge screen will not be seen again and the odometer value cannot be changed 15 3 Setting the Units Prior to setting the odometer value the technician must indicate to the gauge whether English miles or metric kilometers units are being set The gauge will default to the unit that was set when the gauge left the factory To change press the m or t button to scroll to the proper unit and press both buttons to select Service Set Odometer Service Set Odometer Odo in miles Set Odo in miles Set Odo in kilometers Set Odo in kilometers V Select A V Select A 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 673 BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 68 69 15 4 Setting the Odometer Value By using the m or button to scroll you can highlight either Set Odometer V alue or Zero Odometer Service Set Odometer Service Set Odometer Set Odometer value Set Odometer value Zero Odometer Zero Odometer V Select V Select Selecting Set Odometer Value displays the Set Digits screen while selecting Zero Odometer displays the confirmation screen Set Digits mi Odometer will be set to Kap 0 0 mi V Select OK BACK Each digit is set by using the m and buttons to scroll forward
62. inters will drive to zero position The pointers will then drive up scale pausing at scale before completing the sweep to full scale The pointers will then return to zero position before moving to the commanded position 4 3 1 2 LCD D uring the up scale sweep of the pointers the LCD will turn all its segments on for one second off for one second and then display the opening message The opening message is the Bluebird logo followed by the software ID complete with revision level 4 3 1 3 Warning Lights Starting at the up scale pointer sweep all warning lights will turn on for 5 seconds and then out Active warning lights will turn on when the gauges go to their commanded position 4 3 1 4 Audible Alarm The audible alarm will sound three different tones for one second each during the up scale swing of the pointers 4 4 Ignition Mode The ignition mode is active as long as the ignition switch is on The ignition is the normal operational mode of the system 620 If the ignition line goes low the micro will zero all gauges except the fuel gauge which will remain at its last commanded position and store any data to the EEPROM before turning the supply off After storing the data the system goes to sleep mode after a delay of approximately 4 seconds 4 5 Sleep Mode When the system is in sleep mode the clusters microprocessor goes into low power mode and draws less than 3 mA to support the clock function The system exit
63. l Pressure 3 6 100 1 11 and 18 0 DM1 65 226 OOFECA Amber warning light Check 1b 4 amp 3 2003 31 3 Transmission 3 6 DM1 65 226 OOFECA High Trans Temperature 10463 177 15 3 3 6 DM1 65 226 OOFECA Low Coolant Level 3 6 111 1 11 and 18 0 DM1 65 226 OOFECA Trans Fluid Filter 3 4 5 3359 31 3 O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 667 e BLUE BIRD 668 e BLUE BIRD SERVICE MANUAL 110715 F 02 19 09 Page 62 69 DMI 65 226 00FECA Trans Fluid Life 345 477 17 DM1 65 226 Trans Sevice 345 4178 31 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 63 69 14 5 GM LAN Tabel TBD 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX BLUE BIRD D3FE SERVICE 110715 F 02 19 09 Page 64 69 vera Designation Description CLU C261 251 Software C25101 45Vdc Regulated 5V dc Sensor Power 50ma max current draw 10 C25102 CNG Fuel Pressure Sender 5 VAI 1 5V Software Configurable VAI 0 7V 11 C25103 FrontAir Pressure Sender Suspension A ir S VAI 0 5 4 5V Software Configurable VAI 0 7V 12 C25104
64. mulated relay click audible sound W hen this configuration is DISABLED there will be no sound for turn signal 6 5 8 11 4 Ammeter Display When this configuration is ENABLED the Ammeter value is shown in the display beside the V oltmeter See section 7 1 When this configuration is DISABLED only the V oltmeter is shown 11 5 Brake System Type When this configuration is set to AIR the software is configured to use the Front and Rear Air inputs to display the front and rear air pressure on the appropriate gauges When configured as HYD the software will not drive these gauges and will use the Front Air input to determine Suspension Air Pressure This setting will also effect how the Brake Interlock PIM logic works section 9 4 2 1 11 6 Applied Suspension Air When this configuration is ENABLED the software is configured to display Applied Front and Rear Air Pressure for Air Brake System or Suspension Air for Hydraulic Brake System depending on Brake System Configuration When DISABLEED Applied air Suspension air are NOT displayed See section 7 1 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 53 69 11 7 Bus Configuration Type The cluster can be configured to be used on one of two product lines BBD3 or BBCV This setting will effect the binary logic for Park Brake and Fast Idle in
65. n to allow setting the LCD contrast Pressing the lower button will increase contrast while pressing the upper button will decrease contrast This menu will auto exit to the previous screen after 10 sec timeout with no activity CONTRAST Dark 2 10 4 Dimmer Selecting menu item 4 displays a screen to allow setting the cluster backlighting brightness Pressing the lower button will decrease brightness while pressing the upper button will increase it This menu will auto exit to the previous screen after 10 sec timeout with no activity DIMMER par Dark 10 5 Backlight color 652 Selecting menu item 5 displays a screen to allow setting the cluster backlighting color Pressing the buttons will toggle between a list of preset colors BACKLIGHT COLOR RED EN BLUE LTBLUE WHITE o Press both buttons to Save Exit Next D 10 6 Set Clock Selecting menu item 6 allows the user to set the clock Pressing both buttons will first select the hours selection and it will be highlighted Subsequent presses of both the buttons will select minutes and the AM PM selections Once any selection is highlighted then the Jower buttons will decrease the setting and the upper button will increment the setting Once all three selections have been selected this menu will timeout to the previous menu after 15 seconds unless the operator enters back into any of the selections SET CLOCK ipi 00 AM p Pres
66. own will be 0 9 km 0 56 mi Battery loss that occurs gt 4 seconds after turning the ignition off will NOT result in an abnormal shutdown The occurrence of an abnormal shutdown during the life of a vehicle should be rare 9 2 1 5 Durability The EEPROM store routine will allow for a minimum of 4 million store cycles The design will accommodate 200 key offs per day 260 days per year for 20 years plus 1 609344 million kilometers 1 000 000 mi which could be seen if the vehicle is used on a delivery route with a 5096 safety factor 200 260 20 1 609 334 2 649 334 5190 4 000 494 store cycles An error recovery scheme is implemented that will allow the odometer value to be recovered should a hardware failure in one of the EEPROM memory cells occur 9 2 1 6 Error Recovery The error recovery algorithm will check each stored value to determine if the values are in sequence low to high and 1 km or less apart If this condition is found no errors are present and no further action is required If a value is found to be out of order or greater than 1 km from the others the software will identify the largest value in the group with the proper sequence and use that value 641 In the unlikely event the speedometer fails in such a way that the odometer value cannot be displayed the factory in most instances will be able to recover the stored value 9 2 1 7 M aximum R eading The odometer will stop incrementing when the maximum display count is re
67. puts They will be as follows Input BBD3 BBCV Park Brake AL AH Fast Idle AH AL 11 8 Engine Configuration Type This configuration is set by internal logic based on Engine ID s broadcast on the data bus This will effect what messages are sent for Throttle Interlock and Fast Idle functions section 8 6 It may also effect what Parameters are available to display in Quad 3 on the LCD section 9 4 1 11 9 Self Test W hen this configuration is ENABLED the cluster will perform a startup self test at Ignition See section 4 2 1 When the configuration is the cluster will not perform a startup self test 11 10 Battery Controlled Lift When this configuration enabled it affects the logic of several of the outputs See section 7 for 659 details 11 11 Seatbelt Logic When this configuration is ENABLED the Seatbelt Logic for the alarm and lamp detailed in section 5 4 1 will apply If itis DISABLED this logic will not apply No alarm or lamp will be triggered if this is the case When disabled if the seatbelt input is pulled low this will automatically enable the configuration O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 54 69 12 FEATURE PROGRAMMING The following table shows the bit address for the configurable features These will be set by M anf depending on th
68. r Amp brk light shet to 70 10 Parking brake sys long term supv Prev Press on both buttons to Exit Next D 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 51 69 11 CONFIGURATION MENU Holding both buttons pressed while turning the ignition on enters the Configuration M enu In this menu configurable features can be enabled and disabled If the cluster has logged less than 25 mi all menu selections can be changed using the buttons After 25 mi some items will only be able to be modified using a Diagnostic tool via PC or other diagnostic interface that can communicate with the cluster on the diagnostic layer To change a feature configuration with the buttons scroll up or down to it and then press both buttons to change the config After 25 mi you will be able to see all menu items but only change the items that are USER CONFIGURABLE see the feature config tables for this info The rest will require the diagnostic tool after 25 mi This menu will auto exit and the cluster will re initialize its startup routine after 10 sec timeout with no activity CONFIGURATION MENU BUZZER TIME OUT D TEST PANE DISABLED Prev TRUN SIGNAL CLICK ENABLED Press on both buttons to Change Next CONFIGURATION MENU AMMETER DISPLAY ENABLED BRAKE SYS TYPE R Prev APPLIED SUSP AIR ENABLED D Press on both bu
69. rigger Alarm Format Logic Display Duration Voltmeter J1939 XX XV PGN65271 5 168 NR o 9999999 9 16 9 PGN65271 SPN 157 F Trans 12 55AM 158 If both are available SPN 168 will be used GMLAN TBD J1939 PGN61445 SPN N R E 523 9999999 9 16 9V 642 GMLAN TBD 1579F Trans 12 554M Front CL Pin 13 XXX 9999 9 TB SV T55A ii o DE ts 1579F 25 R ear CL Pin 14 XXX Tie NRE Applied A ir PSI 9999 9 Am APR 1579F Suspension 099999999 118 Susp Air bus only 1570F Transiacoam O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 37 69 9 4 Quadrant 3 Quadrant 3 is dedicated to the parameters screen and the priority messages This quadrant is 169 pixels wide by 39 pixels tall 9 4 1 PARAMETERS Quad 3 can be configured by the user to display any one of these parameters The user must press and release the bottom button which will highlight the quadrant in reverse video Then to toggle the selection you must either press the bottom button or top button to scroll through the possible parameters to display This Quad will default back to Trans Temp at each ignition cycle Function Data Source Text Display Example Trigger
70. rporation Initially to be used on the D3 and CV bus lines The instrumentation is based on gauges with stepper motor technology married to a microcontroller that provides the necessary electrical control Circuit provisions are included to assure compliance with SAE 1455 in cab standards and Bluebird electrical SP13 environmental specification All gauges and indicator or warning lamps as well as displays are to comply with FM V SS CM VSS 101 standards unless deviation is approved by the customer in writing 2 SCOPE This document covers the operational specifications of the instrument panel and gauge system for use in Bluebird school buses Engine transmission and ABS systems used in this application are listed in the table below Engines Transmissions ABS Systems Cummins ISB07 Diesel 15 07 Diesel Allison 2000 2500 3000 1939 W abco Hydraulic Systems J 1939 ISLG J 1939 GM 8 1L Gas J1850 amp GMLAN Bendix EC30 Air Systems 1939 CAT C7 Diesel 1939 Bendix EC60 A ir Systems 1939 N ote 1850 communications facilitated through A ctia J 1850 to 1939 converter module A ctia 106622 617 3 RELATED DOCUMENTS For more detail on functional or visual details of this instrument system the following documents must be consulted e 110763 Dial face with Air Gauges If spec change effects graphics updated art must be supplied to the Customer for approval and documentation on
71. s 80x15 If no air features are active then the Quad 4 is 80x23 Quad 4 can be toggled between 12 and 24 hour mode settings To do this you must first press and release the bottom button to activate quad 3 and then press and release both buttons simultaneously which will highlight quad 4 in reverse video and allow you to toggle between the 2 modes by pressing and releasing the top or button Function Data Source Text Display Example Trigger 1 Format Logic Display Note Duration Clock Internal clock crystal N R 9j W hen clock is 9999999 9 ee 1579F Trans 12 55AM pressing amp holding the m Ree amp t buttons 16 9 155A changes from 9999999 9 27 5 henges fr ET 12 to 24 hour 150 PSI _150 PSI 1579F 12 50 mode 650 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 45 69 10 SETTINGS AND DIAGNOSTIC This menu allows the user to change certain features from their default settings and to use diagnostics to trouble shoot the instrumentation Access this menu by setting the park brake and then from the Drive M ode Screen press the lower button for gt 5 seconds SETTING amp DIAGNOSTICS SETTING amp DIAGNOSTICS 1 Air Brake PSI 4 Dimmer 7 Instrument Diag 10 Engine Diag 2 Set Units 5 BL Color Prev 8 Data
72. s both buttons to set hrs min am pm D 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 41 69 10 7 Instrument Diagnostics Selecting menu item 7 in the Settings and Diagnostic M enu will display the instrument diagnostic menu INSTRUMENT DIAGNOSTICS A Gauge Test Status B Lamp Test E Exit Prev C LCD Test D Press on both buttons to select Next D 10 7 1 GAUGE TEST Item A The selected gauge will be driven through three positions pausing at each position as shown in the LCD as a percentage of scale This test will proceed through all gauges and return to the menu Pressing the Zower button Exit will end the test and return to the previous menu Fuel Level Fuel Level Fuel Level 0 Exit O 5 0 Exit 1 00 Ext D 10 7 2 LAMP TEST 653 Item B Turns each IP warning lamp not the vehicle load on then off displaying the lamp name and status in the LCD This test goes through all warning lamps and then returns to the menu Pressing the lower button Exit will end the test and return to the previous menu High beam test shown as an example High Beam High Beam ON OF Ext Ext 10 7 3 LCD TEST Item C Displays the Bluebird logo in normal and reverse video three times and then return to the previous menu Pressing the lower button will end the test and return to the previous m
73. s sleep mode when one of the wake up inputs become active When the cluster wakes up it first begins to control the power supply by activating the power supply maintain output Itthen decides depending on which wake up input is active what mode must be entered W hen the system goes back to sleep it simply deactivates the power supply maintain output 4 6 Self Diagnostic Mode The self diagnostic mode is entered through a menu selection using the LCD Diagnostics is only available when the Park Brake is set The self diagnostic includes the following tests e Gauges e LCD 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 15 69 e Warning Lights e Binary Inputs e Analog Inputs e Binary Outputs Detail specifications are found in the M essage Display Center section 4 7 Test Panel Mode The test cluster mode can only be activated through Actia provided software When selected the software is configured as a production chassis test fixture The functions below describe the difference in operation for this mode 1 An active Binary Input on WB PIN 6 will configure the cluster for Chassis with System A ir If itis not active it will be configured for a Hydraulic system 2 An active Binary Input on WB PIN 7 will configure the cluster for Chassis with Applied Air front and rear applied air 621
74. seat belt logic D411 SEAT BELT RED 610nm 11362 No 8 14 CL Pin 32 section below Beep 3 ON ActiveLow D405 BRAKEFAILURE YEL 590 nm E CL Pin 17 only if configured for Continuous M etric units D 407 SPARE RED 610nm TBD TBD TBD TBD D409 SPARE Y EL 590nm TBD TBD TBD TBD D414 SPARE RED 610nm TBD TBD TBD TBD 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden e 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 21 69 D415 SPARE RED 610nm TBD TBD TBD TBD D419 SPARE Y EL 590nm TBD TBD TBD TBD D421 SPARE Y EL 590nm TBD TBD TBD TBD D 422 SPARE RED 610nm TBD TBD TBD TBD 627 O 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 e APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 22 69 5 4 1 SEAT BELT LOGIC This warning light amp audible alarm are active when the requirements are met shown in the flow chart below Ignition No Warning Light or Audible Alarm Seat Belt Signal NOT ACTIVE unbuckled No Warning Light or Audible Alarm 628 No Warning Light or Audible Alarm Both Warning Light And Audible A larm Warning Light On Only 2009 Any reproduction of this document whether total or partial without the written consent of ACT
75. tem 9 Displays all of the converted values for the applications parameters in a table form for vehicle troubleshooting Y ou can scroll though to view them and press both buttons to exit to the previous screen READ PARAMETERS READ PARAMETERS Engine Speed 775 RPM Trans Temp 160 F Avg Fuel Eoon 12mpg Batter VoBage Coolant Temp 100 F Boost Pressure 5 PSI Intake Temp 100 F Ammeter Pressure S4PSI Engine Load 25 ke Engine Hours 67 80h Front Air Press 120 Pe Prev Fuel Level 27 Inst Fuel Econ 12 mpg Vehicle Speed Omph Rear Ax Press 120 PSI Press on both buttons to Exit Next d Press on both buttons to Exit Next id 10 10 Engine Diagnostic 10 Displays engine DTC s in a format dependant on engine type Engine type and number of active DTC s is located in upper right corner Press both buttons to exit to previous screen CAT Cummins This screen displays the Suspect Parameter Number SPN and Failure mode Identifier as received from the engine for active faults via J 1939 A ctive faults shown below as examples 655 i i i CAT i i i CMNS Engine Diagnostics a ___ Engine Diagnostics ylinder 3 Fault 102 02 Boost Pressure Data Incorect 84 02 Invalid Vehicle Speed 100 18 Low Oil Pressure 100 11 Very Low Oil Pressure Prev 150 00 Engine Speed gt than 2730 RPM Prev 168 02 intermittent Battery D 97 15 Water in Fuel sensor circuit D Press on both buttons to Exit Next D Press on both buttons to Exit Next D GM
76. the fuel gauge which will remain at its last command position The Self Diagnostic Mode is entered through a menu selection The self diagnostic tests include the gauges LCD warning lights binary inputs analog inputs and binary outputs Detailed specifications can be found in the Message Display Cen ter section of the appendix The backlighting on this instrument cluster is adjustable through an internal dimmer This is done using the two buttons on the face of the cluster The backlight color can also be changed through the setting and diagnostics menu accessed using the same two buttons on the face of the cluster Backlight colors are blue light blue white red and green The white LCD and amber pointer backlights are not adjust able The cluster also uses its microprocessor to compute logic required for certain units to function When the logic is satisfyied an output is generated and sent to these units to satisfy their operational needs Units requiring logic outputs include Speed Detect used in the brake interlock system Seat Belt Logic used for alarms and Lift Authorization used to supply power to deploy the handicap wheelchair lift The instrument cluster is a sealed unit with no serviceable parts including gaug es lights and buzzers If your cluster is found to be defective it is replaced in whole as a unit Appendixes In This Chapter Appendix 1 08 Blue Bird Corporate Cluster Functional Specification This AC TIA publica
77. tion was created especially for Blue Bird and details the operation of the instrument system including a detailed explanation of the Message Display Center s menus and diagnostic capabilities INSTRUMENTATION Instrument Cluster Removal The instrument cluster is designed for easily removed from its housing by means of seven screws around the perimeter of its face The instrument cluster is not designed for disassembly and is removed as a unit 1 Turn the iginition switch to the off position and remove the key Lower the steering wheel to the bottom of its travel 2 Remove the seven machine screws from around instrument panel s perim eter 3 Carefully pull the instrument assembly away from the dash housing and tilt face down 4 Disconnect the electrical connectors from the back of the instrument cluster and remove unit Testing a Gauge By Substitution To help quickly determine if a suspected gauge is faulty the harness connnector from an adjacent gauge can be temporarily substituted 1 Label and remove the wiring harness from the gauge in question 605 2 Label and remove the wiring harness from an adjacent gauge 3 Plug the connector from the known good gauge into the suspect gauge 4 Support the instrument cluster in a safe position 5 Turn the ignition switch to the ON position Start the engine if necessary 6 Check whether the suspect gauge now indicates a value If it does not the gauge may b
78. tor Fail PIM logic per J ohn Williams Section 9 4 2 Removed Hi Hydraulic Oil Temp PIM per John Williams Section 9 4 2 Removed Hydraulic Brake Fail Low Front and Rear Air PIM s per John Williams Section 9 4 2 Changed Water in fuel PIM data and logic to 1939 per John Williams Section 13 A dded FM V SS CM V SS 101 105 135 per John Williams Changed Water in Fuel SA to 0 and from TX to RX in the 1939 message table per John Williams Section 14 8 Removed MIL input as it is no longer needed and moved all other inputs except test inputs to cluster connector per J ohn Williams 7 14 08 Changed section 8 6 2 1 to say Throttle interlock instead of Brake interlock to reduce confusion between this and section 9 4 2 1 brake interlock message logic matrix Section 9 4 2 1 updated the brake interlock PIM logic matrix per John Williams A dded Interlock Alarm and vehicle speed Changed displays to flashing and added different alarms per J ohn Williams Section 11 7 Updated bus type config description as the Brake interlock logic is now not exclusive to BBCV but will be used on D3 as well Section 7 1 A dded park brake set to Speed detect logic per J ohn Williams Section 14 6 Added Fast Idle input to PIN 27 as BIN AL Section 8 6 A dded Fast Idle message Section 10 Added an Air Brake PSI view screen to setting and diagnostic menu for Pretrip Brake Inspections per J ohn Williams Moved BRAKE interlock Alarm from pin 25 to pin 27 and moved F
79. tput will be active according to the logic below The display will be on with ODO and Clock and display the message LIFT AUTHORIZATION ON while active when ignition is off START EN Gear Eng BCL ENABLED YES 632 PB ACTIVE OUTPUT ON AL Cont until L ift Door Open is deactivated 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 21 69 8 COMMUNICATION There are two communication channels for data transfer between the vehicle and the speedometer One channel for CAN 2 0B GMLAN Controller Area Network and a second channel for CAN 2 0B SA E J 1939 Controller A rea N etwork All frames transmitted by the speedometer on J 1939 are continuously sent at the standard broadcast rate for the frame using source address SA 23dec 17h The cluster communicates via the LIN bus to slave devices The slave gauges are updated every 80mSec 8 1 J1939 Auto Detect Function The cluster will monitor the J 1939 at start up and will look for Engine SA 00h Transmission SA 03h and ABS SA OB h systems 8 2 Engine ID To allow the cluster to be configured to multiple engines the cluster will request engine make amp model for 1939 protocol engines by sending a request for PGN 65259 SPN 586 and 587 The
80. ttons to Change Next CONFIGURATION MENU BUS CONFIG TYPE BBD3 ENGINE TYPE CAT Prev SELF TEST ENABLED D Press on both buttons to Change Next D The default value of these settings is defined on the assembly line print and set on the line per part number 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden APPENDIX BLUE BIRD D3 FE SERVICE MANUAL 110715 F 02 19 09 Page 52 69 11 1 Buzzer Time out Enable When this configuration is ENABLED the continuous 1 audible alarm Buzzer would be allowed to timeout in 15 sec if the engine speed is lt 400 RPM When this configuration is DISABLED the continuous audible alarm will not time out 11 2 Test Panel When this configuration is ENABLED the cluster is set as a manufacturing tool for the chassis test fixture and the software will ignore the internal configuration for BRAKE SYS TYPE and APPLIED SUSP AIR It will instead receive this configuration information from the optional input module binary inputs See section 12 8 When this configuration is DISABLED the cluster is set as a normal production part and will use the internal configuration to determine BRAKE SYS TY PE and the presence of APPLIED or SUSPENSION AIR This feature is displayed in this menu but can only be changed using a VCI and ACTIA provided software 11 3 Turn Signal Click When this configuration is ENABLED the turn signal will use the si
81. urations messages and menus M oved Data link out of instrument diag submenu and restructured for clarity U pdated all screens in Setup and Diag menu to take advantage of the large screen and stay consistent in navigation features 11 SMyers 5 15 08 M odified Setup menu to be Configuration menu to clear up confusion between this and the diag and setting menu Updated section 4 1 1 by changing dimmer to headlight for ODO limited mode trigger and added the buttons 12 SMyers 6 12 08 Section 4 2 1 Added a little better description of how long the clusters stays in Limited mode when wakeups are used Section 5 3 Clarified and corrected Park Brake lamp function in the table Section 5 3 Removed 1 from Wait to Start to match multigauge function Section 5 3 A dded A mber Lamp to Check trans DM 1 trigger to match A3 Section 5 3 A dded A mber Lamp to Low Coolant DM 1 trigger to match A3 1939 message table updated EBC1 to show SA of 0B instead of 11 as all of these are represented in HEX 1939 message table updated the SA for all sent messages to 17 for same reason This matches function 13 SMyers 6 17 08 Out dented Audible alarm section 5 4 to be section 6 and clarified definition of alarms Added more description to section 5 3 for associated displays and warning alarms and how they are acknowledged Referenced High Exhaust temp Lamp trigger and alarm to be the same as the High Exhaust temp Display message Corr
82. utton the display will go back to the previous screen and the alarm will stop but the indicator lamp will remain active The alarm display will reocure if fault still exists at text ignition of in a predetermined time frame if noted the user Pos Function Color Graphic Data Source Trigger Logic ne urat D401 LEFT TURN 527nm SAE J 1362 14 9 CL_Pin_21 ON Active High Click 1 D413 RIGHT TURN 527nm SAE J 1362 14 9 CL_Pin_23 ON Active High Click 1 On steady if Active NONE and IGN is ON PARK BRAKE CL Pin 22BIN AL Flash 1Hz for 2 min Z 7 7 then Off if not active D406 AED ei SAE No amp Ignition Off 2 when Flash at 1Hz if Active Lamp is on amp flashing Ignition on amp 2 3 MPH dur CL Pin 17 AL On steady if Active Continuous D433 HIGH BEAM BLU 469nm SAE J1362 414 1 CL Pin 20 ON ActiveHigh None UM LRedstopl amp i ik ms EUN Continuous 1 D410 STOP ENGINE RED 610nm Text Stop Engine Value 100 lamp is PGN64892 on steady See DPF PIM D424 WAIT TOSTART GRN527nm Text Wait To 1939 PGN65252 ON 01 NONE 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 APPENDIX 625 e BLUE BIRD D3 F SERVICE MANUAL 110715 F 02 19 09 Page 20 69 Start PIN 36 ON Active Low 11939 DM 1CheckTr
83. wakeup Input 1 M ulti Functional Input J 1850 SAE 1850 Data bus ue SD 672 2009 Any reproduction of this document whether total or partial without the written consent of ACTIA is forbidden 1 BLUE BIRD APPENDIX INSTRUMENTATION 110715 F 02 19 09 Page 67 69 15 APPENDIX B 15 1 Service Set Odometer Feature Warning U S Federal Law requires that the odometer accurately display the vehicle s actual mileage It is the responsibility of the person installing the Cluster to make sure the mileage programmed into the odometer correctly matches the vehicle s actual mileage The Service Set feature allows the season odometer to be set by the service technician installing a new cluster into a vehicle The odometer value is programmed using the front panel buttons and no other tools are necessary When the Cluster is powered up the LCD will display the fact that this is a Service Set Gauge and the odometer must be set The Cluster will function in a limited mode until the Odometer has been set A ccess to the set feature is controlled in the EEPROM and is secured using a four byte code that prevents accidental access to this feature 15 2 Limited Function All gauge pointers will sit at zero position and not operate prior to setting the odometer while the LCD will only show the Service Set messages All other parts of the system will operate Warning icons located in the warning modules and in gau
84. warning lights or brake interlock re quest Another mode of operation is the Start Up Mode This mode is entered when the iginition is turned on When the start up mode is initiated the cluster will go through a functional diagnostic test if the self test option is enabled default Dur ing this test you will see the gauge pointers drive to zero position pause then move 603 to half scale pause and then move to full scale pause before returning to the zero Air Brake Warning Bank r Speedometer Pressure Gauges Tachometer Warning Bank BRAKE BRAKE AIR R CRUISE BRAKE PRESSURE MIL STOP ENGINE ENGINE WARN Coolant Temp Gauge Oil Pressure Gauge Fuel Gauge L Information Display Screen ACTIA 1 APPENDIX BLUE BIRD 0 604 0 BLUE BIRD SERVICE MANUAL position and finaly going to the commanded position During this time all warning lights will perform a lamp check by turning on for 5 seconds and the three differ ent audible tones will be checked by turning on for 1 second During this start up mode the microprocessor also monitors all the inputs If a problem is detected an error message will be displayed and the gauges will wag to flag the communication failure The Ignition Mode is the normal operational mode of the system and is active as long as the ignition switch is on When the ignition is turned off the microproces sor will zero all gauges except

INSTRUMENTATION - Central States Bus Sales, Inc.

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