DigiData (FUEL/AIRDATA COMPUTER/INDICATOR) P/Ns: 912802-A 912802-03A 912802-03A-G INSTALLATION MANUAL REV M Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 USA Sales: (800)-328-0584 Technical Support: (800)-388-2849 www.shadin.
IM2803 FILE: IM2803MG.DOC, DIR: 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M Page: i of v PAGE CONTROL CHART SECTION NO. 1.0 2.0 DESCRIPTION PAGE REVISION LOG v OVERVIEW 1-1 1.1 1.2 1.3 1.4 1-1 1-1 1-2 1-2 The Manual Product Information System Configuration DigiData, Argus Moving Map Configuration FUEL AND AIRDATA SYSTEM SPECIFICATIONS 2-1 2.1 2.2 2.3 2.4 2.
IM2803 FILE: IM2803MG.DOC, DIR: 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M SECTION NO. 5.0 DESCRIPTION Page: ii of v PAGE INSTALLATION PROCEDURE 5-1 5.1 5.2 5.3 5.4 5.5 5.6 5.7 5.8 5.9 5.
IM2803 FILE: IM2803MG.DOC, DIR: 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 10.0 Drawing No. 4005-483 Page: iii of v INSTALLATION DRAWINGS AND INSTALL KIT PARTS LISTS Description/Part Number Installation, DigiData, Hi/Lo Freq. Input TTL FF P/N 912802, Page 1 of 2 DATE REV 05/06/99 E 4005-479 Installation, DigiData, Hi/Lo Freq.
IM2803 FILE: IM2803MG.DOC, DIR: 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 10.0 Page: iv of v INSTALLATION DRAWINGS AND INSTALL KIT PARTS LISTS (continued) Drawing No.
IM2803 FILE: IM2803MG.DOC, DIR: 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M Page: v of v REVISION LOG REV.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 1.0 OVERVIEW 1.1 The Manual Page: 1-1 This manual is designed to facilitate the installation of the Shadin DigiData (FUEL/AIRDATA COMPUTER/INDICATOR). 1.2 Product Information The Shadin DigiData system is designed to provide a combined source of fuel and airdata. The data can be viewed on the DigiData, a navigational receiver or both.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 1.3 Page: 1-2 System Configuration The DigiData is a panel mounted indicator, which communicates with a navigational receiver via the serial port. It is also connected to the pitot and static lines, OAT probe, fuel flow sensors and the aircraft heading source.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 2.0 FUEL AND AIRDATA SYSTEM SPECIFICATIONS 2.1 Input Data Range Pitot Static OAT Heading Fuel Flow K Factor 2.2 20 to 350 kt. -1000 to 50,000 ft. -60°C to, +60°C 0 - 360° 1 to 450 GPH Range Selected 500 to 130000 PPG Continuous Output Data Range PARAMETER IAS P.ALT P.ALT P.ALT P.ALT P.ALT P.ALT P.ALT P.ALT P.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 2.5 Page: 2-2 Output Data Electric Format: RS-422 or RS-232 2.5.1 Serial Output Data Parameters Fuel Group L. ENG. Fuel Flow R. ENG. Fuel Flow Fuel Used Total Total Fuel Used Fuel Used L. ENG. Fuel Used R. ENG.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 2.6 Limitations 2.6.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M Page: 2-4 2.6.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA Rev: M P/N 912802-A, 912802-03A, 912802-03A-G Page: 2-5 2.6.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA Rev: M P/N 912802-A, 912802-03A, 912802-03A-G Page: 2-6 2.6.4 SSEC/PSEC LISTING (Continued) Falcon 50 SSEC Airplane Flight Manual, Section 5. Performance Page 5.25.2 DGAC approved Copilot (for A/C equipped with one ADC) Revision 24 PSEC Airplane Flight Manual, Section 5. Performance Page 5.25.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA Rev: M P/N 912802-A, 912802-03A, 912802-03A-G Page: 2-7 2.6.4 SSEC/PSEC LISTING (Continued) Raytheon Hawker HS125-3A (SSEC only) Airplane Manual, Document No. H.S.1.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 2.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 3.0 CERTIFICATION TSO-C106, TSO-C44a Environmental Categories RTCA/DO-160B Temp. ALT Temp.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 4.0 Page: 4-1 PLACING AN ORDER Please know the aircraft year and model number, its serial number, and the engine make and model number when you call to place orders. Information on the fuel flow system previously installed in the aircraft and any communication interface (RS-232 or RS-422) information may also prove useful.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.0 INSTALLATION PROCEDURE 5.1 General Page: 5-1 All work must conform to AC43.13-1B or later. 5.2 DigiData Panel Location Selection The DigiData should be panel mounted in a dry, temperature stable location with enough distance from motors, pulse generating equipment, relays and cables carrying high DC or AC current.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.4 Page: 5-2 Mounting the OAT Probe 1. Refer to Drawing 4028-005 and OAT Probe Assy Kit 681201-1. Use the supplied stiffener to support the probe. Keep the probe away from transmitting antennas and static ports to avoid interference. 2. Refer to Drawing 4028-207: +5V is supplied to the OAT probe from (red wire) P3:8. The OAT signal is the white (or black) wire from P3:9.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.5 Page: 5-3 Connection to the Fuel Flow Sensor 1. If the aircraft is not equipped with a fuel flow source, refer to the STC covering the installation of the fuel flow transducer on the engine. 2. When connecting to any fuel transducer, Shadin recommends using a 3 conductor, 22 gauge, shielded wire with the shield terminated at the DigiData only. 3.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.6 Page: 5-4 Connection to the Heading Source The system is designed to interface with any ARINC-407 heading system (X,Y,Z) with no effect on the heading system or the bootstrap. Use Drawing 4005-479, 4005-548, or 4028-A24 and the table below when connecting to the bootstrap.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.7 Page: 5-5 Connection to the Pitot and Static Lines The pitot static line should be cut and a tee is installed to tap into these lines. Use the appropriate type of fittings to match the type installed in the aircraft. Use approved practices when installing these lines and perform a leak check before returning the aircraft to service.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 5.8 5.9 5.10 Page: 5-6 Connection to the Navigation Management System 1. Use the appropriate installation wiring diagram (4028-A19 or 4028-A21) to connect the DigiData Connector P1 to the navigation management system. 2. Keep the cables away from power cables, DME and transponder cables. 3. Refer to the specific Nav Receiver Installation Manuals for details.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 6.0 Page: 6-1 BASIC OPERATING INSTRUCTIONS 1. For a complete set of operating instructions consult the DigiData Operating Manual P/N OM2802. 2. Power the DigiData and the Navigation Management System. 3. After the warm-up period density altitude and PALT are available. IAS will be available but will be out of range until actual airspeed is available.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M 7.0 Page: 7-1 INITIALIZATION 1. The DigiData is preprogrammed (Initialized) prior to shipping. If changes are required in the DigiData setup, use Drawing 4028-716 to create a configuration harness (“Loop-Back” harness). Refer to the Operating Manual P/N OM2802 and the Tables listed in section 9 of this manual for programming instructions.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA Rev: M 8.0 P/N 912802-A, 912802-03A, 912802-03A-G MAJOR COMPONENTS OF THE SYSTEM 1. DigiData. 2. Outside Air Temperature Probe Assembly, SHA P/N 681201-1 3.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL 1 DIGIDATA Rev: M 9.0 P/N 912802-A, 912802-03A, 912802-03A-G Page: 9-1 CONFIGURING THE DIGIDATA The DigiData Fuel Airdata Computer comes configured from the factory for a particular installation. The procedure contained in this Installation Manual is for software versions 93.10.75 and above. 9.
IM2803 IM2803MG.DOC., DIR.
IM2803 IM2803MG.DOC., DIR.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA Rev: M P/N 912802-A, 912802-03A, 912802-03A-G Page: 9-4 SSEC and PSEC Selections Table The following SSEC and PSEC corrections and available for the following aircraft with the listed DigiData software versions. If your aircraft model is not listed in Table 2, select “no correction”.
IM2803 IM2803MG.DOC., DIR. 912802 Shadin Avionics INSTALLATION MANUAL DIGIDATA P/N 912802-A, 912802-03A, 912802-03A-G Rev: M Navigational Receiver Types Below find a listing of the DigiData input / output selection definitions.
IM2803 IM2803MG.DOC., DIR.
• NOTES: .&. £ Pla3, TRANSDUCER PO\JER FOR LEFT AND RIGHT ENGINE. FOR SINGLE ENGINE APPLICATION USE P111S LEFT FUEL FLO\J DIGITAL SIGNAL IN ONLY. l~ • DRILL #18 (4) Pi- MALE 'D' CONN. INDICATOR 1 2 3 4 5 6 7 .~? \ 'j,S ;~~ eJ))' • 8 9 10 11 12 13 14 15 +28V DC INSTRUMENT PO\JER INSTRUMENT GROUND FLO\J TRANSDUCER PO\JER (+12V OUT) NC TX, RS-232 COMM.
• I 3.300 •I • I· 3,300 •• 7,600 I I ~ ¢3.l4 HEADIN·G 1/ -STATIC OAT -- NAVIGATIONAL RECEIVER DIGIDAT A -- RS-232 / -- 422 - iI\ r FUEL FLOw 9904/038 I E I 5/6/99 I PAB I pg IREMOVED 'LEFT' REV. I PAGE r. 'RIGHT' FROM FACEPLATE 'VIEIJ, ADDED LOGO, SIJITCH BOOTS, AND BEZEL SCREIJ 9807/021 D 7/30/98 PAB KCL IREMOVE SPECS,. ADD DIMENSIONS 9605/020 C 5/15/96 \IMP RR ICORRECT lAS, P.
·'r-=== 2,500±02 ~ DRILL fll~-+) PL MALE uD" CONN, 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 2.500±.02 +28V DC INSTRUMENT PO\JER INSTRUMENT GROUND NC NC TX) RS-232 COMM, TX) SDA+ RS-422 COMM. RIGHT ANALOG FUEL FLD\J IN (-) TX) SDB- RS-422 COMM. RX) SDA+ RS-422' COMM, GROUND GROUND RX) RS-232 I SDB- RS-422 COMM, RIGHT ANALOG ,FUEL FLO\J IN (+) "LEFT ANALOG FUEL FLO\J IN (-) LEFT ANALOG FUEL FLO\J IN (+) P3) HEADING I 1 4 5 6 ® ® ® ®0 7 STATI 8 9 0® O,A,T.
I • 3.300 I .. I· 3,300 • 7,600 , @. (l)3.14 HEADING PIToT STATIC t DIGIDATA OAT RS-232 / 422 NA VIGA TIONAL RECEIVER FUEL FLOW' DRAVING-DATE 7/30/98 r---r-----.....,;,------------------------------1 APPRDVED 1----.---"""'T"---..r__ REMOVE 'LEFT'S. 'RIGHT' FROM FACEPLATE VIEW', ADDED LOGO, SW'ITCH BOOTS, AND BEZEL SCRE'" 7/30/'38 I PAD KCL IBASELINE RELEASE ALIe. FIL~C~AHE SHA.IJ./H MINNEAPOLIS. MN 55426 INSTALLA TION DIGIDA TAl ANALOG FF GREY FACE I I 1280203GAJ.
• • DRILL #18 (4) l/2~ .ll? N ~ \ 7,0J~~\ o o 0::>' 10 N U EB PI, MALE 'D' CONN, INDICATOR 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 +28V DC INSTRUMENT POW'ER INSTRUMENT GROUND NC NC TX, RS-232 COMM, TX, SDA+ RS-422 COMM.
• o • ,0 ' 1. • THE CONVERTER CAN BE MOUNTED IN ANY ORIENTATION 2, 4' SPACING IS REQUIRED ABOVE CONNECTOR 3. NO COOLING IS REQUIRED 2,94 (3.18) 4. THE CONVERTER CAN BE INSTALLED IN A PRESSURIZED OR NON-PRESSURIZED AREA, PROVIDING TEMPERATURE DOES NOT DROP BELO'vl -20°C 5. 1 AMP CIRCUIT BREAKER IS REQUIRED 6. NO SHOCK MOUNT REQUIRED 7, USE HARD'vIARE PROVIDED IN .INSTALL KIT PIN IK9337 TO ASSEMBLE MArING CONNECTOR.
• I. • 5.228 • -I ~ Th J1: C J1: A J1: 8 CONNECTIVITY TABLE PIN A B C J1 FUEL FLOW POWER INPUT FUEL FLOW SIGNAL FUEL FLOW ,GROUND J2 AC FUEL FLO,W SIGNAL AC FUEL FLOW SIGNAL N/A NOTES: 1. ALL DIMENSIONS FOR REFERENCE ONLY. SHAD/IV NINNE~OUS. I.lN 55426 INSTALLATION, SINE/ SQUAREWAVE CONVERTER ADDED OlNENSlONS at ISONElRIC VIEW: REORAYtt4. BASEUNE RElEASE DRAWING NO. 4005-642.
• • • NOTES: 1. REFERENCE PIN 681201-1 OAT PROBE ASSEMBL Y KIT 2, AVOID INSTALLING OAT PROBE IN OR NEAR: PROP AIRSTREAM ENGINE EXHAUST FLUW PATH ·CABIN HEATERS EXHAUST FLOW PATH TRANSMITTING ANTENNAS (DME, TXP, COMM,) DARK PAINTED AREAS .& OAT PROBE, PIN 681201 & TORQUE NUT, FN 25, TO 1.3 IN-LBS (MAX) @& 10 )4X DRILL 0:098¢ AIRCRAFT FUSELAGE (#40) 4 PL DRILL 0.359¢ o 30 (23/64") DETAIL A MOUNTING HOLE DETAIL ~~;f~;IO~1H~~~I~~ ~~~fs Ut<~~~NJ91UAIt.
• Report: ECO Date: Rev: Sec.: • 40320 April 4, 2007 H IX Page 1 of 1 Shadin Avionics /0 511201 543216 670503 670504 670505 670506 681201 /5 20 25 30 35 40 681201-1 1-- IJ- ~ QTY. 4 I I 1 1 1 1 DESCRIPTION RIVET, AN4703-4 or MS20470AD3-4 OAT STIFFENER RING SHIELD, Temp Sensor Assy NUT, Temp Sensor WASHER, Flat OAT W ASHER, Shoulder OAT OAT PROBE 10 items MFG. SHA SHA SHA SHA SHA SHA MFG.
• Report: ECO Date: Rev: Sec.: • 4028A June 5, 1997 IX Page 1 of I Shadin FILE NAME: IK9128-P.DOC DIRECTORY: IKXXXX ECO# Release date: Approved: 5 10 15 20 25 30 35 40 45 50 PIN 230018 230020-4 230036 230038 230019H-I 511002 512007 541001 PKI002 PKI005 QTY. 1 1 1 I 4 4 4 4 1 1 DESCRIPTION CONNECTOR, 9 Pin D-Sub HOOD 9 Pin D SUB Cinch CONNECTOR, 15 Pin D SUB Socket CONNECTOR, Hood 15 Pin D SUB LATCH Clip Modified SCREW, 4-40XI/4" Phil Pan HD SS NUT, 4-40 3/16XlI16X.062 SS WASHER.
• • ' GARMIN 430 GARMIN 530 P4001 P5001 912802 912802-03 912802-03-G BENDIX! KING BENDIX! KING KLN90 KLN90B KLN89 GARMIN LNS 150. 155. 155XL. 165. 250. 250XL 300. 300XL 6000 BENDIX! KING FOSTER IIMORRO'w' 360 7000 IIMORRO'w' NMS2001 IIMORROV 820 KLN 900 IIMORROV GX 50. 60 ARNAV FMS7000.
• • 912802 912802-03 912802-03-G • PI 1\ / ,-, RS232 RX 12 RS422 RX+ 9 RS422 RX 12 RS232 TX \ ' I ,'f NAVIGATIONAL & ¥ : RECEIVER ¥ & &. ,,-, RS422 TX+ IS I RS422 RX+ \ I I I RS422 'rX RS232 RX 1\ 5 8 RS422 RX ~ '- J1 , I I .p IN 937000-03 12 RS422 RX 11 RS422 RX+ I ~ \ j .r..
• I • .~. 912802 912802-03 912802-03-G TRIMBLE TRIMBLE NORTSTAR 1000, 2100, MIA 2000, 2101. 3000 3100 RX, SDA+ RX, SDA+ • '. '. M2 M3 60/600 P1 1""\ /-, I RS-422 TX, SDA+ \ \ I I 6 \ \I I I I I I I I I I I I I I I I I , , 8 I I I ) I \ I I 9 RX, SDB RX, SDB 4 8 IX, SDA+ IX, SDA+. IX, SDA+ 15 37 11 TX, SDB TX, SDB TX, SDB 3 5 6 . \\ I I I I I I I I I I I I I I RS-422 RX, SDB 7 N/A I .
• +~ /1 -+ ~ ill - fUEL FLOW TRAHSlolITTER ~ H .& SIGNAL CONDI1lONER +~ - A I /1 - - fUEL flOW INDICATOR +9 ffi FUEl.. FLOW TRAHSlolITTER +~ & H I /1 + . • LEFT ENGINE SIGNAL CONDl11ONER /"1 ~~ & A & FUEL FLOW INDICATOR & RIGHT ENGINE SIGNAL CONDI11ONER NOTES: ill ffi DICITAL/FREQUEHCY 912802 & P1 GROUND RIGHT FUEl.. FLOW LEFT FUEL FLOW 2 SlG GND 10 +12Vdc "- \ I v 15 GND 11 , , I \ I \ II I , W \ I R ENGINE \. .
• ~.:----------. .~ HIliH LEVEl.. FUEL FLOW' OPTION CHI/LO FREQ INPUT TTL> 1. 912802 P1 GROUND ~ P3 I- I, DAT [ 5::1 : RIGHT FUEL FLO'W 26V 400Hz Y +SIG -siG 1141 .$IG 15. 9602/050 9502/007 9409/004 n/o. n/o.
i • • • NOTES: .& \-lIRE: £ \-lIRE: SH~ELDED 2 CDND , MIL -C-27500-22TG2T14 3 CDND , SHIELDED MIL -C-27500-22TG3T14 ~SHIELD SHOULD BE CONTINUOUS GROUNDED BACK TO DIGIDATA. DIGITAL/FREQUENCY 912802 PI ~-_ GROUND RIGHT ~~~ LEFT ~~5~ { -~ _ SINE IJAVE FUEL FLOIJ PICKUPS .. 2 t--e::Jo:-----, +12V 3 SIG 'GND 13 10 SINE TO SQUARE 'WAVE CONVERTER SHADIN PIN 631201 R. ENGINE SINE TO SQUARE IJAVE < SIG 115 GND 11 CONVERTER 'SHADIN PIN 631201 ................................. __ ..
• • • NOTES: 1 CONSULT OPERATIONS MANUAL FOR DIGIDATA PROGRAMMING INSTRUCTIONS. PI +28VDC I 1 GND 2 TX J RS232 I 5 RX J RS232 I 12 ---L :.:~~ [DRAlJING DATr-1 2/23/96 _--,----,-_--r_,-...... crUA nrw JJ~.t1.u1J HINN£APOLIS, HN 55426 ::RDr::D "HP INST ALLA TION \JIRING ~------___1~"":'T':":':;=SES::....t LOOP BACK HARNESS DRA'JING NO. SIZE P/ N 4028-716 A J REV ------ .
------=,....--------------------------_. . ------------------------- o-sue: ~12802~'·.· 12l102-03-C ;« ~"D r-. (;ROUND /1 12 t-e::::k ....L -SIC +SlG ;===1~ I'cd 13 & ' PART NUW8ER . NUW8ER 101-384153-1 PC900-XAXXXXPH ~,-e). (A,.). (1,2). OR llC)- 38()()()8-~ \ I DC RIGHT FUEl FlOW /1 PART NUWIIER llC)-38()()()8- 2 OR 101-384153-3 ;==1~ '-. -9J + & CUR't€D PC9OO-XAXXXXPH ~P_~.~ (1 -8). (A,.). o. PC9OO-XAXXXXPH ~PAAT~~ (A,.), (1.2)~7.8), FAa:) (CUR~,Jn.
~.~ -. I P13 P76 J5G P5G f------.,. SIGNAL V 'vi ~ EO.8A20 E06A20 GROUND U E05A20 R/H • =ill'vl= GND 8 i11P-- T E08B20 E06B20 -------lE S E05B20 - - - - - - - l C E04A20N G r- B I-- K J I L '- l=l L:I Z .. 0:: 0:: L:I CI) F IADC-200, PIN 962810-3, PIN 962820-3. £ F IADC-2000, & DIGIDATA PIN 912802-03 PIN 912802-03-G P IN 962830-3, P1 J1 .,.------, 3 -+-'1-------1 2 L----~r-------1 1 --r=r---I10 +----,1---1 9 GROUND RIH SIG. R/H SIG.
/-. PIO02 ,7. A I PC048 r------. R/H CFUEL FLO\J P.C.BJ :t2 SIGNAL GROUND • \.J 12 14 l-J-- I + 8 8' V? V? ~ ~ F IADC-:-200, PIN 962810-3 PIN 9.62820-3. £ & F I ADC-2000, PIN 962830-3. P1 J1 3 -(-t-----1 2 L------'=':f-----1 1 ---r=........----110 --t-+-----1 9 ~--, r- I- DIGIDATA PIN 912802-03 PIN 912802-03-G GROUND R/H SIG. RI H SIG. L/H SIG. L/H SIG. 11 GROUND 13 R/H SIG. 7 R/H SIG. 15 L/H SIG. 14 L/H SIG.
~07 ' . FUEL'l',wNITOR
., .' & RIGHT ENGINE F IF IND. P080 •. F IA'DC-200 PIN 962810-3 PIN 962820-3 & FIADC-2000 PIN 962830-3 Jl SIG. -Ip 111 GROUND M I . SIG. +1 L~ LEFT ENGINE F IF IND. SIG. - ENGINE I II ~ DIGIDATA PIN 912802-03 PI ~I : J 2 SIG + FUEL 3 GROUND .1 J --------------1.;. ----~ 131 R. SIGNAL + FLO'w' P079 ~I I W----P: I P SIG. + I L 1 J j 9 SIG I 10 .SIG + ~ > LEFT ENGINE FUEL t---------------~---~ 14 I L ' I I I I ---------..;-----tj-----! 15 I L.
". .,. '-' ~ ~ r. ~i SIG.+IK~ ,'-'" SIG. -IL I I .1 I SIG ~ 21 SIG I I I - } + 3 GROUND ~I-- ill F/ADC-2000 PIN 962830-3 Jl RIGHT ENGINE FUEL FLOV INDICATOR 'e· - F I ADC-200 PIN 962810-3 PIN 962820-3 RIGHT ENGINE FUEL DIGIDATA PIN 912802-03 PI, t--------------- / 1 1 1 IGROUND ---------------D-----I- I R. SIGNAL ~ 7 - -- SIGNA~ 131 R. + FLO'v/ LEFT ENGINE FUEL FLOV INDICATOR ~. SIG.-IL~ SIG.
• • F/ADC-200 PIN 962810-3 PIN 962820-3 ~ & Jl RIGHT ENGINE FF INDICATOR 1 SIG-} RIGHT ENGINE 2 SIG + FUEL FLO'w' 9 SIG - } LEFT ENGINE m LEFT [ A ENGINE FF INDICATOR , FI ADC-2000 PIN 962830-3 PIN 962830-3-S-5 3 GROUND ~ ... I : :! i : ! 10 SIG + mE RAGEN PIN 3265013-0601 ' FUEL FLO'w' • : £ Jl I FIADC-2POO PIN 962830A-3 -----{-+---~ 43 I R. SIGNAL 1,1 -----!::.~---~ 24 I R. [----r----,26I ---- J---~ SIGNAL + L. SIGNAL ,12 I L.
• •• SHADIN PIN 912802 OR 912802-G SHADIN F/F ~-- "' .ill +28VDC INSTRUMENT PO'WER 1 SHIELD/INSTRUMENT GROUND 2 FUEL FLO'W TRANSDUCER PO'WER 3 LEFT FUEL FLO'W SIGNAL 15 LEFT FUEL FLO'W GROUND 11 L..c::k..
DIGIDA TA '.~L/FREQUENCY SHADl .~ 912802 DIGIDA TA • SHADIN P/N 912802-0 & +28VDC INSTRUMENT POW'ER 1 SHIELD/INSTRUMENT GROUND & JG .
