Wiring Diagram for Cessna Citation X+

ICAS IT DOUBLER ROUTING MOD = LTN DET INSTL - STØ AVN GNDS TRAY INSTL – PNL WIRE FEEDTHRU INSTL-FWD BHD FWD_BHD_ || 9564002–18] FEEDTHRU INSTL - 1003–32| 004-34| 005-6 FEEDTHRU IN$11 - "L/MID_BHD FEEDTHRŲ INSTI – R/MID BHD] MID BH↑ COAX FEEDTHRŲ. QUANTITY STD OPT SER CL I ECR EC 039266 EC 039266 1 | EC 039266 9554002-66 ■ EQUIP INSTL – CVR A200S 9554011-1 9554011-3 9554011-8 9554012-1 | 9554012-2 9554013–1 ■EQUIP INSTI EQUIP. INSTI “STANDARD NOSE TRS COMP EQUIP INSIL - TÁC TỶ 100 EQUIP INSTL - COMM 17DTV XPDR ■EQUIP INSTL - COMM 2/DTV XPDR_ ■EQUIP INSIL SELCAL RCZ-833E RCZ-833E CSD-714 | 9554047-S | EQUIP INSTĽ MAGNASTAR C-2000 1.9556000-16 9556006-1 9559018-2 9559027-1 9560006-1 ENSTL – PANEL SUPPORT STRUCTURE INSTI - BAG COMPT ■ EQUIP INSTI - AFT PEDESTAL ■ EQUIP İNŞTL - FWD PEDESTAL INSTU NOSE COOLING 4 CIRCUIT BREAKER INSTALLATION QUANTITY DRAWING NO SYSTEM STD OPT SER 6718124-9 RH CB PANEL INSTI 9518010-6 SIBY NAV/COM 9518010-14. DIGITAL PHONE 9518010-31 HF 2 9518010-33 9518010-37■ GPS 2 SELCAL 9518010-56′| TCAS || EC 039266 9518010-57 | GPWS W/WIND SHEAR 9518010-75| CVR 1 9518010-86 | LIGHTNING DETECT 9914572-6 RH CB PAÑEL E/L PNL REVISIONS [ZOKE]LTR] DESCRIPTION DATE APPROVED DATE DRAIN GROUP CHECK SECT PROJ M.E. 01/27/99 A WESTHOFF TEED MUTH FACE TOMATORE CARICATE PER PROCEER PR WE TEAMMATION PER FOLL cpp 1COM WICHITA K CITATION X AVIONICS INSTALLATION KIT 750-0094 |B- 0001 1.9.3 TỶ. D 71379 9580094 CITATION. X=112 OF CESSNA FOR 146 EC670094 9580094 D C ) COMM/XPDR UNIT SYSTEM SYSTEM | 1 NAV UNIT SYSTEM SYSTEM 02 1 JUMP CUT 2 JUMP JUMP [ZOME|LTR|| REVISIONS DESCRIPTION IAC INSTALLATION MODULE W SYSTEM SYSTEM JUMP JUMP | SYSTEM | SYSTEM M W 2 2 $1 JUMP JUMP JUMP JUMP JUMP JUMP JUMP JUMP JUMP 53 5 55 CUT CUT JUMP 52 JUMP JUMP JUMP CUT CUT JUAP CUT 2 JUMP JUMP JUMP 3 EVEN PARITY 3 JUMP CUT >>> ་ ODO PARITY ་ CUT JUMP 5 JUMP JUMP S JUMP JUMP B JUMP JUMP 58 JUMP JUMP В JUMP JUMP CUT JUMP 7 CUT CUT 57 JUMP 9 JUMP JUMP JUMP JUMP 58 CUT JUMP CUT JUMP JUMP 7 JUMP JUMP CUT CUT 39 JUMP JUMP 9 10 JUMP JUMP 60 JUMP JUMP 10 11 CUT CUT 61 JUMP JUMP 1 JUMP JUMP 13 JUMP JUMP 14 JUMP JUMP 15 JUMP JUMP 18 JUMP JUMP 17 JUMP JUMP 18 JUMP JUMP 19 JUMP JUMP 20 JUMP JUMP 62 CUT CUT |63|| JUMP ||| JUMP 64JUMP 13 JUMP 21 JUMP JUMP 22 JUMP JUMP |23| JUMP | JUMP 65 JUMP ||JUMP 65 JUMP JUMP 67 JUMP JUMP 5.8 JUMP JUMP 69 JUMP | JUMP 70 JUMP JUMP 71 JUMP JUMP 72 CUT CUT 73 JUMP JUMP 74 CUT CUT 75 JUMP | JUMP 78 JUMP JUMP 77 CUT CUT 78 CUT CUT 79 JUMP JUMP 13 16 1B AIRCRAFT'S MODE S CODE 24 25 CUT JUMP 26 JUMP JUMP 9 JUMP 10 CUT JU 11 CUT JUMP 12 JUMP JUMP 13 JUMP JUMP 14 JUMP JUMP 13 CUT JUMP 15 JUMP JUMP 17 CU1 JUMP 18 JUMP JUMP 19 JUMP 20 JUMP CUT JUMP 21 CUT JUMP 22 CUT JUMP 23 JUMP JUMP JUMP JUNE 8 CUT JUMP JUMP C DATE APPROVED 24 OUT CUT 25 CUT CUT 26 JUMP JUMP 27 CUT CUT 26] CUT CUT 29 JUMP JUMP 30 JUMP JUMP 31 CUT CUT 27 JUMP JUMP 28] JUMP JUMP 29 JUMP JUMP 80 JUMP JUMP 30 30 JUMP JUMP $1 CUT CUT 31 31 CUT CUT 32 JUMP 33] CUT JUMP CUT 02 JUMP JUMP 83 JUMP 32 32 JUMP JUMP JUMP 33 CUT CU1 33. CUT CUT 34 CUT CUT 34 CUT CUT 34 JUMP JUNE 35 CUT CUT 56 JUMP JUMP LIGHTNING SENSOR 35 JUMP JUMP 36 JUMP 35 JUMP JUMP JUMP 36 JUMP JUMP 37 JUMP JUMP 37 JUMP JUMP 37 JUMP CUT 51 8 30 JUMP JUMP 38 JUMP JUMP 38 JUMP CUT 8 39 CUT CUT 59 JUM JUMP 39 CUT JUMP 53 40 JUMP JUMP 40 JUMP JUMP 40 JUMP $4 F 41 JUMP JUMP 41 JUMP ||JUMP " CUT CUT 42 JUMP CUT JUMP JUMP JUMP 42 JUMP CUT SYSTEMS CONFIGURATION & STRAP PROGRAMMING 9580094 D 43 CUT CUT 43 OUT CUT 43 JUMP JUMP ·་ CUT CUT ་་ CUT CUT 44 JUMP JUMP 43 JUMP JUMP 451 CUT CUT 48 JUMP JUMP 16 JUMP JUMP 46 JUMP 47 CUT CUT 47 JUMP JUMP 48 JUMP JUMP JUMP JUMP 49 JUMP JUMP 19 JUMP JUMP 49 JUMP JUMP 50 CUT CUT 30 JUMP JUMP 50 JUMP 45] JUMP JUMP JUMP |47|| JUMP | JUMP 48 JUMP JUMP JUMP DATE DRAB GROUP N.E. FAIRY P PROCES 01/27/99 A WESTHOFF THORIZED SNATURE RAGE TION PR TITLE: CROW't con MRCRAFT DIVISION P.0.80 1794 STA 67277 CITATION X AVIONICS INSTALLATION KIT 750-0094 SIZE COD IDEAT 40. D 71379 མ 9580094 CITATION X 3 OF 3 CESSNA FORM 1466A EC670094 CHECK SECT PROJ .. 100 GPS 1 AHRS 1 AH-840 29 号 T FMS CDU 1 CD-810 00000005 DOODO DO OOOOOO0 422 MADC AZ-840 T 429 429 DAU 1 DA-800 6 DU1 PFO ODABO OOOOOOO DISPLAY BUS DISPLAY BYSİ------------ T 1 ○ ☐ ☐☐ REV CTRL I RC-840 TX ANT WU-870 INST RMT CTRL 1 A1-871 . JAC 1 IC-800 DSP CTRL I DC-840 DU3 QU4 T DU5 EICAS MFO PFD OOOOOOO DISPLAY BUS DISPLAY BUS DSP CTRL 2 DC-840 T FMS COU 2 CD-810 ○ ○ ☐ ☐ O gº ☐ ☐ ☐ ☐ EIGAS CRTL RC-541 |000 ° WX CTRL DC-874 GUIDANCE CTRL GC-810 • BACKUP 2 ASCB BACKUP_1. WX HAP 422 LINEAR ACT 1 SM-725 SERVO SM-200 ELEV SERVO SM-200 AIL PRIMARY ASCU PRIMARY RSB DIGITAL AUDTO BUS RMU 1 RM-855 ADF ANT AT-860 NAY S RHZ-851 CLR DEL CD-850 COMM 1 RCZ-851 AUDIO PANEL 1 AV-850A OOOO DODDO T SECONDARY T AUDIO PANEL 2 AV-850A RS232 AS232 LINEAR ACT 2 SM-725 COMM 2 RCZ-851 SECONDARY REV CRTL 2 RC-840 INST RMT CTRL 2 RI-871 DO DATA LOADER DL-900 IAC 2 IC-800 IT NAV 2 ADF ANT RN2-851 AT-860 DODOD 00 422 DAU 2 DA-800 MADC 2 AZ-840 FOWJ 2 RM-855 0000 G C REVISIÖNS DESCRIPTION | DATE |APPROVED NOTES: 1. THIS DWG FILED IN CADAM FILE: RLSD,E95 THIS DWG FOR REF ONLY AND WILL NOT BE KEPT TO DATE 3. T TERMINATION RESISTOR BLOCK AHRS 2 AH-800 RAD ALT ANT AT-300 RAD ALT ANT AT-300 RAD ALT R7-300 CPS 2 (T T 9500100 GLAM 01-14-94 MESTHOFF OR₤4 SEE SEPARATE PARTS LIST CESSNA AIRCRAFT COMPAN AIRCRAFT DIVISION _ P.D. WICHITA, KANZAS 67277 P2000 SYSTEM BLOCK DIAGRAM CC: F 71379 9500100 THE VERTE NO. ATITINY, [KOLE: NONE EC35048 b MCICNT [T SECT PROJ OTHER 4 с ZONE LTR REVISIONS DESCRIPTION B REDRAWN WITH CHANGES: ADDED STRAP #84. DESCRIPTION WAS "RESERVED" FOR STRAPS #57,#62, #63, & #64. EC 041846 DATE APPROVED 12-04-98 CAR LH RH JAC INSTALLATION MODULE STRAPPING_ DESCRIPTION JUMP JUMP NUMBER OF ASCB |[JUMP JUMP]]] ATTITUDE SENSORS ||JUMP| JUMP]| NUMBER OF AIR 4 JUMP JUMP DATA UNITS CHINING SENSOR NUMBER OF EFIS/FWC LACS 8 JUMP JUMP AFCS IN TAC MPINUM?] FMS IN IAC (HONEYWELL } JUMP POR NUMBER OF FMS UNITS NUMBER OF ASCB GPS UNITS ARINC 429 LONG RANGE SENSOR #1 CONFIGURATION ARINC 429 LONG RANGE JUM: SENSOR #1 NUMBER |JUMP|| NUMBER OF AUTOPILOTS. P JUMP AF IS INSTALLED JUMP JUMP 123 JUMP JUMS 1241 CUT CUT ARINC 429 LONG RANGE SENSOR #2 CONFIGURATION 1231 CUT CUT ARINC 429 LONG RANGE 12 JUMP JUMP SENSOR #2 NUMBER 27 CUT CUT FMS OPERATIONAL MODE [28] CUT | CUT 29 JUMP JUMP ARINC 429 LONG RANGE 30 JUMP JUMP SENSOR #3 CONFIGURATION Batam CUT SHINC 429 LONG RANGE 38 JUMP JUMP SENSOR #3 NUMBER #2 DEFAULT #3 DEFAULT | ASCB SENSOR #4 DEFAULT 39 CUT CUT RADIO INTERFACE TYPE 41 JUMP JUMP NUMBER OF ATC UNITS NOTES STANDARD CONFIGURATION STANDARD CONFIGURATION CUT=|NSTALLED STANDARD CONFIGURATION ■STANDARD CONFIGURATION JUMP-DUAL CUT || CUT=FMS EXTERNAL TO LẠC CUT JUMP -SINGLE (STANDARD GPS IS NOT ON ASCB) STANDARD CONFIGURATION STANDARD CONFIGURATION JUMP–QUAL CUT=SINGLE CUT=INSTALLED STANDARD CONFIGURATION STANDARD CONFIGURATION CUT CUT CDU CONTROL STANDARD CONFIGURATION STANDARD CONFIGURATION CUT-IRS 1 INSTALLED" | CUT-IRS 2 INSTALLED. | STANDARD CONFIGURATION I STANDARD CONFIGURATION JUMP CUT DUAL XPOR LH RH 1AC INSTALLATION MODULE STRAPPING DESCRIPTION |70 JUMP JUMPI RESERVED (FLEX) [ 71 | JUK?] JUMPI STRẠP 71 NOT USED 172 JUMP JUMPI GPWS INSTALLED [73] JUMP | JUMP| FD BARS SYNCRONIZED Į VOICE WARNING DISABLE 176/JUMP UP FD BAR TYPE CONTROL 1971 CUT CUT VERTICAL PROFILE" 801 JUMP JUMP 181 CUT | CUT | 82 JUMPI JUMP 831 JUMPIJUMP [84] JUMPI JUMP #176 #15 #131 121 18 CUT CUT HONEYWELL RSB JUMP JUMP 429 JUMP JUMP 48 JUMP JUMP CUT NUMBER OF ADF UNITS NUMBER OF DME UNITS NUMBER OF MLS UNITS CUT JUMP |CUT=INSTALLED --SINGLE JUMP CUT STANDARD CONFIGURATION ---DUAL STANDARD CONFIGURATION STANDARD CONFIGURATION CITATION X AIRCRAFT SOFTWARE IDENTIFICATION NOTES STANDARD CONFIGURATION · STANDARD_CONFIGURATION | CUT=INSTALLED JUMP=INDEPENDENT JUMP-ENABLED STANDARD CONFIGURATION CUT-ENABLED STANDARD CONFIGURATION FOR ALL CITATION X AIRCRAFT 13700 0039 40] 1AC INSTALLATION MODULE STRAPPING CARD LOCATED FORWARD OF LACS IN NOSE COMPARTMENT STANDARD CONFIGURATION REFER TO AIRCRAFT'S AVIONICS KIT FOR SPECIFIC REQUIREMENTS JUMP JUMP ST JUMP JUMP 2 JUMP JUMP JUMP JUMP FMS CONTROLS UTC CLOCK FMC CONTROLS UTC CLOCK EXTERNAL UTC CLOCK TAC/WX CONTROL VIA RS-422 NUMBER OF RADIO ALTIMETERS CAT 11 ILS JUMPI CAT || MLS. METRIC FUEL/WEIGHT ENAB=CUT | SLIP-SKID (ACARS) GPWS INSTLD=CUT ELEC BUS-CUT WARN FAIL ENABLE P|JULP] HEADING KNOB SYNC JUMP] NUMBER OF RUDDER LIMITERS" | JUMP] RESERVED IJUMP NUMBER O YSAC SYSTEMS IUMPIJUMPI RESERVED. STANDARD CONFIGURATION STANDARD CONFIGURATION | STANDARD CONFIGURATION STANDARD CONFIGURATION STANDARD CONFIGURATION JUMP=PILOT/COPILOT IN SYNC JUMP-DUAL RUDDER LIMIT SYSTEMS STANDARD CONF I GURATION JUMP■DUAL YSAS STANDARD CONFIGURATION WBC THIS DRAWING FOR REFERENCE ONLY 06/22/95 DATE DRAWN • FAIRBANKS TITLE. GROUP CHECK SECT PROJ M.E. FABRICATE PER PROCESSOR TONATURE TION PER CESAFT COMPAT AIRCRAFT RIVIST WICHITA 0711 CITATION X AVIONICS SYSTEMS PROGRAMMING REFERENCE D71379 9500400 CITATION X | OF CES FOR 1466 035048 9500400 B i. NAV UNIT STRAPPING COMM/XPDR UNIT STRAPPING SEET MENT REVISIONS DESCRIPTION || DATE APPROVED W SYSTEM SYSTEM W SYSTEM SYSTEM 21 °2 el £2 1 1 SYSTEM POSITION SYSTEM POSITION 2 2 EXAMPLE OCTAL MODE-S CODE: 70612534 3 EVEN PARITY 3 EVEN PARITY OOD PARITY 4 CDO PARITY 5 ADF EMERGENCY CHANNEL 5 AOF ANTENNA POSITION 6 SQUAT SWITCH POLARITY AIRCRAFT MAXIMUM 7 7 TRUE AIRSPEED 8 ADF QUADRANTAL 8 . ERROR CORRECTION 9 315° 9 16 10 10 11 ADF 315° QEC SIGN 11 12 12 13 ADF QUADRANTAL 13 ERROR CORRECTION 14. 225' 14 15 15 50 16 ADF 225 QEC SIGN 16 17 17 18 ADF QUADRANTAL 18 ERROR CORRECTION 19 135° 19 20 20 AIRCRAFT'S MODE S ADDRESS STRAP OCTAL BINARY POSITION CUT 32 CUT 31 1 CUT 30 1 JUMPER 29 O ° JUMPER 28 37 04 25 U JUMPER 27 1 CUT 26 1 CUT 25 ° JUMPER 24 ° JUMPER 23 1 ° JUMPER 22 CUT 21 0 JUMPER 20 2 ' CUT 19 ° JUMPER 18 CUT 17 ° JUMPER 16 ' CUT 15 ° JUMPER 14 3 1 CUT 13 ㅁㅁㅁㅁ 1 CUT 12 CUT 11 4 ° JUMPER 10 0 JUMPER 9 1- CUT. 0 - JUMPER PARITY - SUM OF CUT STRAPS 1-2 & 5-50 TOTAL NUMBER OF CUTS = 17 [000 PARITY) THEREFORE CUT #4, JUMPER #3 DO NOT COUNT STRAPS 3&4 WHEN COUNTING PARITY 13 03 STRAP A1 SIDE ASSY 7510280 " 0 0 0 '50 COMM/XPDR 1 21 ADF 135° QEC SIGN 21 REFER TO PROCEDURE ON THIS SHEET 22 22 TO DETERMINE WHICH 23 ADF QUADRANTAL 23 STRAPS TO CUT ERROR CORRECTION 24 45' 24 MODE S CODE WORK SHEET 25 25 STRAP 26 ADF 45° QEC SIGN 26 OCTAL BINARY POSITION * 27 27 32 ADF ANTENNA 28 28 31 ROTATION OFFSET 29 29 30 30 ROTATION OFFSET SIGN 30 29 31 DC SIN/COS - XYZ SELECT 31 28 32 SIN/COS MAX AMPLITUDE 32 27 33 FMS INSTALLED 33 SQUAT SWITCH SOURCE 26 34 OKE 1 INSTALLED 34 ATTITUDE SOURCE 25 35 VHF COMM FREQ PAIRED 35 DLP INSTALLED 24 36 SINGLE ONE 568 SELECT 36 RESERVED 23 37 37 RESERVED 22 DHE ANTENNA PROCEDURE FOR SETTING MODE S CODE 1) OBTAIN AIRCRAFTS SPECIFIC MODE S CODE FROM THE AIRCRAFT ORDER. 2) WRITE THIS CODE ONTO THE WORKSHEET FROM TOP TO BOTTOM IN THE OCTAL COLUMN. 3) FILL IN THE 3 BINARY BLOCKS FOR EACH DIGIT OF THE OCTAL CODE. EXAMPLE - 6 EQUALS CUT, CUT. JUMPER AS SHOWN IN THE EXAMPLE ABOVE THE WORKSHEET, 4) FOR EVERY "CUT" LISTED ON THE WORKSHEET FIND AND CUT THE CORRESPONDING STRAP ON THE CARD. 5) ONCE THE STRAPS FOR MODE S CODE HAVE BEEN SET AND ALL OTHER STRAPS HAVE BEEN CUT PER THE AVIONICS KIT (SHT 3) 17 IS NECESSARY TO SET THE PARITY, PARITY IS BASED ON THE SUM OF ALL THE CUT STRAPS EXCLUDING STRAPS 3 AND 4. IF THIS SUM IS EVEN THEN CUT STRAP 3 AND JUMPER 4. IF THE PARITY IS ODD THEN CUT STRAP 4 AND JUMPER STRAP 3. 38 38 TRANSFER TONE 21 CABLE TRIM 39 LENGTH/8.13FT 39 (W37 IS LSB) RCVR AUDIO COMPRESSOR 20 10 40 EXTENDED FREQUENCY 19 11 DME-EFIS/MLS CONTROL 41 RESERVED 18 42 NAV AUX CONTROL HEAD 12 COM AUX CONTROL HEAD 17 43 DME 2 INSTALLED 43 TCAS INSTALLED 16 44 VOR ROTOR MOD FILTER 44 TCAS ANTENNA CABLES 15 INSTALLATION 45 VOR COMPASS SOURCE 45: 14 461 VOR ELECTRICAL ZERO 46 TCAS TA DISPLAY ENABLE 13 DATE 5722795 - 47 VOR OBI AC SIN/COS AMP FAIRBANKS] 47 12 48 RMI BEARING 48 11 CHECK इल RESERVED 49 RESERVED 49 10 50 RESERVED 50 9 SEE STO. SAKET CENA AIRCRAFT COMPANY AIRCRAFT DIVISION P.O. Box 770 WICHITA, KANSAS $7277 CITATION X AVIONICS SYSTEMS [PROGRAMMING REFERENCE. F71379 9500400 L ||ME 2 OF 2 EC 035048 ■ 9500400 B C. JQ901 MID PRESS BLKHD LH AVIONICS MS27474E2DF35SA CONNECTOR PQ901 MID PRESS BLKHD LH ELECTRICAL MS27473E2DF35PA CONNECTOR JQ902 MID PRESS BLKHD RH AVIONICS MS27474E2OF355A CONNECTOR PQ902 MID PRESS BLKHO RH ELECTRICAL MS27473E20F 35PA CONNECTOR 6708278 JB901 FWD PRESS BLKHO LH ELECTRICAL MS27474E20F 395 CONNECTOR 6708313 6708313 PB901 FED PRESS BLKHD LH AVIONICS MS27473E20F 39P CONNECTOR JB902 FNO PRESS BLKHO RH ELECTRICAL MS27474E20F 395 CONNECTOR 6708313 PB902 FWO PRESS BLKHO RH AVIONICS MS27473E20F 39P CONNECTOR AHRS 2 SLEW C 6708278 PEDAL POSN EXC A- 6708278 PEDAL POSH EXC A- 6708278 AHRS 1 SLEW C AHRS 1 SLEW R 6708313 AHRS 2 SLEW R 6708278 6708278 6708.313 AHRS I SLEW L 6708313 PEDAL POSN OUT A- PEDAL POSN OUT A- AHRS Z SLEW L 6708278 6708278 6708313 AHRS 1 MODE C 6708313 AHRS 2 MODE C 6708278 6708278 6708313 AHRS 1 MODE TEST 6708313 PEDAL POSN EXC B- PEDAL POSH EXC B 6708278 6708278 6708.313 AHRS 1 MODE GYRO 6708313 AHRS 2 MODE TEST AHRS 2 MODE GYRO 6708278 6708278 6708341 PEDAL POSN OUT B- PEDAL POSH OUT B. 6708278 6708278 6708241 YSAC A POWER YSAC A MOTOR_EN YSAC A ENABLE ELT POWER 6708278 6708278 6705278 YSAC B POWER 6708278 6708313 YSAC B MOTOR EN 6708278 YSAC B ENABLE 6708278 6708320 6708323 $5K ALT TRIP AVN MASTER SW EVENT MARKER SW GEAR ON & LOCK SW 6708341 6708241 35K ALT TRIP AVN MASTER S 6706243 6708243 GIA FOR AHRS 1 6708323 DAU A POWER 6708243 6708312 DAU 2A POWER 6705312 6708280 6708280 DAU 28 POWER 6708312 6708280 -429 FROM AHRS 1 6708280 DAU 18 POWER 6708312 ASCB PRI 1 6708312 ASCB PRI 15: 6708312 6708772 6708312 6708772 429 BUS TO FADECS 6708772 6708772 6708312 6708312 6708772 8708312 ASCB PRI 2—1 6708312 6708772 -429 BUS TO FADECS 6708772 6700772 ASCB PRI 2-1 6708312 6708312 6708271 STICK SHAKER 6708271 ASCB BU 2 6708312 6708312 6708312 ASCB BU 1—5 6708312 XMIT 6708312 6708213 XMI】 6708312 RS232 A - RCVR. 6708312 6708213 -429 TO PRESS CNTLR 6708272 RS232 A-RCVR- 6708312 COM 6708312 6708320 GEAR ON & LOCK_S# COM 6708312 XMIT 6708312 6708313 STBY PER SW GND 6708313 ¡XMIT- 6708312 RS232 BRCVR 6703312 6708311 O'SPEED WARN TEST RS232 B RCVR- 6708312 COM 6705312 6708323 W.D.W. GND 6708323 COM 6708312 6708331 DAY/NIGHT SN 6708331 6708311 TEST SGNO 6708311 6708277 6708312 6708277 -STAB RVT EXC 6708213 NOSE RECIRC FAN- 6708312 6708277 GLARE FAN 1- 6708312 6708312 6708277 -STAB AVT POSN 6708213 EMERG PER SW N.C. EMERG PWR SW COM GIA FOR AHRS 2 -429 FROM AHRS 2 H-429 BUS TO FADECS -429 BUS 10 FADECS STICK SHAKER GUST LOCK AILERON RATIO STBY PWR SW GND W.O.W. GND DAY/NIGHT SW TEST SW GND 429 PRESS 6708277 CLARE FAN 2 6708312 6708312 6708520 GEAR DN & LOCK SW 6708277 -STAB RVT EXC HF 1 RCCB CONT 6708231 HF 2 RCCB CONT 6708231 6708277 TRIM VALID 6708277 HF 1 RCCB RESET-- 6708231 HF 2 RCCB RESE 6708231 6708277 TRIM UP CMO -STAB RVT POSN 6708277 6708277 ONE TRIM ON CMD 6708277 TRIM UP CMD YSAS A MOTOR VALID--- AURAL WARN FAIL L 6708276 YSAS B MOTOR VALID 6708278 6708312 AURAL WARN FAIL R 6708312 6708272 6708271 AILERON RATIO MADC <70/80 KNOTS 6708277 6708271 TRIM DN CMD 6708312 RAT PROBE SHUNT 6708312 RAT PROBE SHUNT- 6708312 6708312 1 C NEVISIONS DESCRIPTION C REDRAWN WITH CHANGES: UPDATED PAGE 1 EC 042440 MADC <70/80 KNOTS NOTES: 1 THIS ORAWING FILED IN CCD FILE RLSD,E95. 2) AN ASTERISK PRECEDING A LETTER INDICATES LOWER CASE. MS27474E14F35S CONNECTOR SELCAL VHF 1 ---- ---6708312 6708331 SELCAL VHF 2 -6708312 6708331 SELCAL HF 1 -6708312 6708331 SELCAL HF 2 -6708312 6708270 SELCAL VHF 3 -6708312 6708324 -6708312 6708324 SATCOM CHI --6708512 SATCOM CH 2 -6708312 6708277 6708277 6708750 6708290 COMM 1 PTT-FOR-- -6708312 COMM 2 PTT-FOR- HF 1/2 PTT-FDR-- -6708312 -6708312 6708522 6708522 6708307 RH BLEED AIR DIAG- 6708522 8708270 6708307 AA-300/ALT-55--- ⚫6708312 PCU MONITOR- 6708272 6708272 LH BLEED AIR DIAG- 6708307 6708307 HW RAD ALT-1H- RAD ALT VAL ID- CVR FAIL -6708312 ---6708312 6708270 6708277 -6708312 6708331 ---6708312 6708341 6708312 FDR ACCEL VERT- 8708341 6708312 25---6708312 6708341 FOR ACCEL LAT 6708312 6708312 FOR 717 DATA H -6708512 6708341 -6706312 6708341 6708312 FOR ACCEL LONG- ---6708312 6708341 6708312 TCAS TA- TCAS RA PREV· TCAS RA CORR -6708312 6708341 -6708312 6706270 +6703312 6708270 CPWS 429- -6708312 JK901 BAGGAGE COMPARTMENT AVIONICS FOR FAIL PK901 BAGGAGE COMPARTMENT ELECTRICAL MS27473E14F35P CONNECTOR JC905 LH SIDE CONSOLE ELECTRICAL MS27474E14F355 CONNECTOR 6708270 6708270 PC905 LH SIDE CONSOLE AVIONICS MS27473E14F55P CONNECTOR EL PANEL POWER UPPER RUDDER ANNUN RAD ALT 500 FT TRIP LH PER STEERING OFF RH PWR STEERING OFF PRI TRIM ENABLE PRI TRIM NTR PER STATUS RUO HYD STBY PUMP GC - FLAPS >- 15- GC - FLAPS FULL IN.O. DOOR LOCK SW) COM DOOR LOCK SW N.C. DOOR LOCK SW RH LAND GEAR HORN LH LAND GEAR HORN STAB TRIM MOTION UPPER RUD ANNUN DIM M-RH ADA RH ADA VALID {AOA REFERENCE) H-LH ADA LH ADA VALID FLAPS 0 FLAPS 5- AVIONICS / ELECTRICAL DISCONNECTS GO AROUND SW 6708270 -6708312 6708270 FLAPS 15° FLAPS FULL 6708522 6708270 COL RAD ALT- --6708312 6708270 ---6708312 6708323 MASTER CAUTION RESET _ UPPER YO PEDAL RVT DISCONNECT W.O.W. FOR FGC DATE DRA GROUP CHECK 07-08-96 FAIRBANKS {tact | མ C. CESSNA AIRCRAFT COMPANT IRCAN DIVISION __7304 WICHITA, KANSAS 67277 AVIONICS SYSTEMS REFERENCE AVN/ELE DISCONNECTS F 71379 9500500 WECT OF 4 CO36717 9500500 C ■ DATE [APPROVED 08/02/99 ANV PN325 IRS 1 FA R$ 1 FAN $10 IN NC C PN326 ANHUN / LIGHTING IRS 2 FAM 31 IRS 1 TA SIG IN 28 MC PN321 PN322 AUDIO / AHRS MUD TO PL [1] SPARE AUDIO PHL 3 (1) SPARE LAS1415 ΚΑ MUDIO PHIL 1 [M) SPARE DUT AUDIO PHL 2 [M) SPARE FAN CABIN SPKA {H} SPARE 25 C1 GND GHO C 019 ANDOUT FOR IN n❘ CONT R/CAUTION LT SPARE +26/13 APR IN 19 016 CABIN SP (L} SPARZ • 040 +26VDC AUDIO SPARE 13 AUDIO ST CO SPARE FMS 2 CONT 36 017 MARK/CAUTION £1 34 HE FAR OUT FOR OUT 11 016 ARE +2/15 33 013 RADAR CONT SPARE +20/15 35 014 PRI FOR LA PRI POR 045 24 FLT GUIDE CONT FLT GUIDE CONT 15 013 SPARE +28/15 SPARE +28/13 30 DIZ PRI POR OUT ALO POR OUT PRI PAR OUT AUX PAR OUT IRS 120/18 IRS 2 +20/15 29 " 22 D47 HF 1 XFER +20/15 HF 2 KFER +28/15 27 AUX PR 1 AUL POR 046 21 D5Z CPU +28/15 ELT +28/15 12 FMS 1 DIN CHABLE PIS Z DIN CHABLE 22 ככס R17 AHRS/195 PRI PER |_ SHEET [DEV] PN323 PN324 TOW TCAS NOW LIGHT DET FOR 2 IAC 1 NOV TAC 2 TON 21 028 AIRE POWER AHRS AUX) INNOVER 3 AHS 19 ANTS 2 FOR 13 C REVISIONS. DESCRIPTION |_ DATE APPROVED SPARE VOT SPARE NOW 7 ADF LOCK OUT ADF LOCK OUT 17 028 ADF LOCK OUT ADF LOCK OUT 16 D29 027 HF 1 PTT YLF/ONEDA YOU RADAR CONT FOR HF 2 PTT 18 ELT WOR 1 SPARE TOY " RADAR R/T YO SPARE YOU 12 SPARE WOR SPARE DE 9 K12 HOW KIS DIG K5 DAY/WITE 039 043 MRS/IRS ON/OFF AH/IRS ON/OFF 14 AHRS/IRS FM | TO 2 15 AUX PWR CLR DEL YOU SPARE YOU 22 044 DAY/TIT CH NAY AUDIO (K) DAY/NITE CND UNUSED 17 26 2.21K RI 1/ ER MAY AUDIO H UNUSED 25 OUR WAY AUDIO H UNUSED 24 m 2.21K R2 1/8 011 SPARE TEST OUT SPARE TEST OUT 7 TEST OND TEST DO 18 DC CMD TAN DAMP TEST PITEST DC GAD 16 SPARE TEST OUT 32 FMS 2 TEST 37 FOC TEST FCC IEST 23 GPWS TEST SPARE TEST 9 SPARE TEST ELT TEST 14 IRS 1 AN UN TEST IRS 3 MIUN TEST 13 BALT CAT ALT OUT 21 BAR LT BIC IN CAUTION IT OUT CAUTION LT IN GPUS LT IN HF XFER HEI PER LT IN CS LT IN CPUS NOW #05 #4 25 D8 01 041 LT $IG IN CAUTION L1 out K1 2 D2 050 CAUTION LT IN OPUS LT IN 11 OPMS ANNU 10 F2 PER ANN 2 FELT IN OPBLT IN 2-0 on on D$1 053 DS 03 04 010 HF 1 RESET UNUSED H2 RESET 10 UMUSED NF 1 PTT IN 2 PTT IN 16 B COM RESET COM +289DC IN COP IN UNUSED UN 1+2 VOC IN UMUSED OC GROUND SPARĘ +20/15 THE 2 RESET W 1 UNUSED DC GROUND SPARE +28/15 COMM 2 REST 037 COMM 2 +20VDC IN COMM 2 PTT IN N MADT I HOV MADC 2 FO 23 XPON 1 OP XPDR ZON ° NOW HIG CVR ERASE ARE CVR CRASE SPARE 030 034 D32] DC GROUND DC CROUND LTH DET INHIBIT IN DET N 034 K13 035 KIB UHF SELCAL RESET THE SELCAL RESET NE SELCAL RESET ALTG DET INHIBIT AVIONICS NOSE J-BOX THIS SHEET CREATED FROM DRAWINGS 9555015 & 9555016 19 LÜK DET INHIBIT, LIN DET UDUBIT 20 D30 1+2VDC IN HF 2 +28VOC IN 4 025 K10 CIA IN QIA IN 10 054 GHD IN AIR DATE 07-08-96 FAIRBANKS] CHECK OTHER NIF T CESSNA AIRCRAFT COMPART AIRCRAFT DIVISION WICHITA, KANSAS 67277 AVIONICS SYSTEMS $122] P501 ■*. REFERENCE NOSE J-80x F(71379 9500500 |11 2. OF 4 * 9500500 C ECO36717 ☑ 24 25 C KP4A RPSA m RPEA Z6 254 22 w RP1A w APZA KPSC APAC 407 of RPJA TET 23 11q го 5 53 C$ ت C2 010 DS 014 D12 011 013 U3 MC7SMOSC1 VOC VDC UTA U18 m R13 01 HC132 BTS1ZIA HC132 ID-ID HC132 HC132 1 D&F 5 C7 DIG DIS m 27 USA 028 w D MC132 HC132 K14 D-D HC1.52 HC132 813 02 OT$121A K1 B 04 UPPER YAW DAMPER SWITCHOVER CIRCUIT THIS SHEET CREATED FROM DRAWING 9555018 JI & REVISION Ş QESCRIPTION PF 301 ■E DATE [APPROVE ANNUN TEST GND IN A MOTOR ENABLE IN (28V) 6 A MOTOR VALID IN [28V) 9 A ANNUN GND OUT GND IN 2BY OUT (A OR B) 3 28 VDC IN 2 28V IN THRU PB SWITCH A YSAC ENABLE OUT J2 PF 303 B YSAC ENABLE OUT CND IN 25V IN THRU PB SWITCH 3 28 VDC IN 7 28V OUT (A OR B) ANNUN TEST GND 1N B MOTOR VALID IN [28V) B MOTOR ENABLE IN (28V) g B ANNUN GND OUT CATE 07-0--96 OTHER FAIRBANKS] བུས་ SHEET CES AIRCRAFT COMPANT AIRCRAFT DIVISION _ PO. BON 7704 WICHITA, KANSAS $7277 AVIONICS SYSTEMS REFERENCE UPPER YD SWITCHOVER: | 412E] PHÓM MG. F 71379 9500500 | 3 OF 4 9500500|"C HF2 AUDIO IN DC GND 2 SELECT 3 LH SELECT 2 LH SELECT 2 RH HF2 PTT IN +28VDC OUT 1 SELECT 3 RH +28VDC OUT 2 +28VDC IN 2 HF1 PTT IN +25VDC IN 1 HF1 AUD 10 IN SIG OND 2 HF2 SWITCH GND HF2 XFER LIGHT HF2 MEC AUDIO HF2 S/T OUT HF2 RCVR OUT HF2 MIC OUT HF2 PTT OUT し HF1 XFER LIGHT SIG GND 1 HF1 MFC AUDIO HFI S/T OUT HF1 RCVR OUT HANDSET AUDIO HF1 MIC OUT HANDSET MIC HFI PTT OUT HANDSET PTT N || 11 || 1 | | | ||| || | || IUI || |||||| ||||| ||| 1 E +28VDC IN AUX HFI S/T ENABLE HANDSET SWITCH GND HANDSET HF SELECT HF1 XFER SWITCH HF2 S/T ENABLE E 1 1 I || I 1 151131 J2 1 511 J1 11 1 J2 1 J1 05 مش K10 HF SELECT 1 014 18 K9 013 HF SELECT 2 احل K2 HF2 CUTOUT 04 D18 HF2 K8 SIDETONE & INTERLOCK K7 HF2 SIDETONE & INTERLOCK 016 K12 D12 SELCAL ANNUN POWER FOR K13 ERASE 08 0153 REVISIONS © SHELT (REU)] DESCRIPTION J3 | DATE APPROVE CHIME SIG GND IN CALL CHIME OUT 10 DC GNO +28VDC IN (SELCAL) E CALL ANNUN + OUT ANNUN PER IN J1 RELAY COMMON-8 S1 LETTER 1 J3 K11 SELCAL CHIME S2 LETTER 2 Do K4 HF2 LATCH 12 010 011 09 0 ! K6 OVER-RIDE + D2 141 هلا 7-012 all K1 D1 D3 K3 07 K5 HF/TELE SEL HF1 CUTOUT HF1 LATCH 017 HF J-BOX REFERENCE THIS SHEET CREATED FROM DRAWING 9255026 S3 LETTER 3 S4 LETTER 4 J1 5432 IIII FINNN RELAY NC-B RELAY HO-8 RELAY NC-A RELAY NO-A RELAY COIL RELAY COIL + RELAY OMMON-A SELCAL CODE SEL 0 SGL HF 012 له S5 HF 1/2 SEL - HF TO ANT COUP. HF1 PTT TO ADAPT. AUDIO LOW HANDSET AUDIO LOW HF1 MIC IN AUDIO LOW HF RCVR/ST AUDIO LOW HEI AUDIO OUT 33 AUDIO LOW HF1 MIC OUT AUDIO LOW HF2 AUDIO OUT AUDIO LOW HF2 MIC OUT AUDIO LOW HF2 RCVR/ST AUDIO LOW HF2 MIC IN 2 HF1 PIT TO BOG AMP HF1 PT TO BDC AMP ↑ I QUAL HF J2 SCHEMATIC FOR -1 -3 P/C ASSY'S DATE 07-08-96 FAIRBANKS CROUP CH аст PROJ M.E. OTHER STO. GREET COMPANY CENA AIRCRAVISION P.O. SOK 7704 WICHITA, KANSAR 7277 AVIONICS SYSTEMS REFERENCE F 71379 SOLE: HF J-BOX 9500500 BEET 4 9500500 C PK601A NAV 1 (164JIA) ·(WHT) NAV AUX DATA (BLU) (WHT NAV AUX CLK PK601B [164J18) NAV 1 NAY AUT SHIFT LO -(BLU) 【WHT) (BLU) PK501 (14331) RCZ-851 < COMM ACH DATA- (WHT) (BLU) SIMULCOM (WHT) SIMULCOM RET (BLU) VOC IN VDC IN VDC 1N +28 VDC RTM +28 VDC ATN +28 VDC RTN TDC11 PK547 r XK501 5 VDC OUT H 16 [W2-BLK) DATA 101 2-WHT CLK BB [W1-BLK) E6 COMM 1 STRAPPING STRAP LOAD 5 VDC OUT L 102 [▼1-WHT) EZ CIRCUIT CARD 4. -[W3-BLK) ₤4 28V FAN PWR 28Y FAN RTN COMM (14343) ANTENNA 2 (RED) 154 -(BLU}- COMM RF IN/OUT MK501 [16} ZK501A ZK501 ZK5018 90° BNC PK502 C PQ501 JQ501 WHT (BLU) WHT (BLU) COM 2 (C143J1} SIMUL.COM SIMULCOM RET ' MID PRESS BHD (THT. (BLU) XC90 CDC21 (WHI) (BLU) CDC22. P1507 (165) STBY NAV/COM HENAY AUX DATA NAV AUX CLK REVISIONS "DESCRIPTION A REORAWN WITH CHANGES: 11 ADD PK547 AND REDRAW STRAP CARD & WIRING 2) ADD NOTE 6 EC 035047 | DATE [LYTROVE P. | 04/27/95| TLF WHT (BLU) NAV AUX SHIFT LO D 0-5 VDC EDGE LT 2 LTG COMMON PROGRAM GND 1 RM1 BRG LCSB WIDE BAND SEL INSIDE SELECT C SQUAT SW POLARITY COMM AUX YWOW (GND/OPEN) J+28 VDC PER RTN E 28 PER IN (16) PF903 PF902 1 COMM 1 2001 STBY NAV/COM PN323 PILOTS J-BOX PB303 JB303 CDC13 WOW OUT WOW OUT PF901 1 RMU T P1501 RMU 1 (14421) C+28 VDC PER IN D+28VDC PWR GND PWOW (GND/OPEN) SV LTG GND NOTES: 1. ". 2. 3. THIS DRAWING FILED IN CADAN FILE RLSD.E95. ALL WIRE 22 ANG. EXCEPT AS NOTED. AN ASTERISK PRECEEDING A LETTER INDICATES LOWER CASE. ☑COOLING FAN IS MOUNTED TO BACK OF RACK AS PART OF MTG TRAY ASSY. GND STUD IS LOCATED ON THE BACK OF THE TRAY 15 STRAP CARD IS REMOTELY LOCATED WITH THE NAV 1 STRAP CARD. WIRING AND CONNECTOR IS VENDOR FURNISHED BUT SHOULD HAVE SHIELDS TERMINATED AS SHOWN USING APPROVED METHODS. FWD PRESS BHD CDC31 (BLU) (WHT: 5V LTG IN XC90 HKR BCN SENSE MKR BCN SENSE DSIDE 100 ⚫C SIDE IDI B SIDE 1D2 R SQUAT SW POLARITY UCHASSIS CND DATE 11-04-93 FAIRBANKS] GROUP CHEER PROJ M... OTHER | FABRICATE FO sia. 9501101 A काम. COMPANY KANSAS 67277 CABLE ASSY COMM 1 035047 F 71379 9501101 | CITATION X | meci 1 OF | ទ PK502 (C143J1RCZ-B51 RTN RTN VDC RTN C -(16)- TDC21 PQ502 JQ502 5 VDC OUT К 16 DATA 101 (W2-BLK) (W2-WHT CLK 88 (WI-BLK) PK548 XK502 COMM 2 STRAPPING WD LOAD 5 VDC OUT L 1022 45 (WI-WHT) (#3-BLK) CIRCUIT CARD E4 MID PRESS BHD (16)- MX502 28V FAN WR 28V FAN RIN (RED> {BLU} PN324 COPILOTS J-BOX WOW OUT 15 PB304 JB304 COMM 2 (C14333 ANTENNA BAGGAGE FLOOR FEEDTHRU ZK502B ' FND PRESS ВНО ZYJDZA ZK502 ZY502 COMM RF IN/OUT ZK302A JKSTO ZY5028 90° BNC CDC23 CDC33 PF 904 PF902, 20100 COMON 2 2030 ANU 2 NEVISIONS SHEET KEYI DESCRIPTION ABY REVISION: (1) ADD PK548 AND REDRAW STRAP CARD & WIRING 2) ADD NOTES 5 & 6 EC 035047 | DATE APPROVED (BLU) ΨΗΤ NOTES: RH CB PANEL 1 1. 2. 3. P1502 RMU 2 (C144J1) C28 VDC PWR IN D 28VDC P♥R GND SV LTG GNO 5V LTG IN THIS DRAWING FILED IN CADAM FILE RLSD.E95. ALL WIRE 22 AWG. EXCEPT AS NOTED. AN ASTERISK PRECEEDING A LETTER INDICATES LOWER CASE. ✓ COOLING FAN MOUNTED TO BACK OF RACK AS PART OF MTG TRAY ASSY. STRAP CARD IS REMOTELY LOCATED WITH THE NAV 2 STRAP CARD. WIRING AND CONNECTOR IS VENDOR FURNISHED BUT SHOULD HAVE SHIELDS TERMINATED AS SHOWN USING APPROVED METHODS. GROUND STUD IS LOCATED ON BACK SIDE OF TRAY WOW (GND/OPEN) MKR BCN SENSE MKR BCN SENSE SIDE 101 SQUAT SW POLARITY CHASSIS GND DATE 11-04-93 GROLE FAIRBANKS CHECK ист OTHER CARD PO BEE STO. SHEET CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION P.O. BOK 7704 WICHITA, KANSAS #7277 $121(1961 19. CABLE ASSY COMM 2 F 71379 9501102 | CITATION EET 1 OF 1 EC 035047 9501102 A ! C. C i AVN ACC DISC PC512 | JC512 NOTES: 1. THIS DWC IS FILED IN CADAH FILE. RLSD,E95. [2>CONNECT TO AN INPUT WITH AN IMPEDANCE OF 600 OHMS. SIGNAL LEVEL WILL BE APROX 3 V RMS MAX. 3. AN ASTERISK PRECEEDING A LETTER INDICATES LOWER CASE. (WHT (BLU) {10 AUDIO DWG) SEVISIONS DESCRIPTION |_DATE_|APPROYEC PI501 AUDIO 2 C160JI 1 COPILOT PHONE H KCOPILUT PHONE L - 9011096 ** EC037548 DATE 11/04/96. IDMANN NARAN SMALL GOLIA CICCA SECT PROJ RESPE CESSNA ARANY 41HDHAFT DIVISION WICHT: RON KANGAS 67577 CABLE ASSY- CABIN HEADSET JACK ICOPILOT AUDIO S.E.R.: F71379 9501106 SI NOTES: ' THIS DRAWING IS FILED IN CADAN FILE RLSD.E95. 2 ALL WIRE IS 22 AUG. EXCEPT AS NOTED. 3 AN ASTERISK PRECEEDING A LETTER INDICATES LOWER CASE. ☑✓ PART OF 422535-801 CABLE ASSY. CABLE ASSY INCLUDES WIRE AND IS PARTIALLY ASSEMBLED. ✓ PART OF 422613-802 CABLE ASSY. RAD-TEL CAB-INPH PF519 COBR 1 CDBR CLOCK CDBR CLOCK CDBR FS CDBR FS CDBR TXD CDBR TXD (1) CDBR RXD CDBR RXD +12 VDC GROUND +12 VDC GROUND RESERVED CDBR RESERVED CDBR SPARE PF522 CDBR 1 UTE DRI (34) UTE +5 CLK FS UTE TXO GROUND PF 520 CDBR 1 CDBR CLOCK CDAR CLOCK (J2) ффффффф IPF903 ☑ -16 (16) [16) (TO ACC COBR-2 PTR IF INSTALLED] 1/H M10 BHD JQ513 PQ513 •|- TDC22 C REVISIONS DESCRIPTION ||| DATE |APPROVED PK555 ATRU TRAY (J2} (18). B +28VDC IN PRI +28VDC IN SEC {16}· C GROUND PK557 ATRU TRAY {J}}| FAN CONTROL 422650-801 VENDOR SUPPLIED CABLE DO NOT ATTEMPT TO TEST. DISASSEMBLE. OR REPAIR. JQ511;PQ511 (BRN ORN ORN (YEL YEL GRN (VIO) VIO) WHT WHT GRY GRY CLR CLR (RED) RED (BLK) (BLK) +12 VDC (RED/WHT (RED/WHT) GROUND (BLK/WHT RESERVED COBA RESERVED COBR (BLU) RESERVED COBR (810) RESERVED CDBR (TAN) (BLK/WHT) (TAN) PK543 ATRU (POWER}} POWER IN PK541 ATRU (DATA) CDBR CLOCK NCDBR CLOCK ⚫D CDBR FS P CDBR FS JCDBR TXD K CDBR TXD CDBR RXD BCDBR RXD +12 VDC GROUND +12 VDC GROUND COCOCOCO RESERVED COBR H RESERVED CDER (BRN) (ORN) (YEL CRN (VID) WHTI (GRY) (CLR) (RED) (BLK) (RED/WHT) (BLK/WHT) (BLU (TAN) JF 523 PF523 (REF ACC DWG) AIU JZ PF535 CDBR CLOCK COBR CLOCK COBR FS 4 CDBR FS COBR TXD CDBR TXD 10 CDBR RXD 11 COBR RXD 12 +12 VDC GROUND 13 +12 VDC 9 GROUND 30000000 √1 PF533 CDBR CLO CDBR CLOCK CDBR F5 CDBR FS COBR TXD CDBR FXD CDBR RXD CDBR RXD +12 VDC GROUND M² 30000000 422613-801 CABLE ASST PHONE RECEPTACLE PF524 CAS D (H) CAS O (L) CAS 1 (H) CAS 1 {L} (J2) COBR FS CDBR FS CDBR TXD CAS 2 (H) CDBR TXO CAS 2 (L) CDBR RXD TO CABIN COBR {H} CDBR RXD REF ACC DVC +12 VDC GROUND +12 VDC GROUND JF539 PF539 CAS RESERVED COBR RESERVED CDBR {16}- UF 501 CAS 6 (H) SPARE PF521 CDBR 1 UTE DRI (J3) UTE +5 CLK FS UTE TXO GROUND RCV ZX525B - хит Zx5268] (ZY307) DUPLEXER ZY507A (2K526) XMT ZX3264 (2K525) ☐ RCV (ZK517) 33 ZY507B JK516 ZK517A PK517 PF 537 (ORN) (BLU) (WHT) (WHT (BLU) (ORN) JQ503! PQ503 12 PHONE AUDIO 37 AUDIO COMMON 13 PHONE MIC AUDIO 14 PHONE PTT 17 PHONE HOOK ST 16 HF SEL CND HF J-BOX (J1]] REF HF 1 +28 VDC IN AUX 1 (REF HF 1 DWG) MID вно CDC21 422035-801 CABLE ASSY (WHT/GRN) (WHT/ORN) (HT BLU) (WHT] CAS 6 (L) -SPARE PF525 CAS UTE DRI (31)] UTE +5 CLK FS UTE TXO GROUND HF RECEIVER AUDIO IN (H) HF AUDIO COMMON KF MIC AUDIO OUT (H) HF PTT OUT PHONE HOOK SWITCH HF CONF CONF GROUND X325A ANT ZX5170 DATE 01/27/99. CJA WESTHOF F 1091 T CESSNA AIRCRAFT COMPANY ROAT DIVISION _ _ O. BOX 7704 WICHITA, RANBAS 7277 CABLE ASSY- MAGNASTAR PHONE F 71379 (TAIL) 9501315 SHEET 1 OF I EC 670094 *** 9501315 -