REV REVISION DESCRIPTION ECO NO.DATE
NOTES
SHIELD BLOCK GROUND
CONTINUATION (CONNECTOR)
NO CONNECTION
CONNECTION
VENDOR CODE FLAGX
SG SHIELDED TWISTED 3 CONDUCTORW
B
O
SHIELDED TWISTED 2 CONDUCTORW
B
SHIELDED SINGLE CONDUCTOR
1) UNLESS OTHERWISE SPECIFIED, REFER TO SAE AS50881, REV B; WIRING AEROSPACE VEHICLE.
2) UNLESS OTHERWISE SPECIFIED, ALL STRANDED WIRE IS 22 AWG MINIMUM AND SHALL MEET OR EXCEEDM22759/16 SPEC OR EQUIVALENT, UNLESS OTHERWISE SPECIFIED, ALL SHIELDED WIRE IS 24 AWG MINIMUMAND SHALL MEET OR EXCEED M27500 SPEC OR EQUIVALENT. THE FOLLOWING SYMBOLS ARE USED ON THIS DRAWING:
ELECTRICAL EQUIPMENT AND THEIR SUPPORTING BRACKETS SHALL BE ELECTRONICALLY BONDED. THE SURFACE PREPARATIONSHALL BE PER SAE ARP 1870, SECTION 5. THE ELECTRICAL BOND SHALL ACHIEVE A DIRECT CURRENT (DC) RESISTANCE OF 2.5MILLIOHMS OR LESS BETWEEN EACH FAYING SURFACE AND THE AIRCRAFT STRUCTURE. COMPLIANCE SHALL BE VERIFIEDBY INSPECTION USING A CALIBRATED MILLIOHM METER. ELECTRICAL EQUIPMENT INCLUDES METAL CONNECTORS WITH SHIELDS.
3
REMOVE EXISTING WIRES FROM HATCHED CONNECTOR AND ROUTE TO CONNECTOR POSITIONS SHOWN ON 1P261. NOTE AIRCRAFTSERIAL NUMBERS SHOWN FOR DETERMINING CORRECT WIRING CONNECTIONS.
4
REMOVE EXISTING WIRES FROM HATCHED CONNECTOR AND ROUTE TO CONNECTOR POSITIONS SHOWN ON 2P261. NOTE AIRCRAFTSERIAL NUMBERS SHOWN FOR DETERMINING CORRECT WIRING CONNECTIONS.
5
REMOVE EXISTING WIRES FROM HATCHED CONNECTORS AND ROUTE TO CONNECTOR POSITIONS SHOWN ON P9201 OR P9202 AS SHOWN.NOTE AIRCRAFT SERIAL NUMBERS SHOWN FOR DETERMINING CORRECT WIRING CONNECTIONS.
6
REMOVE EXISTING WIRES FROM HATCHED CONNECTORS AND ROUTE TO CONNECTOR POSITIONS SHOWN ON 1P711. VERIFY WIRING
AIRCRAFT SERIAL NUMBERS LJ-1063 THROUGH LJ-1360 AND LJ-1362.
7
8 REMOVE EXISTING WIRES FROM HATCHED CONNECTOR P119. SPLICE WIRE "E13A22" TO WHITE WIRE OF W129. SPLICE WIRE "E15C22"TO BLUE WIRE OF W129. ROUTE ORANGE AND GREEN WIRES OF W129 TO POSITIONS 46 AND 47 RESPECTIVELY OF CONNECTOR1P711. THIS NOTE APPLIES ONLY TO AIRCRAFT SERIAL NUMBERS LJ-1361, LJ-1363 AND AFTER.
9
10 REMOVE EXISTING WIRES FROM HATCHED CONNECTOR P120. SPLICE WIRE "E14A22" TO WHITE WIRE OF W130. SPLICE WIRE "E20C22"TO BLUE WIRE OF W130. ROUTE ORANGE AND GREEN WIRES OF W130 TO POSITIONS 46 AND 47 RESPECTIVELY OF CONNECTOR2P711. THIS NOTE APPLIES ONLY TO AIRCRAFT SERIAL NUMBERS LJ-1361, LJ-1363 AND AFTER.
11 FOR AIRCRAFT SERIAL NUMBERS LJ-1108 THROUGH LJ-1360 AND LJ-1362, REMOVE BALANCING RESISTORS AND CONNECTTHERMOCOUPLE WIRES TO GEA CONNECTOR AS SHOWN. THE WIRE USED FOR GROUNDING PIN 63 IS M22759/16-22-9. USE MIL-W-5846
12 FOR AIRCRAFT SERIAL NUMBERS LJ-1361 AND LJ-1363 AND AFTER, REMOVE WIRES FROM HATCHED CONNECTOR AND CONNECTTHE THERMOCOUPLE WIRES TO GEA CONNECTOR AS SHOWN. THE WIRE USED FOR GROUNDING PIN 63 IS M22759/16-22-9. USE MIL-W-5846
THAT THE SHIELD IS MAINTAINED THROUGH THE GEA BACKSHELL.
?
GBXXX
?
SPECIFIC NOTE
GROUND BLOCK
CONTINUATION (WIRE)
GROUND TERMINAL LUG
CAP & STOW
CIRCUIT BREAKER?
W
B
O
G
SHIELDED TWISTED 4 CONDUCTORETHERNET
TABLE OF CONTENTS:
SHT DESCRIPTION SHT DESCRIPTION
1 NOTES2 NOTES (CONTINUED)3 BOM4 BOM (CONTINUED)
6 NO1 GDU, DU FAN, GMC 7105 FLAP-IN-MOTION SENSING
7 NO 1 GRS8 NO1 GDC9 NO 2 GDU, DU FAN
10 NO 3 GDU (MFD), DU FAN, GCU 47511 NO 1 GIA12 NO1 & NO 2 GIA POWER, FANS,
13 NO 2 SERVO (PITCH TRIM), NO 3
14 NO 2 GIA15 NO 2 GRS16 NO2 GDC17 NO 1 & NO 2 GTX18 COLLINS ADF19 COLLINS DME20 STBY ATTITUDE, STBY ALT/AS
21 TRAFFIC SYSTEM PROVISIONS22 GDL 69A DATA LINK, GWX 68 RADAR
23 NO 1 GEA, NO 1 TACH ADAPTR24 NO 2 GEA, NO 2 TACH ADAPTR25 PC 920 FF SIGNAL CONDITIONER26 ENGINE TORQUE CONNECTIONS27 ENGINE ITT CONNECTIONS28 ENGINE OIL TEMP/PRESSURE
29 CWS SW, MET SW30 AP DISCONNECT31 NO 1 & NO 2 GMA COM AUDIO,
32 NO 1 & NO 2 GMA ANALOG AUDIOS,
33 NO 1 GMA JACK CONNECTIONS34 NO 2 GMA JACK CONNECTIONS35 NO 1 & NO 2 DIGITAL AUDIO36 NO 1 & NO 2 AUDIO POWER, MKR ANT,
37 PA AUDIO CONNECTIONS, PASSENGER
38 RH CB PANEL (A146)39 STBY BATT CONNECTIONS
40 STBY BATT CONNECTIONS (CABIN/NOSE)41 LH CB PANEL (A124)
NO1 GSA SERVO (ROLL)
SERVO (PITCH), NO 4 SERVO (YAW)
LIGHTING
PASS MIC PROVISIONS
NOTES
QUALIFIED WIRE TO EXTEND THERMOCOUPLE WIRES. USE ENVIRONMENTAL CRIMP SPLICES FOR WIRE-TO-WIRE CONNECTIONS.
QUALIFIED WIRE TO EXTEND THERMOCOUPLE WIRES. USE ENVIRONMENTAL CRIMP SPLICES FOR WIRE-TO-WIRE CONNECTIONS. NOTE
SOLDER SLEEVE SPLICE
ENVIRONMENTAL CRIMP SPLICE
13 CONFIGURATION MODULE RESIDES WITHIN THE BACKSHELL OF THE HARNESS CONNECTOR.
14 CONNECTOR IS INSTALLED ON HARNESS AFTER WIRING IS IN PLACE.
15 THERMOCOUPLE RESIDES WITHIN THE BACKSHELL OF THE HARNESS CONNECTOR.
16) BUSSING MODULES USED ON THIS DRAWING:
16 POSITION MODULE;POSITIONS 1 THROUGH 16 ARE COMMON
16 POSITION MODULE;POSITIONS 1 THROUGH 4 ARE COMMONPOSITIONS 5 THROUGH 8 ARE COMMONPOSITIONS 9 THROUGH 12 ARE COMMONPOSITIONS 13 THROUGH 16 ARE COMMON
16 POSITION DIODE MODULE;DIODES ARE 1N4007
9 POSITION MODULE;POSITIONS 1 THROUGH 3 ARE COMMONPOSITIONS 4 THROUGH 6 ARE COMMONPOSITIONS 7 THROUGH 9 ARE COMMON
9 POSITION MODULE;POSITIONS 1, 4, AND 7 ARE COMMONPOSITIONS 2, 5, AND 8 ARE COMMONPOSITIONS 3, 6, AND 9 ARE COMMON
9 POSITION MODULE;POSITIONS 1 THROUGH 3 ARE COMMONPOSITIONS 4 THROUGH 9 ARE COMMON
9 POSITION RELAY MODULE;RELAY CONFORMS TO MIL-R-39016 SPECPART # M39016/19-036L
22 GAUGE CONTACTS
22 GAUGE CONTACTS
22 GAUGE CONTACTS
20 GAUGE CONTACTS
20 GAUGE CONTACTS
20 GAUGE CONTACTS
20 GAUGE CONTACTS
ANTENNA
ELECTRICAL BONDS OF EQUIPMENT SHALL BE PERFORMED WITH HARNESS CONNECTOR DISCONNECTED.
EXISTING WIRING / COMPONENT
NEW WIRING
? REMOVED CONNECTOR / COMPONENT
REMOVE EXISTING WIRES FROM HATCHED CONNECTORS P123 & P124 AND ROUTE THEM TO CONNECTORS 1P701 & 2P701 RESPECTIVELY.
APPLIES TO AIRCRAFT SERIAL NUMBERS LJ-1063 THROUGH LJ-1360, AND LJ-1362.
17CONNECT WIRES AS SHOWN NOTING THAT WIRES THAT WERE FORMERLY IN PINS F & E NEED TO BE SPLICED TOGETHER. THIS NOTE
REMOVE EXISTING WIRES FROM HATCHED CONNECTORS P123 & P124 AND ROUTE THEM TO CONNECTORS 1P701 & 2P701 RESPECTIVELY.THIS NOTE APPLIES TO AIRCRAFT SERIAL NUMBERS LJ-1361, LJ-1363 AND AFTER.
18
REMOVE EXISTING WIRES FROM HATCHED CONNECTOR P123 AND ROUTE THEM TO CONNECTOR 1P701. WIRE E30B22 NEEDS TO BE SPLICED19INTO THE BLUE WIRE OF W141 BEFORE BEING CONNECTED TO 1P701 AS SHOWN. NOTE THAT WIRE E27B22 IS CAP AND STOWED.THIS NOTE APPLIES TO AIRCRAFT SERIAL NUMBER LJ-1361, LJ-1363 AND AFTER.
TITLE
SIZE
SCALE
DWG. NO. REV.
SHT. OF
DATE
DRWN.
CHKD.
RLS
PROJ.
TOLERANCEUNLESS NOTED OTHERWISE
MGR.
BY
AJK
RGM
RGS
SMP 09/01/06
08/31/06
08/31/06
08/18/06
WIRING DIAGRAMG1000 / GFC700 KING AIR C90A/C90GT
005-W0022-00 11
501NONE DER REVIEW REQ'D
42 STBY BATT CONNECTIONS
23
2343 J-BOX INTERNAL CIRCUITS USED
44 RF CONNECTIONS
PIC WIRE COLORS
W/B
B/W
O/W
W/O
SHIELDED TWISTED 4 CONDUCTORETHERNET
ECS WIRE COLORS WHERE:PRIMARY COLOR/DASH COLOR
45 PA SPKR AMP (NEW INSTALL)
CONNECTIONS TO THE PRESSURE TRANSDUCER COMPLY WITH CENTEX DRAWING 008-7713-3026. THIS NOTE ONLY APPLIES TO
REMOVE EXISTING WIRES FROM HATCHED CONNECTORS AND ROUTE TO CONNECTOR POSITIONS SHOWN ON 2P711. VERIFY WIRING
AIRCRAFT SERIAL NUMBERS LJ-1063 THROUGH LJ-1360 AND LJ-1362.CONNECTIONS TO THE PRESSURE TRANSDUCER COMPLY WITH CENTEX DRAWING 008-7713-3026. THIS NOTE ONLY APPLIES TO
4146 OPTIONAL GB4, GBA4, GBB4
9 1/15/09 57899
CONNECTIONS
SPKRS
UNSWITCHED AUDIOS
HEADPHONES 41
(EXISTING TAIL)
SHT DESCRIPTION
(NEW INSTALLATION)
(REFERENCE)
BULKHEAD CONNECTORS
THROUGH 50 TO SHOW VIBRO-METER SIGNAL CONDITIONERAND NEW PA AMPLIFIER WIRING. CORRECTED CLERICALERRORS.
47 LT VIBRO-METER SIGNAL CONDITIONERCONNECTIONS
48 RT VIBRO-METER SIGNAL CONDITIONERCONNECTIONS
49 ENGINE INSTRUMENT CB LOCATIONS( WHEN VIBROMETER SIGNALCONDITIONERS INSTALLED)
50 DB AUDIO 240 PA AMP( MDL REV 5 AND SUBSEQUENT)
10 05/07/09 62109
ADDED "BLACKHAWK" NOTES TO CLARIFY TORQUE DATA,(SHEET 26). CORRECTED NOTE 35. ADDED SHEETS 47
11 10/20/09 66384CORRECTED NOTE 11 AND 12 TO ADD MIL-W-5846.
REVISED VMI SIG COND FF INTERFACE SHTS 47 & 48
NOTES (CONTINUED)
REMOVE EXISTING WIRES FROM HATCHED CONNECTOR P124 AND ROUTE THEM TO CONNECTOR 2P701. NOTE THAT WIRE E50B22 IS CAP AND20STOWED. THIS NOTE APPLIES TO AIRCRAFT SERIAL NUMBER LJ-1361, LJ-1363 AND AFTER.
NOTES
21 EXISTING WIRE "L35B22" MUST BE MOVED FROM ITS EXISTING LOCATION (J-TB105) TO G-TB106. EXISTING WIRE "L41C22" MUST BE RELOCATED FROMITS EXISTING LOCATION (K-TB106) TO H-TB106. THIS ALLOWS BOTH PILOT AND COPILOT CLOCKS TO BE CONTROLLED BY THE SAME DIMMER CONTROL.
22 WIRE "L20A22" IS CAP & STOWED NEAR TB 122 LOCATION PER ELECTRICAL REMOVAL DRAWING. LOCATE THIS WIRE AND ROUTE AS CLOSE TO BULKHEADCONNECTOR GBB2 AS PRACTICAL. SPLICE IN NEW WIRE (IF NECESSARY) AS SHOWN.
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
2 50
11
NTS
23 FOR AIRCRAFT WITHOUT AN EXISTING STBY BATTERY INSTALLATION, DISREGARD SHEET 39 AND USE SHEET 42 FOR CONNECTIONS. FOR AIRCRAFT WITHAN EXISTING STBY BATTERY INSTALLATION, USE SHEET 39 FOR NECESSARY WIRING MODIFICATIONS AND DISREGARD SHEET 42. SEE DRAWING
24 WHEN INSTALLED AS PROVISIONS, EACH JACK MUST BE INDIVIDUALLY BAGGED IN A NON-CONDUCTIVE MATERIAL BAG, STOWED, AND ANCHORED. WHEN INSTALLINGTHE JACKS FOR USE, THEY MUST BE ISOLATED FROM GROUND TO MINIMIZE GROUND-LOOP INDUCED NOISE.
25 FOR AIRCRAFT SERIAL NUMBERS LJ-1063 THROUGH LJ-1282 THAT USE "GULL AIRBORNE" FUEL FLOW TRANSDUCERS, THE PC 920 SIGNAL CONDITIONER ISNOT INSTALLED. CONNECTORS P9201 AND P9202 SHOULD BE BAGGED AND STOWED AND WIRES G77109A22 AND G77113A22 SHOULD BE REMOVED FROMCONNECTORS 1P712 AND 2P712 RESPECTIVELY AND CAP & STOWED.
27 OBTAIN CONTACTS FROM KIT. REFER TO THE FOLLOWING TABLE FOR TOOLING FOR GMU 44 MATING CONNECTORS.
1P441 / 2P441 TOOLING
CRIMPER M22520/2-01POSITIONER M22520/2-09
I/R TOOL M81969/1-04
26) ALL ITEMS SHOWING A VENDOR OTHER THAN GARMIN MUST BE OBTAINED BY THE INSTALLER. IF NO VENDOR IS LISTED, THE ITEM MAY BE OBTAINED FROM THEBEST AVAILABLE SOURCE. VENDOR CONTACT INFORMATION:
GARMIN: 1200 E 151ST STREETOLATHE, KS 660621-888-606-5482WWW.GARMIN.COM
HAWKER BEECHCRAFT CORP. (RAPID): 10511 EAST CENTRALWICHITA, KS 672061-888-727-4344WWW.HAWKERBEECHCRAFT.COM
P69A1
64
61
G24C22G34167A22
G34168A223
XDS 258LIGHT ASSY
(STALL WARN)W22A22
P258
3
P200A223 PANEL
ASSY
28 FOR AIRCRAFT SERIAL NUMBERS LJ-1063 THROUGH LJ-1352 THE LANDING GEAR WARNING AND STALL WARNING CIRCUITSUTILIZE INDEPENDENT AURAL ALERTING DEVICES. FOR THESE AIRCRAFT, PROVISIONED WIRES "G34167A22" AND "G34168A22"NEED TO BE CONNECTED AS SHOWN BELOW:
FOR THESE SERIAL NUMBER AIRCRAFT, DISREGARD THE TONE GENERATOR WIRING SHOWN ON SHEET 32.
29 TONE GENERATOR CONNECTIONS ARE APPLICABLE TO AIRCRAFT SERIAL NUMBERS LJ-1353 AND UP. FOR AIRCRAFT WITHOUTA TONE GENERATOR, WIRES "G23162A22" AND "G23163A22" ARE CAP AND STOWED.
30 THESE WIRES ARE CAP AND STOWED IF AUTOPILOT SWITCHES ARE NOT INSTALLED IN THE COPILOT YOKE.
31 THE INTERNAL SCHEMATIC IS PROVIDED FOR REFERENCE PURPOSES ONLY ON SHEET 43.
32 REFERENCE GARMIN DRAWING 005-00375-23 "CONTROL WHEEL MODIFICATION G1000/GFC700 KING AIR C90" FOR MORE INFORMATION.
35
SOLDER SLEEVE AS83519/1-4 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED TWISTEDPAIR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES.
SOLDER SLEEVE AS83519/1-5 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED TWISTEDTRIPLE CABLES, ETHERNET CABLES, AND THE RG-400 COAX AT THE GMA CONNECTORS. BRAID WIRE LENGTH SHOULD
SOLDER SLEEVE AS83519/1-3 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED SINGLECONDUCTOR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES.
37) INSTALLATION OF G1000 INTEGRATED AVIONICS SYSTEM (IAS) AND GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS) ISELIGIBLE ON C90() KING AIR AIRCRAFT EQUIPPED WITH FOUR-BLADE PROPELLORS, TRIPLE-FED ELECTRICAL POWER DISTRIBUTIONSYSTEM, AND COLLINS APS-65 AFCS. FOR AIRCRAFT SERIAL NUMBER ELIGIBILITY, REFER TO GARMIN GENERAL ARRANGEMENTDRAWING, 005-00375-22.
NOT EXCEED 4 INCHES.
USE HEATSHRINK TUBING M23053/5-104-X FOR INSULATING FLOATING SHIELDS ON SINGLE-CONDUCTOR WIRE.
USE HEATSHRINK TUBING M23053/5-106-X FOR INSULATING FLOATING SHIELDS ON TWISTED TRIPLE CONDUCTORS.
36
THE LAST "-X" IN THE PART NUMBERS REFERENCED REPRESENTS COLOR. COLOR USED IS INSTALLER/FABRICATOR'S PREFERENCE.
CRIMP SLICE M81824/1-1 IS USED FOR 26 - 20 GAUGE WIRE.CRIMP SLICE M81824/1-2 IS USED FOR 20 - 16 GAUGE WIRE.
THESE PARTS ARE INCLUDED IN ANNUNCIATOR/SWITCH ASSEMBLY KIT.33REFERENCE G97AE P/N IS: LED-44-15-EA-37698REFERENCE GS 150 P/N IS: LED-44-15-BB-36601.
34
P/N 005-00375-71 (STANDBY BATTERY) FOR PARTS USED IN NEW STBY BATTERY INSTALLATION.
38 OLDER SERIAL NUMBER AIRCRAFT MAY HAVE DIFFERING CONNECTOR DESIGNATIONS THAN WHAT IS SHOWN ON THIS WIRINGDIAGRAM. IN THOSE CASES, CONSULT THE ORIGINAL AIRCRAFT WIRING DIAGRAMS FOR SPECIFIC CONNECTOR INFORMATION. THE
39 THESE CABLES MAY BE PURCHASED AS A GROUP VIA ECS KIT P/N 500-14971-101.
P269 M/W J1
K105 - FLAPS RELAY
1P8X1 M/W J801 GSA 80 (R)
CB1 -
06AN M/W P461
96AA M/W J3
A125 ANN CTL
A146 CB PNL
#1 OXY MIC SW
PIL YOKE
P200 M/W J1 A100 ASSY
CB3 M/W J111 A124/A146CB4 M/W J109 A124/A146
96AB M/W J4 COPIL YOKE
07AN M/W P460 #2 OXY MIC SW
P621 M/W P1 CTL-6295AC M/W P452 PED LTG
06AR M/W 06AS PIL AUDIO06AF M/W 06AG PIL SPKR
GB89AN M/W 89AZ GND BLK
TB105 - PIL LTG
P258 M/W J1 XDS258
97BC M/W 97BE97BS M/W 97BU72AH M/W 72AG CVR IN-LINE
TB122 - STBY INST LTSTB106 - COP LTG
GB89AD M/W 89AJ GND BLK
88AD M/W 88AA FWD PR BH
CB2 - A146 CB PNL
07AR M/W 07AS COP AUDIO07AF M/W 07AG COP SPKR
1P441 M/W J441 #1 GMU 442P441 M/W J441 #2 GMU 44
52AZ M/W 52AY AFT BH
ID CONNECTOR UNIT
GB89AB M/W 89AG GND BLK
GB89AE M/W 89AK GND BLKGB89AL M/W 89AM GND BLK
88AC M/W 88AA FWD PR BH
88AE M/W 88AB FWD PR BH
19AA19AB
M/W J1 ADF-60AM/W J1 CAD-62
ID CONNECTOR UNIT
06DE M/W P50 600-001
90AC M/W 90AG J-BOX90AD M/W 90AH J-BOX
P681 M/W J400 GWX 68
41AA M/W J1 DME-42
10AM M/W P40 24010AN M/W P50 240
M/W LMD-5001-P J-BLK91AD,91FF,91FG,
91AK,91BV,91BY,
91BP,91BT,91BU,
91BR,91BS,91BZ
91GJ
91BW
91CA,91FY,91FZ
91BX,91CC,91CJ,
91CE
91CG,91FJ
M/W LMD-6009-P
J-BLK
J-BLK
M/W LMD-7111-P J-BLK
M/W LMD-6002-P
M/W LMD-6004-P
M/W LMD-6001-P
M/W LMD-6006-P
91FXJ-BLK
J-BLK
J-BLK
52AY M/W 52AZ AFT BH
HANGOUT M/W CONNECTOR M/W
IDENTIFICATION FOR UN-TERMINATED WIRES MAY USE WHAT IS EXISTING IN THE AIRCRAFT (IF APPLICABLE) OR USE THE GUIDANCEIN THE TABLES BELOW.
CONNECTOR USED MUST ACCOMMODATE THE WIRE GAUGE SPECIFIED ON THIS DRAWING WITHOUT DOWN-SPLICING.
40)
P7101 M/W J7101 GMC 710
AUDIO IN-LINE
W
B
W
B( )( )( )( )( )( )
W
B
O
W
B
O
( )
W
B
O
W
B
GM4(STA 260, LH)
GPP4PART OF CABIN HARNESS,
P/N 320-00326-02
OPTIONAL IN-LINE CONNECTORS MAY BE INSTALLED TO ALLOW QUICK DISCONNECTION/CONNECTION OF THE CABIN PASSENGER AUDIO JACKS. THE IN-LINE CONNECTORSSHALL BE LOCATED WITHIN 18 INCHES OF THE AUDIO JACKS THEY ARE ASSOCIATED WITH. SHIELD CONTINUITY SHALL BE MAINTAINED THROUGH THE IN-LINE CONNECTORUSING SHIELD TERMINATIONS NOT GREATER THAN 1.5 INCHES IN LENGTH. THE IN-LINE CONNECTORS ARE INSTALLER SUPPLIED. SEE WIRING EXAMPLE BELOW:
< 1.5 INCHES
USE HEATSHRINK TUBING M23053/5-105-X FOR INSULATING FLOATING SHIELDS ON TWISTED PAIR CONDUCTORS.
PART ORIDENTIFYING NUMBER
NOMENCLATURE ORDESCRIPTION
DESIGNATORSHT
M22759/16-22-9 22 GA STRANDED-REFM22759/16-20-9 20 GA STRANDED-REFM22759/16-18-9 18 GA STRANDED-REFM22759/16-16-9 16 GA STRANDED-REF
22 GA SHIELDED SINGLE-REF M27500-22TE1T1422 GA SHIELDED TWISTED PAIR-REF M27500-22TE2T14
22 GA SHIELDED TWISTED TRIPLE-REF M27500-22TE3T14-REF M27500-20TE2T14-REF M27500-16TE2T14
ETHREF E40424
20 GA SHIELDED TWISTED PAIR16 GA SHIELDED TWISTED PAIR
ETHERNET
NOTES & BILL OF MATERIAL (BOM)
REFREF
REFREFREFREF
REFREFREFREF
REFREFREFREFREF
REF
LLREF 44
400REF M17/128-RG400 COAX CABLEREF 4,36
M22759/16-12-9 12 GA STRANDED-REFM22759/16-10-9 10 GA STRANDED-REFM22759/16-8-9 8 GA STRANDED-REF
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
3 50
11
NTS
QTY(NOSE)
QTY(CABIN)
QTY(TAIL)
VENDOR
BEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCEBEST SOURCE
BEST SOURCE
PIC WIRE & CABLEOR
392404ETH ECS ETHERNET
C90() WIRING DIAGRAM BILL OF MATERIAL (BOM)
REFREF
ECSLL XPDR1B-LL COAX ASSYREF 44
BRAID QQB575R36T0375 TUBULAR BRAID, 3/8 INCHREF 7,15 BEST SOURCESHIELDS AA59569F36T0062 FLAT BRAID, 1/16 INCHAR AR BEST SOURCEAR AR
- AA59163-1II0020 TAPE, SILICONE FUSIONAR AR BEST SOURCEAR AR- MIL-T-43435B TAPE, LACING/TYING, NYLONAR AR BEST SOURCEAR AR
- M23053/5-X-Y SHRINK TUBINGAR AR BEST SOURCEAR AR- M81824/1-X SPLICE (X=SIZE)AR AR BEST SOURCEAR AR
- MS83519/1-X SOLDER SLEEVEAR AR BEST SOURCEAR AR
(X=SIZE, Y=OPT COLOR)
(X=SIZE)
- MS25036-103 RING TERMINAL, #10 18-22 AWGREF BEST SOURCE18,19,37REF 4- MS25036-149 RING TERMINAL, #8 18-22 AWGREF BEST SOURCE-REF REF
1P3281, 2P3281 SAFE328 NO 1/NO 2 EQ BAY FANSSANDIA AEROSPACE12REF
1P1281, 2P1281 SAFE128 NO 1/NO 2/NO 3 DU FANSSANDIA AEROSPACE6,9,10REF3P1281
- 011-00979-00 CONFIGURATION MODULEGARMIN INTL6,7,8,15,REF REF16,23,24
1P10401, 011-00820-01 CONNECTOR KIT (SB)GARMIN INTL6,9,10REF(PIL GDU, COP GDU, MFD GDU)2P10401,P15001
P7101,P4751 011-01040-01 CONNECTOR KITGARMIN INTL6,10REF(GMC AFCS/ GCU FMS CNTLRS)
1P74B1,2P74B1 011-01010-01 CONNECTOR KIT (SB)GARMIN INTL8,16REF(NO 1/NO 2 GDC AIRDATAS)
- 011-00978-00 GTP TEMP PROBE KITGARMIN INTL8,16REF
1P771,2P771 011-00869-01 CONNECTOR KIT (SB)GARMIN INTL7,15REF(NO 1/NO 2 GRS AHRS)
1P441,2P441 011-00871-00 CONNECTOR KITGARMIN INTL7,15REF(NO 1/NO 2 GMU MAGNETOMETERS)
1P601-1P605, 011-01000-01 CONNECTOR KIT (SB)GARMIN INTL11,12,14REF(NO 1/NO 2 GIA INTEG AVIONICS)2P601-2P606
1P711,1P712, 011-00797-03 CONNECTOR KIT (SB)GARMIN INTL23,24REF(NO 1/NO 2 GEA ENGINE AIRFRAME)2P711,2P712
- 011-00981-00 THERMOCOUPLE (GEA)GARMIN INTL23,24REF
1P331,2P331 011-01012-01 CONNECTOR KITGARMIN INTL17REF(NO 1/NO 2 GTX XPDRS)
- MS25036-156 RING TERMINAL, #8 10-12 AWGREF 7,15 BEST SOURCE(BRAID)
- MS25036-101 RING TERMINAL, (OXY-NRM MIC SW)BEST SOURCE33,344
-----------
-
-
-
34
3635
ECS 500-14971-01 XPDR1A-LL COAX ASSYXPDR2B-LL COAX ASSYXPDR2A-LL COAX ASSY
ECSECSECS
LL
LL
REF 44
REF 44
ECS 500-14971-02
ECS 500-14971-04ECS 500-14971-03
39
GPP1 - PASS 1 PHNGM1 - PASS 1 MICGPP2 - PASS 2 PHNGM2 - PASS 2 MICGPP3 - PASS 3 PHNGM3 - PASS 3 MICGPP4 - PASS 4 PHNGM4 - PASS 4 MICGPP5 - PASS 5 PHNGM5 - PASS 5 MICGPP6 - PASS 6 PHNGM6 - PASS 6 MICGPP7 - PASS 7 PHNGM7 - PASS 7 MICGPP8 - PASS 8 PHNGM8 - PASS 8 MIC
ID CONNECTOR UNITCONNECTOR M/W
(cont)
41 FOR AIRCRAFT WITHOUT AN EXISTING DB AUDIO SYSTEMS 240 PA SPKR AMP INSTALLATION, DISREGARD PA SPKR AMP CONNECTIONS (10AM, 10AN)
005-00375-78 FOR PARTS USED IN NEW PA SPKR AMP INSTALLATION.
ON SHEET 37 AND USE SHEET 45 FOR CONNECTIONS. FOR AIRCRAFT WITH AN EXISTING DB AUDIO SYSTEMS 240 PA SPKR AMP INSTALLATION, USE SHEET
42) THE FOLLOWING INFORMATION IS PROVIDED TO ASSIST THE INSTALLER WITH OLDER SERIAL NUMBER AIRCRAFT THAT MAY HAVE DIFFERENT CONNECTORDESIGNATIONS THAN WHAT ARE REFERENCED IN THIS WIRING DIAGRAM. SEE TABLE BELOW:
PILOT CONTROL WHEEL DISCONNECT J491 96AACOPILOT CONTROL WHEEL DISCONNECT J488 96ABPEDESTAL LIGHTING IN-LINE CONNECTOR P016 95AC
PILOT GROUND BLOCK (EQ BAY) J342 GB89ALJ343 GB89AEJ493 GB89ABJ440 GB89ADJ238 06ANP082 06ASJ239 06ARJ240P083J241
PILOT SPEAKER IN-LINE CONNECTOR J245 06AF
SERIAL NUMBER: LJ-1268FUNCTION / LOCATION STC AIRCRAFT
SERIAL NUMBER: LJ-1654STC AIRCRAFT
COPILOT GROUND BLOCK (EQ BAY)
COPILOT GROUND BLOCK (INST PANEL)PILOT OXYGEN MASK SW IN-LINE
COPILOT OXYGEN MASK SW IN-LINE
PILOT JACKS IN-LINE (JACK SIDE)PILOT JACKS IN-LINE (HARNESS SIDE)
COPILOT JACKS IN-LINE (JACK SIDE)COPILOT JACKS IN-LINE (HARNESS SIDE)
COPILOT SPEAKER IN-LINE CONNECTOR J251
GROUND BLOCK (EQ BAY)
07AN07AS07AR
07AF
AIRCRAFT PRIOR TO SERIAL NUMBER LJ-1306 MAY HAVE A J372 CONNECTOR (WITH MATING CONNECTOR J373) THAT IS A NUMBERED CONNECTOR ASOPPOSED TO THE LETTERED CONNECTOR DEPICTED IN THIS WIRING DIAGRAM. USE THE FOLLOWING "CONVERSION" CHART IF A NUMBERED CONNECTORIS UTILIZED:
28 U27 V26 W25 X9 H8 J
PRE LJ-1306EARLIER S/N DESIGNATION
LJ-1306 AND ON.LATER S/N DESIGNATION
43
J372 PINOUT (NUMBERS) J372 PINOUT (LETTERS)
56
EF
(WIRING DIAGRAM DEPICTS THESE DESIGNATIONS)
40)
REFERENCE TACH-GEN FILTER ASSY., KING AIR C90A/C90GT, 005-00375-93 FOR DETAILS. REFERENCE GENERAL ARRANGEMENT DRAWING005-00375-22 FOR APPLICABILITY.
44
37 FOR THE PA SPKR AMP CONNECTIONS AND DISREGARD SHEET 45. SEE DRAWING "CABIN SPEAKER AMPLIFIER INSTALLATION KING AIR C90" P/N
45 FOR AIRCRAFT THAT ALREADY HAVE THE DB AUDIO SYSTEMS 240 PA AMPLIFIER INSTALLED, INSTALL ONLY THE SOLID WIRES SHOWN. IF THE AIRCRAFTDOES NOT HAVE A PA SYSTEM INSTALLED, INSTALL ALL WIRES SHOWN. NOTE THAT THE WIRES SHOWN AS DASHED WILL NEED TO BE FABRICATED/INSTALLEDAS SEPARATE ITEMS SINCE THEY ARE NOT INCLUDED IN THE FABRICATED HARNESS.
BOM (CONTINUED)
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
4 50
11
NTS
PART ORIDENTIFYING NUMBER
NOMENCLATURE ORDESCRIPTION
DESIGNATORSHTQTY
(NOSE)QTY
(CABIN)QTY
(TAIL)VENDOR
C90() WIRING DIAGRAM BILL OF MATERIAL (BOM)
P681 011-01114-00 CONNECTOR KITGARMIN INTL22REF(GWX RADAR R/T)
P69A1 011-00997-01 CONNECTOR KIT (SB)GARMIN INTL22REF(GDL DATALINK)
1P13471, 011-00813-01 CONNECTOR KITGARMIN INTL31,32,33,REF(NO 1/NO 2 GMA AUDIO MKR)1P13472,
2P13471,2P13472
34,35,36,37
G23AA,G24AA 225973-4 (AMP) 90 DEGREE BNC (MKR RF)36REF
1P8X1,2P8X1, 011-01027-00 CONNECTOR KITGARMIN INTL12,13REF(NO 1 - NO 4 GSA SERVOS)3P8X1,4P8X1
REF
D20419-18 (ITT CANNON) RETAINING SCREWS (ST26)23,244M85049/48-1-3 BACKSHELL (ST26)BEST SOURCE23,242
1P261,2P261 M24308/2-283 CONNECTOR (ST26)BEST SOURCE23,242
P9202 MS3116F14-15SX CONNECTOR (PC920)BEST SOURCE251P9201 MS3116F14-15S CONNECTOR (PC920)BEST SOURCE251
PSALT MS3476L106S CONNECTORBEST SOURCE20(STBY ALT)
PSALT M85049/52-1-10N BACKSHELLBEST SOURCE20
PSAS MS3476L0833S CONNECTORBEST SOURCE20(STBY ASPD)
PSAS M85049/52-1-08N BACKSHELLBEST SOURCE20
52AZ M39029/18-178 20 GA PINS (52AZ)REF52AZ M81511/13-18B1 BACKSHELL (52AZ)BEST SOURCEREF
52AZ A81516F18-38P1 CONNECTOR (52AZ)7,12,15,30
241
1
REF
REF
REF
REF
88AC,88AE M39029/4-110 CONTACT, #20 PIN (88AC,88AE)BEST SOURCE15,18,20,22,29,40
24
88AD,90AA, M39029/5-115 CONTACT, #20 SOCKETBEST SOURCE15,18,20,22,40
20(88AD,90AA,90AC,90AD)
20
52AY M39029/17-173 20 GA SOCKETS (52AY)7,12,15,52AY M81511/13-18B1 BACKSHELL (52AY)BEST SOURCEREF
241
30
VARIOUS M39029/63-368 #20 SOCKETSBEST SOURCE18,32,37(06DE,10AN,19AB,96AA,96AB,97AN)
33 9
19AA,41AA 372-2514-110 (COLLINS) CONTACT (19AA, 41AA)18,1911
GB89() 201328-1 (AMP) CONTACT #16 SOCKET5-10,12,23(GB89AB,GB89AD,GB89AE,GB89AL,
GB89AN)15-18,20,22-25,29,33,34,36,
40
43
VARIOUS LMD-4120-96LD (PYLE NATL) CONTACT #20 SOCKET5,18,19,81(91FX/FY/BY/BV/AD/BR/BS/AK/FZ/BW,
CB/CA/BZ/FF/FG, K105)20,21,30,32,37,40
2
VARIOUS LMD-4122-96LD (PYLE NATL) CONTACT #22 SOCKET14,17,18,77(91BT/BU/CE/BP/CJ/CL/CG/CD/CC,
FJ,BX,GJ)20,21,37,
40
TB105,TB106 M39029/1-101 CONTACT (TB105,TB106)BEST SOURCE6,9,10595AC 60618-1 (AMP) CONTACT (95AC)10,184
60617-5 (AMP) CONTACT (06AN,06AR,07AN,07AR)33,3422 VARIOUS97BC LMD-4116-36L (PYLE NATL) CONTACT (97BC)403
97BS,72AH LMD-4122-36LJ (PYLE NATL) CONTACT (97BS,72AH)33,34,401097BM LMD-4016-36L (PYLE NATL) CONTACT PIN (97BM)39197BR LMD-4022-36LJ (PYLE NATL) CONTACT PIN (97BR)392P269 66010-2 (AMP) CONTACT (P269)401
VARIOUS 60618-8 (AMP) CONTACT PIN (P460,P461,06AS,07AS)33,341097BF M39029/5-116 CONTACT #16 (97BF)BEST SOURCE392
G06BD,G07BD 12B PHN JK (G06BD,G07BD)33,342
PART ORIDENTIFYING NUMBER
NOMENCLATURE ORDESCRIPTION
DESIGNATORSHTQTY
(NOSE)QTY
(CABIN)QTY
(TAIL)VENDOR
C90() WIRING DIAGRAM BILL OF MATERIAL (BOM)
G02AF,G16AH,
44REF
G23AC,G23AE,G17AH,G16AF,G17AF,GRFA,GRFB,G01AF
REF 1P611,1P612, M39012/16-0503 OR1P613,1P614,2P611,2P612,2P613,2P614,
STRAIGHT BNC, CRIMPBEST SOURCE
PAGPS1,PAXM, 225554-6 (AMP) 90 DEGREE TNC, CRIMP44REF
P69A2 225555-6 (AMP) STRAIGHT TNC, CRIMP44REF
1P261,2P261 MS25036-148 RING TERMINAL #4, 18-22 AWGBEST SOURCE23,242
G97AE,GS150 18-200 (VIVISUN) CONNECTOR, ANNUN/SWAEROSPACE OPTICS40REFMIL-C-39029/22-192 CRIMP CONTACTS (20 GA)40REF G97AE,GS150 BEST SOURCE 33
33
CONNECTOR (NOSE SIDE)- BEST SOURCE
CONNECTOR (CABIN SIDE)-REF BEST SOURCE
GBA2, GBA3
GBB2, GBB3BACKSHELL, 22 SIZE-REF BEST SOURCEGBA2, GBA3
GBB2, GBB3REF
REF
CONNECTOR (NOSE SIDE)- BEST SOURCE
CONNECTOR (CABIN SIDE)-REF BEST SOURCE
GBA1
GBB1BACKSHELL, 24 SIZE-REF BEST SOURCEGBA1, GBB1
REFREF
MS3476W22-55P
M85049/52-1-22WMS3476W22-55SMS3476W24-61P
MS3476W24-61SM85049/52-1-24W
CONNECTOR W/ BACKSHELL181 BEST SOURCEP621 MS3126F20-41SXCONNECTOR W/ BACKSHELL20REF BEST SOURCEP42001 MS3116F8-4S
1P261,2P2611P261,2P2611P261,2P26123,2422 BEST SOURCE M39029/63-368 20 GA CRIMP CONTACTS, SOCKETS
90AC,90AD
STBY POWER RELAY391 LEACHG97BF K-J2A-300M 23
PAPGS2
BEST SOURCE
BEST SOURCE
STBY POWER RELAY391 BEST SOURCEG97BF M83536/15-024M 23OROR
225395-6 (AMP)
PA "KEY" RELAY45REF KG100 50-380048-1 41
CONNECTOR, PA SPKR AMP45REF BEST SOURCEP245 MS3106F-16S-1S 41
VARIOUS 81539-23 SEALING PLUG-ARVARIOUS 101-342277-27 CONNECTOR, FEM w/ CONTACTS-ARVARIOUS LMS-01T-TL SPLICE HOUSING-ARVARIOUS 101-342277-25 CONNECTOR, MALE w/ CONTACTS-AR
24
1PVIB1,2PVIB1 MS25036-148 RING TERMINAL #4, 18-22 AWGBEST SOURCE47,488GARMIN47,482
BEST SOURCE47,482011-01855-02MS24308/2-3
BACKSHELL KITCONNECTOR W/ CONTACTS
1PVIB1,2PVIB11PVIB1,2PVIB1
FLAPS-IN-MOTION SENSING - GFC 700 AFCS
91FZ
7
4
19
3
LMD-5001-P(DN MOTION)
6
8
2
91FY
7
4
19
3
LMD-5001-P(UP MOTION)
6
82
1P604NO 1 GIA 63W
15DISC (+) IN 16 (FLAP EXT)
FWDPRESS BULKHEAD
GBA3 GBB3
E
16DISC (+) IN 17 (FLAP RET)
GB89AB
BC
C2
C1C8A22
C12A22
K105 RELAY - FLAP MOTOR
(REF KINGAIR 90 SERIESDRAWING 27-51-01)
D G22117B20
G22118B20
G22117A20
G22118A20
G22119A22
G22120A22N
G22123A22N
G22121A22G22122A22
G22124A22
ACTIVE=FLAP EXTEND
ACTIVE=FLAP RETRACT
(28V = DN)
(28V = UP)
GK101
GK102
1P604-15 1P604-16 GK101 GK102
STATE TABLE
FLAP EXT (DN)
FLAP RETRACT (UP)
NO FLAP MOTION
28 V
GROUND
GROUND
28 V
GROUND
GROUND
ENERGIZED RELAXED
ENERGIZEDRELAXED
RELAXED RELAXED
(PK17-D)
(PK17-E)
2P604NO 2 GIA 63W
15DISC (+) IN 16 (FLAP EXT)
16DISC (+) IN 17 (FLAP RET)
G22124B22
G22119B22
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
5 50
11
NTS
NO 1 GDU 1040A (PIL PFD) 1P10401
ETHERNET OUT 1 AETHERNET OUT 1 B
ETHERNET IN 1 AETHERNET IN 1 B
23
45
POWER GROUND 27
AIRCRAFT POWER 1 35
POWER GROUND 29
GB89AN
LLMM
AIRCRAFT POWER 1 37
CFG MODULE GROUND 1CFG MODULE POWER 23
CFG MODULE DATA 22CFG MODULE CLOCK 43
CFG MODULE(NOTE 13)
1432
GNDVCCDATACLK
BLK
RED
YEL
WHT
FAN MONITOR VALID 14
W
B
SG
ARINC 429 IN 2 A 1617ARINC 429 IN 2 B
ETHERNET OUT 2 AETHERNET OUT 2 B
ETHERNET IN 2 AETHERNET IN 2 B
6789
ARINC 429 IN 1 A 1819ARINC 429 IN 1 B
1P13472 NO 1 GMA 1347D
3637
REV MODE 1REV MODE COMMON
W
B
SG
W
B
SG
REV MODE SELECT 1 5838AIRCRAFT GROUND
NO 1 GDU 1040A PILOT DU, GMC 710 AFCS CTLR
ETHERNET OUT 3 AETHERNET OUT 3 B
ETHERNET IN 3 AETHERNET IN 3 B
10111213
RS 232 OUT 2 4630SIGNAL GROUND
RS 232 IN 2 47
RS 232 OUT 1 4426SIGNAL GROUND
RS 232 IN 1 45
P15001 GDU 1500 (MFD)
8967
ETHERNET IN 2AETHERNET IN 2BETHERNET OUT 2AETHERNET OUT 2B
W
B
O
G
SG
W
B
O
G
SG
2P10401 NO 2 GDU 1040A (COP PFD)
8967
ETHERNET IN 2AETHERNET IN 2BETHERNET OUT 2AETHERNET OUT 2B
W
B
O
G
SG
W
B
O
G
SG
RS 232 OUT 24630 SIGNAL GROUND
RS 232 IN 247
W
B
O
SG
P7101 GMC 710 AFCS CTLR
483
5
RS 232 IN 2SIGNAL GROUNDRS 232 OUT 2
POWER GROUND
W
B
O
SG
261
RS 232 IN 1SIGNAL GROUNDRS 232 OUT 1
W
B
O
SG
W
B
O
SG
7 A/C PWR 1
JJ
15 POWER GROUND
KK
REF SHEET 11
1P1281 NO 1 SAFE128 AXIAL FAN
1
2
AIRCRAFT POWER IN
FAN FAIL OUT3 AIRCRAFT GROUND
NN
W
B
O
G
SG
(NO 1 GIA)
REF SHEET 7W
B
SG(NO 1 GRS)
G31110A22
G31102A22
G31100A22
G31175B22
G31107A22
G31112A22
G31113A22
G31105A22NG31106A22N
G31103A22NG31104A22N
G31101A22
G31108A22NG31109A22
REF SHEET 8(NO 1 GDC)
G31163A22
G31160A22
AIRCRAFT POWER 2 39AIRCRAFT POWER 2 41
G31161A22
G31162A22
PFD 1
5(SEC)
SEE SHT 38
REF RH CB PANEL (A146)
REF SHEET 38
PFD 1
5(PRIM)
SEE SHT 38
MODE
1CTL
SEE SHT 38
ETH
ETH
LIGHT LO 60 G31177A22N D
A
B
C
D
E
F
G
H
J
K
TB105
52 28 VDC LTG HI
LIGHT HI 59 G31176A22
G31176B22
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
6 50
11
NTS
REF PIC COLORS
REF PIC COLORS
FLT TEST USE ONLY
NO 1 GRS 77 AHRS
NO 1 GRS 77 1P771
CFG MODULE GROUND 1171631
POWER GROUND 22
AIRCRAFT POWER 1 18
POWER GROUND 24
GB89AL
KKLL
CFG MODULE
1432
GNDVCCDATACLK
BLK
RED
YEL
WHT
W
B
SG
(GIA 1) ARINC 429 OUT 1 A 1429(GIA 1) ARINC 429 OUT 1 B
(MFD) ARINC 429 OUT 2 A 1328(MFD) ARINC 429 OUT 2 B
W
B
SG
MAG RS 485 IN A 2539
CFG MODULE POWERCFG MODULE DATA
CFG MODULE CLOCK
MAG RS 485 IN B
MAG RS 232 OUT 2 10MAG POWER OUT 9
MAG GROUND 40
W
B
O
SG
FWDPRESS BULKHEAD
W
B
W
B
O
SYSTEM ID PGM 1 2SYSTEM ID PGM 2 3
W
B
SG
W
B
(GIA 1) RS 232 OUT 1 26
(GIA 1) RS 232 IN 1 11SIGNAL GROUND 41
W
B
O
SG
(GDC 1) ARINC 429 IN 1 A 1530(GDC 1) ARINC 429 IN 1 B
W
B
SG
W
B
CROSSIDE GPS RS 232 IN 6SIGNAL GROUND 35
W
B
SG
(FLT TST) SPARE RS 232 OUT 1 23
(FLT TST) SPARE RS 232 IN 1 8SIGNAL GROUND 37
(FLT TST) ARINC 429 OUT 3 A 1227(FLT TST) ARINC 429 OUT 3 B
NO 1 GMU 44
42
89
RS 485 OUT ARS 485 OUT B
RS 232 IN
GROUND
1P441
W
B
W
B
O
W
B
W
B
O6
+12 VDC POWER IN
1P10401 NO 1 GDU 1040A (PIL PFD)W
B
SG
ARINC 429 IN 1 A1819 ARINC 429 IN 1 B
W
B
1P603 NO 1 GIA 63W
1415
56
58
MAIN ARINC 429 IN 6 AMAIN ARINC 429 IN 6 B
MAIN RS 232 IN 6
MAIN RS 232 OUT 6
W
B
SG
57 SIGNAL GROUND
W
B
O
SG
1P74B1 NO 1 GDC 74BW
B
SG
ARINC 429 OUT 2 A2930 ARINC 429 OUT 2 B
W
B
2P603 NO 2 GIA 63W
4645
MAIN RS 232 OUT 2SIGNAL GROUND
W
B
SG
NNMM
LLKKJJ
GGHH
HHGG
AFTPRESS BULKHEAD
W
B
W
B
O
W
B
W
B
O
12
345
FWDPRESS BULKHEAD
G31114A22NG31115A22N
G31116A22
G31117A22
G31119A22
G31111B22
G31120A22
G31122A22
G31111A22
G31118A22
G31121A22
G31117B22
G31119B22
G31118B22
G31117C22
G31118C22
GBA1 GBB1
PP
GBA3 GBB3
52AY 52AZ
G31116B22
HH
FWDPRESS BULKHEAD
GBA2 GBB2
AIRCRAFT POWER 2 20 G31159A22 G31159B22
1
3
SHLD GROUND
SHLD GROUND
AHRS 1
5(SEC)
SEE SHT 38
REF RH CB PANEL (A146)
AHRS 1
5(PRIM)
SEE SHT 38
P15001 GDU 1500 (MFD)W
B
SG
ARINC 429 IN 1 A (AHRS)1819 ARINC 429 IN 1 B (AHRS)
W
BZ*AA G31175B22
(PFD 1) ARINC 429 OUT 3 A 3319(PFD 1) ARINC 429 OUT 3 B
W
B
SG
W
BG31175A22
BRAID
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
7 50
11
NTS
13
27 14
FLT TEST USE ONLY
NO 1 GDC 74B 1P74B1
CFG MODULE GROUND 1214060
POWER GROUND 17
AIRCRAFT POWER 1 55
POWER GROUND 18
GB89AN
BBCC
CFG MODULE
1432
GNDVCCDATACLK
BLK
RED
YEL
WHT
(GIA 1) ARINC 429 OUT 1 A 2627(GIA 1) ARINC 429 OUT 1 B
(PFD 1) ARINC 429 OUT 3 A 3233(PFD 1) ARINC 429 OUT 3 B
CFG MODULE POWERCFG MODULE DATA
CFG MODULE CLOCK
SYSTEM ID PGM 1 6SYSTEM ID PGM 2 71
W
B
SG
(GIA 1) RS 232 OUT 1 11
(GIA 1) RS 232 IN 1 10SIGNAL GROUND 12
(GRS 1) ARINC 429 OUT 2 A 2930(GRS 1) ARINC 429 OUT 2 B
(MFD) ARINC 429 OUT 1 A 4142(MFD) ARINC 429 OUT 1 B
NO 1 GDC 74B AIRDATA
TEMP PROBE POWER OUT 2TEMP PROBE IN HI 3
TEMP PROBE IN LO 4
W
B
O
SG
NO 1 GTP 59 O.A.T. PROBE
POWERSENSELOW
W
B
O
SG
POWER GROUND 19POWER GROUND 20
DDEE
1P10401 NO 1 GDU 1040A (PIL PFD)W
B
SG
ARINC 429 IN 2 A1617 ARINC 429 IN 2 B
REF SHEET 7
(FLT TST) RS 232 OUT 2 14
(FLT TST) RS 232 IN 2 13SIGNAL GROUND 15
REF SHEET 11
(NO 1 AHRS)
(NO 1 GIA)
W
B
SG
W
B
SG
W
B
O
SG
G31123A22N
G31112A22
G31124A22NG31125A22NG31126A22N
G31129A22
G31128A22
G31119B22
G31164A22
AIRCRAFT POWER 2 58 G31165A22
AIRDATA 1
5(SEC)
SEE SHT 38
REF RH CB PANEL (A146)
AIRDATA 1
5(PRIM)
SEE SHT 38
P15001 GDU 1500 (MFD)W
B
SG
ARINC 429 IN 2 A (AIRDATA)1617 ARINC 429 IN 2 B (AIRDATA)
(FLT TST) ARINC 429 OUT 2 A 4445(FLT TST) ARINC 429 OUT 2 B
W
B
SG
G31158A22
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
8 50
11
NTS
13
FLT TEST USE ONLY
NO 2 GDU 1040A (COP PFD) 2P10401
ETHERNET OUT 1 AETHERNET OUT 1 B
ETHERNET IN 1 AETHERNET IN 1 B
23
45
POWER GROUND 27
AIRCRAFT POWER 1 35
POWER GROUND 29
GB89AD
KKLL
AIRCRAFT POWER 1 37
FAN MONITOR VALID 14
W
B
SG
ARINC 429 IN 2 A 1617ARINC 429 IN 2 B
ETHERNET OUT 2 AETHERNET OUT 2 B
ETHERNET IN 2 AETHERNET IN 2 B
67
89
ARINC 429 IN 1 A 1819ARINC 429 IN 1 B
2P13472 NO 2 GMA 1347D
3637
REV MODE 1REV MODE COMMON
W
B
SG
W
B
SG
REV MODE SELECT 1 5838AIRCRAFT GROUND
REF SHEET 15
ETHERNET OUT 3 AETHERNET OUT 3 B
ETHERNET IN 3 AETHERNET IN 3 B
10111213
RS 232 OUT 2 4630SIGNAL GROUND
RS 232 IN 2 47
RS 232 OUT 1 4426SIGNAL GROUND
RS 232 IN 1 45
P15001 GDU 1500 (MFD)
12131011
ETHERNET IN 3AETHERNET IN 3BETHERNET OUT 3AETHERNET OUT 3B
W
B
O
G
SG
W
B
O
G
SG
NO 2 GDU 1040A COPILOT DU
REF SHEET 6
REF SHEET 6
NNCDU ID PROG 1 55
SG
REF SHEET 14
2P1281 NO 2 SAFE128 AXIAL FAN
1
2
AIRCRAFT POWER IN
FAN FAIL OUT3 AIRCRAFT GROUND
W
B
SG
W
B
O
G
SG
W
B
O
G
SG
W
B
O
SG
(NO 2 GIA)
(NO 1 GDU)
(NO 2 GRS)
(GMC 710)
REF SHEET 16(NO 2 GDC)
G31101A22
G31132A22
G31131A22
G31100A22
G31130A22
G31133A22NG31134A22N
G31136A22
G31137A22
G31138A22
G31135A22N
G31166A22
G31162B22
REF RH CB PANEL (A146)
PFD 2
5 SEE SHT 38
REF SHEET 38
ETH
A
B
C
D
E
F
G
H
J
K
TB106
LIGHT LO 60 AAG31179A22N
52 28 V LIGHT HI
G31178A22LIGHT HI 59
G31178B22
L41C22
A
B
C
D
E
F
G
H
J
K
TB105
L35B2221
21
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
9 50
11
NTS
L35B
22
EXTEND AIRCRAFT WIRE AS NECESSARY TO REACH TB 106.
REF PIC COLORS
FLT TEST USE ONLY
GDU 1500 (MFD) P15001
ETHERNET OUT 1 AETHERNET OUT 1 B
ETHERNET IN 1 AETHERNET IN 1 B
2345
W
B
O
G
P69A1 GDL 69A DATA LINK
23222524
ETHERNET IN 1 AETHERNET IN 1 BETHERNET OUT 1 AETHERNET OUT 1 B
W
B
O
G
SG SG
POWER GROUND 27
AIRCRAFT POWER 1 35
POWER GROUND 29
GB89AD
BBFF
AIRCRAFT POWER 1 37
FAN MONITOR VALID 14
ETHERNET OUT 2 AETHERNET OUT 2 B
ETHERNET IN 2 AETHERNET IN 2 B
67
89
2P13472 NO 2 GMA 1347D
5657
REV MODE 2REV MODE COMMON
W
B
SG
W
B
SG
REV MODE SELECT 2 1536AIRCRAFT GROUND
ETHERNET OUT 3 AETHERNET OUT 3 B
ETHERNET IN 3 AETHERNET IN 3 B
1011
1213
RS 232 OUT 2 4630SIGNAL GROUND
RS 232 IN 2 47
RS 232 OUT 1 4426SIGNAL GROUND
RS 232 IN 1 45
P4751 GCU 475 (FMS CTLR)
261
RS 232 IN 1SIGNAL GROUNDRS 232 OUT 1
REF SHEET 6
CDU ID PROG 3 57SG
GDU 1500 MFD, GCU 475 FMS CTLR
REF SHEET 9
W
B
O
SG
1P13472 NO 1 GMA 1347D
5657
REV MODE 2REV MODE COMMON
W
B
SG
W
B
SG
REV MODE SELECT 1 5838AIRCRAFT GROUND
W
B
O
SG
5 AIRCRAFT GROUND
7 AIRCRAFT POWER 1 INJJ
3P1281 NO 3 SAFE128 AXIAL FAN
1
2
AIRCRAFT POWER IN
FAN FAIL OUT
3 AIRCRAFT GROUND
W
B
O
G
SG
W
B
O
G
SG
(NO 1 GDU)
(NO 2 GDU)
G31139A22
G31145A22
G31140A22N
G31146A22
G31141A22N
G31147A22
G31144A22
G31143A22N
G31142A22N
G31107A22
G31130A22
G31167A22
G34166A22
G31162C22
11 LIGHTING BUS HI12 LIGHTING BUS LO
G31170A22G31169A22
IN-LINE
127
P452 95AC
REF HAWKER BEECHCRAFT DRAWING33-17-01
GB89AN
U
ETH
W
B
SG
429A 1 IN (AHRS) 1819 G31111A22
REF SHEET 7(NO 1 GRS)429B 1 IN (AHRS)
W
B
SG
429A 2 IN (AIRDATA) 1617
G31158A22 REF SHEET 8(NO 1 GDC)429B 2 IN (AIRDATA)
LIGHT LO 60 AG31181A22N
LIGHT HI 59 G31180A22
A
B
C
D
E
F
G
H
J
K
TB106
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
10 50
11
NTS
REF SHEET 38
REF SHEET 38
REF SHEET 38
REF PIC COLORS
FLT TEST USE ONLY
NO 1 GIA 63W 1P603
ETHERNET OUT AETHERNET OUT B
ETHERNET IN AETHERNET IN B
23
7677
1P10401 NO 1 GDU 1040A (PIL PFD)
4523
ETHERNET IN 1 AETHERNET IN 1 BETHERNET OUT 1 AETHERNET OUT 1 B
W
B
O
G
SG SG
MAIN ARINC 429 IN 6A 14
MAIN RS-232 IN 6 56
REF SHEET 7
NO 1 GIA 63W
MAIN ARINC 429 IN 6B 15
SIGNAL GROUND 57MAIN RS-232 OUT 6 58
MAIN ARINC 429 IN 5A 12
MAIN RS-232 IN 1 41
MAIN ARINC 429 IN 5B 13
SIGNAL GROUND 42MAIN RS-232 OUT 1 43
MAIN RS-232 OUT 2SIGNAL GROUND
4645
REF SHEET 15
GEA RS-485 1A 2324GEA RS-485 1B
MAIN RS-232 IN 5 53SIGNAL GROUND 54
MAIN RS-232 OUT 5 55
FWDPRESS BULKHEAD
W
B
W
B
W
B
W
B
EE
CC
BBAA
Z*Y*
W
B
O
G
W
B
O
G
W
B
O
GDD
FF
W
B
SG
W
B
O
SG
NO 1 GTX 33 MODE S1P331
NO 1 GEA 71 ENGINE/AIRFRAME1P711
56
RS 485 1ARS 485 1B
W
B
SG
235122 RS 232 IN 1
SIGNAL GROUNDRS 232 OUT 1
W
B
O
SG
RS-485 5A/RS 422 OUT A 3637RS-485 5B/RS 422 OUT B
RS-485 3A/RS 422 IN A 2728RS-485 3B/RS 422 IN B
REF SHEET 19
MAIN RS-232 IN 7 59MAIN RS-232 OUT 7 62
W
B
SG
1P13472 NO 1 GMA 1347D
67
RS-232 OUT 1W
B
SG
RS-232 IN 1
(DME)
SERVO RS-485 A
46
SERVO RS-485 B57
SERVO RS-485 ASERVO RS-485 B
REF SHEET 12(SERVO)
1P74B1 NO 1 GDC 74B
2627
ARINC 429 OUT 1AW
B
SG
W
B
W
BX*W*
W
B
SG
W
B
O
W
B
O
V*U*T*
W
B
O
SG
ARINC 429 OUT 1B
11 RS-232 OUT 112 SIGNAL GROUND10 RS-232 IN 1
W
B
O
SG
(NO 1 AHRS)
(NO 2 AHRS)
GEA RS-485 2A 2526GEA RS-485 2B
W
B
W
B
W
B
SG
NO 2 GEA 71 ENGINE/AIRFRAME2P711
56
RS 485 1ARS 485 1B
W
B
SG
VOICE ALERT DIGITAL AUDIO OUT 69SIGNAL GROUND 64 REF SHEET 35
(DIG AUD)
S*R*
W
B
SG
W
B
SG
W
B
SG
W
B
SG
W
B
SG
W
B
SG
W
B
SG
W
B
O
SG
G31110B22
G31128B22
G31129B22
G34101A22
G34100A22
G34102A22
G34103A22
G34104A22
G34105A22
G34106A22
G34107A22
G34108A22
G31120A22
G31121A22
G34109A22
G31110A22
G31128A22
G31129A22
G34101B22
G34100B22
G34102B22
GBA1 GBB1
ETH ETH
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
11 50
11
NTS
REF PIC COLORS REF PIC COLORS
(COM) POWER GROUND 30
(COM) AIRCRAFT POWER 1 17
GB89AB
FF
132
AIRCRAFT POWERPOWER GROUND
FAN FAIL
NO 1 SAFE328SANDIA PORTED FAN 1P3281
(COM) AIRCRAFT POWER 1 19(COM) AIRCRAFT POWER 1 21
1P601
1P605
78
2931
(NAV) POWER GROUND
(NAV) AIRCRAFT POWER 1(NAV) AIRCRAFT POWER 1
NO 1 GIA 63W, NO 2 GIA 63W, GSA 80 (ROLL)
NO 1 GIA 63W
P*
FWDPRESS BULKHEAD
W
B
W
BK*J*
Q*
1P603
SERVO RS-485 A
46
SERVO RS-485 B57
SERVO RS-485 ASERVO RS-485 B
W
B
SG
W
B
SG
REF SHEET 13
AFTPRESS BULKHEAD
3837
1P8X1 GSA 80 (ROLL)
JT
RS 485 1AW
BRS 485 1B
SE
RS 485 2ARS 485 2B
H SERVO PROGRAM 1G SERVO PROGRAM 2F SERVO PROGRAM 3U STRAP GROUNDR STRAP GROUND
W
B
N AIRCRAFT POWER 1
P AP DISCONNECT
V POWER GROUND
REF SHEET 30
W
B
W
BN*M*
W
B
1P604
24DISCRETE IN* 12
I*
L
(COM) POWER GROUND 30
(COM) AIRCRAFT POWER 1 17
GB89AE
MM
132
AIRCRAFT POWERPOWER GROUND
FAN FAIL
NO 2 SAFE328SANDIA PORTED FAN
2P3281
(COM) AIRCRAFT POWER 1 19(COM) AIRCRAFT POWER 1 21
2P601
2P605
76
2931
(NAV) POWER GROUND
(NAV) AIRCRAFT POWER 1(NAV) AIRCRAFT POWER 1
NO 2 GIA 63W
EE
PRESS BULKHEAD
W
B
W
BDDCC
FF
2P603
SERVO RS-485 A
46
SERVO RS-485 B57
SERVO RS-485 ASERVO RS-485 B
W
B
SG
W
B
SG
W
B
W
BBBAA
2P604
24DISCRETE IN* 12Z
LL
W
B
FWD
22GIA SYSTEM ID PROGRAM 1
KK
38ANNUNCIATE 15 REF SHEET 21(TRAFFIC PROV)
38ANNUNCIATE 15 REF SHEET 21(TRAFFIC PROV)
GB89AL
A
GB89AB
KK
52GS001
2423
REF SHEET 13
G34110A20
G34106A22
G34111A20N
G34165A22N
G34114A22
G34105A22
G34115A22
G34116A22
G34117A20
G34118A20N
G34113A22N
G34119A22N
G34120A22
G34121A22
G34122A22
G34123A22NG34124A22
G34125A22NG34126A22
G34106B22
G34105B22
G34121B22
G34122B22
G22100A20N
G34155A22G34155B22
G34155A22
W
B G34105C22
W
B G34121C22
G22114B20
G22106B20
GBA1 GBB1
GBA3 GBB3
52AY 52AZ
G34117B20
G34120B22
G34126B22
G34116B22
G34110B20
G34114B22
76(NAV) POWER GROUND EEG34112A22N
BB
FWDPRESS BULKHEAD
GBA2 GBB2
3335(NAV) AIRCRAFT POWER 2
(NAV) AIRCRAFT POWER 2 G34164A22
G34164B22
COMM
5NO 1
SEE SHT 38
REF RH CB PANEL (A146)
GIA 1
5(PRIM)
SEE SHT 38
GIA 1
5(SEC)
SEE SHT 38
COMM
5NO 2
SEE SHT 38
GIA 2
5 SEE SHT 38
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
12 50
11
NTS
REF SHEET 38
REF SHEET 38
14
2P8X1 GSA 81 (PITCH TRIM)
JT
RS 485 1AW
BRS 485 1B
SE
RS 485 2ARS 485 2B
H SERVO PROGRAM 1G SERVO PROGRAM 2F SERVO PROGRAM 3U STRAP GROUNDR STRAP GROUND
N AIRCRAFT POWER 1
P AP DISCONNECT
V POWER GROUND
REF SHEET 12
GSA 8X SERVOS (PITCH, PITCH TRIM, YAW)
3P8X1 GSA 80 (PITCH)
JT
RS 485 1ARS 485 1B
SE
RS 485 2ARS 485 2B
H SERVO PROGRAM 1G SERVO PROGRAM 2F SERVO PROGRAM 3U STRAP GROUNDR STRAP GROUND
N AIRCRAFT POWER 1
P AP DISCONNECT
V POWER GROUND
4P8X1 GSA 80 (YAW)
JT
RS 485 1ARS 485 1B
SE
RS 485 2ARS 485 2B
H SERVO PROGRAM 1G SERVO PROGRAM 2F SERVO PROGRAM 3U STRAP GROUNDR STRAP GROUND
W
B
N AIRCRAFT POWER 1
P AP DISCONNECT
V POWER GROUND
W
B
W
B
W
B
W
B
W
B
W
B
W
B
W
B
52GS002
52GS003
52GS004
G34105B22
REF SHEET 12 G34121B22
G34105C22
G34121C22
G34105D22
G34121D22
G34105E22
G34121E22
REF SHEET 30G22112C20
G22107C20
G22103A20N
REF SHEET 30G22115C20
G22108C20
G22102A20N
REF SHEET 30G22116C20
G22109C20
G22101A20N
(AP DISC)
(AP DISC)
(AP DISC)
AFTPRESS BULKHEAD
3837
W
B
W
B2423
W
B
W
B
52AY 52AZ
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
13 50
11
NTS
W
B
O
SG
47
4948
MAIN RS 232 IN 3
MAIN RS 232 OUT 3SIGNAL GROUND G34133A22
NO 2 GIA 63W 2P603
ETHERNET OUT AETHERNET OUT B
ETHERNET IN AETHERNET IN B
23
7677
2P10401 NO 2 GDU 1040A (COP PFD)
4523
ETHERNET IN 1 AETHERNET IN 1 BETHERNET OUT 1 AETHERNET OUT 1 B
W
B
O
G
SG SG
MAIN ARINC 429 IN 6A 14
MAIN RS-232 IN 6 56
REF SHEET 15
MAIN ARINC 429 IN 6B 15
SIGNAL GROUND 57
MAIN ARINC 429 IN 5A 12
MAIN RS-232 IN 1 41
MAIN ARINC 429 IN 5B 13
SIGNAL GROUND 42MAIN RS-232 OUT 1 43
GEA RS-485 2A 2526GEA RS-485 2B
MAIN RS-232 IN 5 53SIGNAL GROUND 54
MAIN RS-232 OUT 5 55
FWD
W
B
W
B
W
B
W
B
Y*
W*
T*S*
W
B
O
G
W
B
O
G
W
B
O
GX*
Z*
W
B
SG
W
B
O
SG
NO 2 GTX 33 MODE S2P331
NO 2 GEA 71 ENGINE/AIRFRAME2P711
78
RS 485 2ARS 485 2B
W
B
SG
235122 RS 232 IN 1
SIGNAL GROUNDRS 232 OUT 1
W
B
O
SG
MAIN RS-232 IN 7 59MAIN RS-232 OUT 7 62
VOICE ALERT DIG. AUDIO OUT 69
W
B
SG
2P13472 NO 2 GMA 1347D
67
RS-232 OUT 1W
B
SG
RS-232 IN 1
SERVO RS-485 A
46
SERVO RS-485 B57
SERVO RS-485 ASERVO RS-485 B
REF SHEET 12(SERVO)
2P74B1 NO 2 GDC 74B
2627
ARINC 429 OUT 1AW
B
SG
W
B
W
BR*Q*
W
B
SG
W
B
O
W
B
O
P*N*M*
W
B
O
SG
ARINC 429 OUT 1B
11 RS-232 OUT 112 SIGNAL GROUND10 RS-232 IN 1
W
B
O
SG
(NO 2 AHRS)
MAIN RS-232 OUT 6 58
MAIN RS-232 OUT 2SIGNAL GROUND
4645 REF SHEET 7
(NO 1 AHRS)
NO 2 GIA 63W
GEA RS-485 1A 2324GEA RS-485 1B
W
B
W
BV*U*
W
B
SG
NO 1 GEA 71 ENGINE/AIRFRAME1P711
78
RS 485 2ARS 485 2B
W
B
SG
ARINC 429 IN 4A 10ARINC 429 IN 4B 11
MAIN ARINC 429 OUT 1A 71MAIN ARINC 429 OUT 1B 70
REF SHEET 21(TRAFFIC SYSTEM)
SIGNAL GROUND 64
K*J*
SS34105C22REFERENCE OPTIONALWX-500 STORMSCOPE
SYSTEM
REF SHEET 35(DIG AUD)
W
B
SG
W
B
SG
W
B
SG
W
B
SG
W
B
O
SG
W
B
SG
W
B
SG
W
B
SG
G34130A22
G31131B22
G34127A22
G34128A22
G34129A22
G34131A22
G34144A22
G34132A22
G31122A22
G34121A22
G34122A22
G34140A22
G34142A22
G34143A22
G34141A22
G34130B22
G31131A22
G34127B22
G34128B22
G34129B22
G34131B22
PRESS BULKHEAD
GBA3 GBB3
91BT
1
95
LMD-6004-P(WX500 DATA)
1216
13
84
W
B
O
W
B
O
ETH ETH
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
14 50
11
NTS
REF PIC COLORS REF PIC COLORS
NO 2 GRS 77 AHRS
NO 2 GRS 77 2P771
CFG MODULE GROUND 1171631
POWER GROUND 22
AIRCRAFT POWER 1 18
POWER GROUND 24
GB89AE
DDEE
CFG MODULE
1432
GNDVCCDATACLK
BLK
RED
YEL
WHT
W
B
SG
(GIA 2) ARINC 429 OUT 1 A 1429(GIA 2) ARINC 429 OUT 1 B
(PFD 2) ARINC 429 OUT 2 A 1328(PFD 2) ARINC 429 OUT 2 B
W
B
SG
MAG RS 485 IN A 2539
CFG MODULE POWERCFG MODULE DATA
CFG MODULE CLOCK
MAG RS 485 IN B
MAG RS 232 OUT 2 10MAG POWER OUT 9
MAG GROUND 40
W
B
O
SG
FWDPRESS BULKHEAD
W
B
W
B
O
SYSTEM ID PGM 1 2SYSTEM ID PGM 2 3
W
B
SG
W
B
(GIA 2) RS 232 OUT 1 26
(GIA 2) RS 232 IN 1 11SIGNAL GROUND 41
W
B
O
SG
(GDC 2) ARINC 429 IN 1 A 1530(GDC 2) ARINC 429 IN 1 B
W
B
SG
W
B
CROSSIDE GPS RS 232 IN 6SIGNAL GROUND 35
W
B
SG
(FLT TST) SPARE RS 232 OUT 1 23
(FLT TST) SPARE RS 232 IN 1 8SIGNAL GROUND 37
(FLT TST) ARINC 429 OUT 3 A 1227(FLT TST) ARINC 429 OUT 3 B
NO 2 GMU 44
42
89
RS 485 OUT ARS 485 OUT B
RS 232 IN
GROUND
2P441
W
B
W
B
O
W
B
W
B
O6
+12 VDC POWER IN
2P10401 NO 2 GDU 1040A (COP PFD)W
B
SG
ARINC 429 IN 1 A1819 ARINC 429 IN 1 B
W
B
2P603 NO 2 GIA 63W
1415
56
58
MAIN ARINC 429 IN 6 AMAIN ARINC 429 IN 6 B
MAIN RS 232 IN 6
MAIN RS 232 OUT 6
W
B
SG
57 SIGNAL GROUND
W
B
O
SG
2P74B1 NO 2 GDC 74BW
B
SG
ARINC 429 OUT 2 A2930 ARINC 429 OUT 2 B
W
B
1P603 NO 1 GIA 63W
4645
MAIN RS 232 OUT 2SIGNAL GROUND
W
B
SG
SG
W
B
W
B
O
W
B
W
B
O
1819
202122
J*
H*F*
D*
YB*
H*G*
XW
FWDPRESS BULKHEAD
G31148A22N
G31152A22
G34141A22
G31151A22
G31153A22
G31132B22
G34140A22
G34109A22
G31149A22N
G31150B22
G31152B22
G31151B22
G31153B22
G31132A22
G31152C22
G31151C22
88AC 88AD
GBA1 GBB1
AFTPRESS BULKHEAD
52AY 52AZ
G31150A22
1
3
SHLD GROUND
SHLD GROUND
AHRS 2
5 SEE SHT 38
REF RH CB PANEL (A146)
BRAID
SEE SHT 7
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
15 50
11
NTS
13
27 14
FLT TEST USE ONLY
GB89AD
NP
CFG MODULE
1432
GNDVCCDATACLK
NO 2 GDC 74B AIRDATA
NO 2 GTP 59 O.A.T. PROBE
POWERSENSELOW
W
B
O
RS
2P10401 NO 2 GDU 1040A (COP PFD)W
B
SG
ARINC 429 IN 2 A1617 ARINC 429 IN 2 B
NO 2 GDC 74B 2P74B1
CFG MODULE GROUND 1214060
POWER GROUND 17
AIRCRAFT POWER 1 55
POWER GROUND 18
BLK
RED
YEL
WHT
(GIA 2) ARINC 429 OUT 1 A 2627(GIA 2) ARINC 429 OUT 1 B
(PFD 2) ARINC 429 OUT 3 A 3233(PFD 2) ARINC 429 OUT 3 B
CFG MODULE POWERCFG MODULE DATA
CFG MODULE CLOCK
SYSTEM ID PGM 1 6SYSTEM ID PGM 2 71
W
B
SG
(GIA 2) RS 232 OUT 1 11
(GIA 2) RS 232 IN 1 10SIGNAL GROUND 12
(GRS 2) ARINC 429 OUT 2 A 2930(GRS 2) ARINC 429 OUT 2 B
TEMP PROBE POWER OUT 2TEMP PROBE IN HI 3
TEMP PROBE IN LO 4
W
B
O
SG
SG
POWER GROUND 19POWER GROUND 20
REF SHEET 15
(FLT TST) ARINC 429 OUT 2 A 4445(FLT TST) ARINC 429 OUT 2 B
(FLT TST) RS 232 OUT 2 14(FLT TST) RS 232 IN 2 13
SIGNAL GROUND 15
REF SHEET 14(NO 2 GIA)
(NO 2 AHRS)
W
B
SG
W
B
O
SG
W
B
SG
G31154A22N
G31137A22
G31155A22NG31156A22NG31157A22N
G34130B22
G34129B22
G31153B22
G31168A22
AIRDATA 2
5 SEE SHT 38
REF RH CB PANEL (A146)
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
16 50
11
NTS
13
FLT TEST USE ONLY
GB89AL
MM
NO 1 GTX 33 1P331
POWER GROUND 27
AIRCRAFT POWER 1 21
(GIA 1) RS 232 OUT 1 23
(GIA 1) RS 232 IN 1 22SIGNAL GROUND 51
NO 1 & NO 2 GTX TRANSPONDERS
EXT SUPPRESSION I/O 31
REF SHEET 19
EXTERNAL IDENT SELECT 12
NN
NO 2 GTX 33 2P331
POWER GROUND 27
AIRCRAFT POWER 1 21
(GIA 2) RS 232 OUT 1 23
(GIA 2) RS 232 IN 1 22SIGNAL GROUND 51
EXT SUPPRESSION I/O 31
EXTERNAL IDENT SELECT 12
S8IDENT
20
21
A191P1 (REF)
YE/BK
YE/BN
REF COPILOT CONTROL WHEEL A192
6
5
J3 (REF) (REF) J1
J1-20-J3-6
J1-21-J3-5
(REF) 96AA
REF COIL CORD INTERFACE HARNESS
S8IDENT
YE/BK
YE/BN
REF PILOT CONTROL WHEEL A191
17
16
J2-20-J3-17
J2-21-J3-16
A192P1 (REF)(REF) J2
20
21
REF SHEET 11
GB89AE
JJ
REF SHEET 14
PRESS BULKHEAD
E*
FWD
D*
P
W
B
O
SG
SG
(NO 2 GIA)
W
B
O
SG
SG
(DME)
(NO 1 GIA)
SKY030A316REF OPTIONAL(TRAFFIC SYSTEM)
G34145A22N
G34132A22
G34146A22
G34150C22
G34152A22
G34151A22
G34150B22
G34147A22N
G34103A22
G34148A22
G34149B22N
G34150A22
G34149A22
GBA1 GBB1
F*
PRESS BULKHEADFWD
GBA3 GBB3
G34146B22
G34148B22
91BU
9
10
1
LMD-6004-P(SUPPR)
124
2
31141AA014-91BU011
XPDR
5 SEE SHT 38
REF RH CB PANEL (A146)
NO 2
XPDR
5 SEE SHT 38
REF RH CB PANEL (A146)
NO 1
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
17 50
11
NTS
EXTERNAL XPDR IDENT SWITCH INTERFACE IS OPTIONAL
ADF-60A
ADF-60A 19AA
48
13
DC POWER
POWER GROUND
51AUDIO HI
8QEC
52AUDIO LO
W
B
3500 HZ
12QEC
4QEC16QEC20QEC
141 KHZ182 KHZ224 KHZ238 KHZ2610 KHZ2720 KHZ3040 KHZ3180 KHZ34100 KHZ35200 KHZ38400 KHZ39800 KHZ421 MHZ43FREQ COM10BFO11ADF/ANT MODE6SELF TEST
A1AF INPUTA1 SHIELD
9ANT B+17ANT B-37SIN MOD41COS MOD
29BEARING C44BEARING H
45BEARING Z36BEARING Y40BEARING X
24DC SIN
32DC SIN33BEARING COMMON28DC COS
NO 2 GIA 63W
19AB ADF CAD 62
3014
SERIAL DATA IN 1A
W
B
SG
SERIAL DATA IN 1B
W
B
SG
42
38
MODE SEL 1
POWER GROUND
29 SERIAL DATA OUT 1A13 SERIAL DATA OUT 1B
47 SHLD GROUND
48 POWER GROUND
15 LOCK MONITOR
23 500 HZ6 1 KHZ
39 2 KHZ5 4 KHZ4 8 KHZ
36 10 KHZ3 20 KHZ
18 40 KHZ34 80 KHZ8 100 KHZ7 200 KHZ
10 400 KHZ9 800 KHZ
27 1 MHZ49 FREQ COM37 BFO19 ADF/ANT MODE1 SELF TEST
17 28 VDC IN
19AC ANT-60
A
E
AF OUTPUT
GROUND
G ANT B+C ANT B-D SIN MODF COS MOD
BHJK
19AA003-19AB02319AA014-19AB00619AA018-19AB03919AA022-19AB00519AA023-19AB00419AA026-19AB03619AA027-19AB00319AA030-19AB01819AA031-19AB03419AA034-19AB00819AA035-19AB00719AA038-19AB01019AA039-19AB00919AA004219AB02719AA043-19AB04919AA010-19AB03719AA011-19AB01919AA006-19AB001
GB89AA
ZCC
89AA0AA-19AB03889AA0BB-19AB006
BBAA
19AA013-89AA00Z19MP001-89AA0CC(18)
MOUNTGROUND
19AJ19AH
19GS003
19AA0A1-19AH001 19AJ001-19AC00AM17/128-RG400 L2201TX
19GS00219GS002-19AC00E (20)
19AG19AF
19AA009-19AF001 12345
19AA017-19AF00219AA037-19AF003WH19AA041-19AF004BL
W
B
W
B
19AG001-19AC00G19AG002-19AC00C
19AG003-19AC00DWH19AG004-19AC00FBL
W
B
W
B
1P13471 NO 1 GMA 1347D
ADF AUDIO IN HI35ADF AUDIO IN LO36
W
B
SG
2P13471 NO 2 GMA 1347D
ADF AUDIO IN HI35ADF AUDIO IN LO36
W
B
SGW
B
SG
88AD88AC
LK
W
B
W
B
W
B
O
25ADF LOCK 19AA025-91CE001
91CE002-19AB015
91BY008-19AB017
19AA048-91BY005
J
W
B
O
SG
G34136A22
G34137A22
G34138A22
G34139A22
G34135B22
G34134B22
G34136D22
G34136C22
FWDPRESS BULKHEAD
91CE
1
3
2
LMD-6006-P(ADF LOCK)
91BY
8
5
6
LMD-6002-P(ADF PWR)
2P606
2P605
60 DISCRETE IN 23A
11 ADF DC SIN32 ADF DC REFERENCE10 ADF DC COS
ADF
2 SEE SHT 38
REF RH CB PANEL (A146)
33 KEY PIN40 KEY PIN
32 MODE SEL 0
CTL-62P621
V CTL IN 1AU
CTL OUT 1AS
28VDC IN
R
T*
S*
R*
I*H*
F*E*
CTL IN 1B
CTL OUT 1B
POWER GROUND
28 VDC LT HI
AUDIO IN HI
Q* LT LO
AUDIO IN LO
AUDIO OUT HIAUDIO OUT LO
W
B
W
B
W
B
W
B
G34136B22
G34139B22
AB
W
B
W
B
CN
W
B
W
BG34135A22
G34134A22
GB89AN
T
G34169A22N
IN-LINE
114
P452 95AC
REF HAWKERBEECHCRAFT G34170A22
G34171A22
28VDC SW OUTK*G34139C22
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
18 50
11
NTS
DWG 33-17-01
DME-42
DME-42 41AA
SERIAL CONTROL SELECT 487
60
59
GB89AE
FF
STRAP COMMON
DC POWER
POWER GROUND
15CH 1 AUDIO HI
1SERIAL DATA 1A-A
54SERIAL CONTROL 1A-A
14SUPPRESSION
41AB
16CH 1 AUDIO LO
2SERIAL DATA 1A-B
55SERIAL CONTROL 1A-B
DME ANTENNA
W
B
41AA060-91BV007(20)
41AA059-89AE0FF(20)
W
B
W
B
41AA014-91BU011
41AB001-41AF001(M17/127-RG393)
FWDPRESSURE
41AF 41AH
41AH001-41AC001(M17/127-RG393)
41AC
DME ANTENNA
41AG
BULKHEAD
FEED--THROUGH
41MP001-89AE0HH(18) HH
MOUNT GROUND
G34154A22
FWDPRESS BULKHEAD
W
BG34153A22
2728
RS 485 3A/RS 422 IN A
W
B
SG
RS 485 3B/RS 422 IN B
W
B
SG
3637
RS 485 5A/RS 422 OUT ARS 485 5B/RS 422 OUT B
1P13471 NO 1 GMA 1347D AUDIO/MKR
DME AUDIO IN HI15DME AUDIO IN LO16
W
B
W
B
SG
2P13471 NO 2 GMA 1347D AUDIO/MKR
DME AUDIO IN HI15DME AUDIO IN LO16
W
B
SG
W
B
SG
8RT ON/OFF (OPEN=ON)
NO 1 GIA 63W 1P603
B*A*
C*
G34107A22
G34108A22
G34153B22
G34153C22
GBA1 GBB1
91BV
7
4
LMD-6002-P(DME PWR)
REF SHEET 17(XPDRS)
G34154B22
DME
2 SEE SHT 38
REF RH CB PANEL (A146)
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
19 50
11
NTS
STBY INSTRUMENTS, AIR/GROUND LOGIC
G31171A22N
ATT
2
STBYSEE SHT 38
REF RH CB PANEL (A146)
STBY ATT 4200
+28VDC POWER INC
LIGHT HI INB
POWER GROUND/LIGHT LOA
P42001
GB89AD
HH
G31173A22G31173B22
G31173C22
G31174A22NG31174B22
G31172A22
CB2-GB2OOH
FWDPRESS BULKHEAD
H
GBA2 GBB2JUNCTION BOX
SSTBY ATT PWR IN GB200H-90AC00S
JTDIODE ORd POWER 1 OUT
91AD
74
1
LMD-5001-PAIR/GND
8
2
GB89AB
K
91GJ009-91AD004
K013
D*DIODE ORd POWER 3 OUT
91FJLMD-7111-PVARIOUS
7
6
FWDPRESS BULKHEAD
F
J37288AE
REF HAWKER BEECHCRAFT DRAWING 31-21-01-2
GB200J-90AC00T
91GJ013-91AD007
89AB00K-91AD001
88AE00F-91FJ007
91AD002-91FJ006
91GJLMD-6004-PAIR/GND
911
13
90AC
90AC0D*-GB20EE SHT 40
GB89AN
L
X*
Y* G31182B22
90AD
G31173D22
G31182A22
T*LIGHTING VOLTS OUT
U*INSTR LIGHT VOLTS IN
S*FIXED DIM LIGHT VOLTS IN
G31184A22
STBY ALTM
VIBRATOR (+)
E LIGHT HI IN
CHASSIS GROUNDC
PSALT
LIGHT LO INF
VIBRATOR (-)A
B
RS
G31186A22NG31187A22N
G31185A22
ALTM
1
STBY
G31127A22V*MSTBY ALTM PWR IN G31127B22
NDIODE ORd POWER 2 OUT W*G31185B22
L20A22
J1
D REF HAWKER BEECHCRAFT DRAWINGS33-01-01 & 33-11-02
(A110 - OVERHEAD CONSOLE)22
STBY AIRSPEED
B LIGHT HI IN
PSAS
LIGHT LO INA
EXISTING (CLK)
(REF TB122)
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
20 50
11
NTS
38DISCRETE IN* 2A
NO 1 GIA 63W 1P605
38DISCRETE IN* 2A
NO 2 GIA 63W 2P605
G31201A22
G31202A22
1514
(FLT HOUR METER) (GROUND = AIRCRAFT IN AIR)
(PWR 1 IN)
(PWR 2 IN)
31
ORFWD
PRESS BULKHEAD
6
EFFECTIVE LJ-1306, LJ-1316, LJ-1318,LJ-1320 AND AFTER.
D12B22
D12A22D11A22
P
S135
REFINSTL
153ZONE
REF HAWKER BEECHCRAFT DRAWING31-21-01-1 (FLT HOUR METER)
EFFECTIVITY:
LJ-1307 THROUGH LJ-1315,LJ-1063 THROUGH LJ-1305,
LJ-1317 & LJ-1319
38
(GND=AIRCRAFT ON GROUND)
(GND=AIRCRAFT ON GROUND)
43
43
J372J373
91AD008-90AC0D*
TRAFFIC SYSTEM (G1000 WIRING)
2P604
2P603
W
B
SG
W
B
SG
G34155A22
1P604
ANNUNCIATE 15 (GPWS MUTE)ANNUNCIATE 13 (SOFTKEY 2)ANNUNCIATE 14 (SOFTKEY 4)ANNUNCIATE 19 (AIR/GND)
ARINC 429 IN 4AARINC 429 IN 4B
MAIN ARINC 429 OUT 1AMAIN ARINC 429 OUT 1B
ANNUNCIATE 15
38363742
1011
7170
38
NO 1 GIA 63W
NO 2 GIA 63W
G34142A22
SKY031A316SW34101A22SW34102A22
SKY28A22
W
B
W
BREFERENCE OPTIONALTRAFFIC SYSTEMSKY032A22
REFERENCE OPTIONALTRAFFIC SYSTEMSKY002A22
REFERENCE OPTIONALTRAFFIC SYSTEM
G34143A22
G34155B22G34156A22G34157A22G34158A22
369
91BSLMD-6001-P(AIRDATA)
147
369
91BRLMD-6001-P(TRF DISPL)
147
W
B
W
B
48
12
91BPLMD-6004-P(GIA DISCR)
159
16
13
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
21 50
11
NTS
FWDPRESS BULKHEAD
GDL 69A DATA LINK / GWX 68 WX R/T PROVISIONS
P69A1 GDL 69A (DATA LINK)
2928
2726
ETHERNET OUT 2 AETHERNET OUT 2 B
ETHERNET IN 2 AETHERNET IN 2 B
W
B
O
G
SG
W
B
O
G
W
B
O
G
VUTS
23222524
ETHERNET IN 1 AETHERNET IN 1 BETHERNET OUT 1 AETHERNET OUT 1 B
REF SHEET 10
31303332
ETHERNET IN 3 AETHERNET IN 3 BETHERNET OUT 3 AETHERNET OUT 3 B
1P13471 NO 1 GMA 1347D
MUSIC IN 2 LEFT56
AUDIO 1 OUT LEFT19AUDIO 1 OUT RIGHT18AUDIO 1 LO17
AUDIO 2 LINE OUT LEFT54AUDIO 2 LINE OUT RIGHT53AUDIO LINE OUT 2 LO52
20 AIRCRAFT GROUND
35 AIRCRAFT POWER INGB89AD
Z
MUSIC IN 2 RIGHT57
MUSIC IN 2 LO76
W
B
O
W
B
O
MUSIC IN 1 LEFT17MUSIC IN 1 RIGHT18MUSIC IN 1 LO37
W
B
O
SG
2P13471 NO 2 GMA 1347D
MUSIC IN 1 LEFT17MUSIC IN 1 RIGHT18MUSIC IN 1 LO37
W
B
O
SG
75 SIGNAL GROUND
70 AUDIO MUTE
N/C
N/C
W
B
O
G
SG
(GDU 1500- MFD)
G34160A22N
G31139A22
G34161A22
G34162A22
G34162B22
88AD88AC
G34165A22
LINK
5
DATA
SEE SHEET 38
REF RH CB PANEL (A146)
ETH
ETH
N/CN/CN/C
MUSIC IN 2 LEFT56MUSIC IN 2 RIGHT57
MUSIC IN 2 LO76
GWX 68 WX RADAR P681
AIRCRAFT POWER 1 7
POWER GROUND 13
RADAR REMOTE POWER OFF 44POWER GROUND 15
ETHERNET OUT AETHERNET OUT B
ETHERNET IN AETHERNET IN B
36373435
W
B
O
G
SG
AIRCRAFT POWER 1 9 P
5
RADAR
WX34100A22
WX34101A22 WX34101B22
WX34102A22
SEE SHEET 38
ETH
AUD MUTE SEL* 4 (GND=ACTIVE)64
61 AUD MUTE SEL 1 (28V=ACTIVE)
G24C22REF HAWKER BEECHCRAFT DWG 32-31-01
G34167A22
(LANDING GEAR CONTROL)
G34168A22
3XDS 258
LIGHT ASSY(STALL WARN)
W22A22 REF HAWKER BEECHCRAFT DWG 27-31-01(STALL WARN)
P258
3
P200A223 PANEL
ASSY
GB89AE
W
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
22 50
11
NTS
28
28
REF PIC COLORS REF PIC COLORS
REF PIC COLORS
14
FLT TEST USE ONLY
NO 1 ST 26 TACH-GEN ADAPTER, NO 1 GEALEFT ENGINE PROP TACH/TURBINE TACH
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
23 50
11
NTS
1(TURB TACH) ANALOG IN 1 HI(TURB TACH) ANALOG IN 1 LO 2
12POWER GROUND
25AIRCRAFT POWER IN13AIRCRAFT POWER IN
1P712 NO 1 GEA 71 ENGINE/AIRFRAME
7431
DIGITAL IN 1ASIGNAL GROUND
7532
DIGITAL IN 2ASIGNAL GROUND
NO 1 ST 26 TACH-GEN ADAPTER J1
15DIGITAL OUT 1 HI14DIGITAL OUT 1 LO
18DIGITAL OUT 2 HI17DIGITAL OUT 2 LO
W
B
SG
W
B
SGGB89AN
Z
M102 IND ENG TURB TACH - L
HP
P115
G
W
B
OW137
4(PROP TACH) ANALOG IN 2 HI(PROP TACH) ANALOG IN 2 LO 5
M100 IND ENG PROP TACH - L
HP
P146
G
W
B
OW135
M100 IND ENG PROP TACH - L
AB
P146
E3C22E4C22
45
REF CHPTR61-41-01
REF CHPTR61-41-01
REF CHPTR77-11-01
1P711
20 AIRCRAFT GROUND
AA
G77103A22N
REF SHEET 41
TACH-GEN FILTER ASSY 1P261
1514
1817
W
B
W
B
G77100A22
G77101A22
12
2513
44
12
45
45
M102 IND ENG TURB TACH - L
AB
P115
E9A22E10A22
12
REF CHPTR77-11-01
12
(TURB TACH) ANALOG IN 1 HI(TURB TACH) ANALOG IN 1 LO
(PROP TACH) ANALOG IN 2 HI(PROP TACH) ANALOG IN 2 LO
OR
G77115A22
G77102A22N
APPLICABLE TO AC S/N LJ-1361, LJ-1363 AND AFTER4
APPLICABLE TO AC S/N LJ-1063 - LJ-1360 AND LJ-13624
35 AIRCRAFT POWER IN
121
CFG MDL GROUNDCFG MDL POWER
1432
GNDVCC
DATACLK
BLK
RED
YEL
WHT
CFG MODULE
4060
CFG MDL DATACFG MDL CLK
BACKSHELL THERMOCOUPLEYELRED
6869
THERMOCOUPLE REF HITHERMOCOUPLE REF LO
56
RS 485 1ARS 485 1B
78
RS 485 2ARS 485 2B
REF SHEET 11
REF SHEET 14
W
B
SG
W
B
SG
G34100B22
G34127B22
(NO 1 GIA)
(NO 2 GIA)
G77116A22REF SHEET 41
13
15
THIS SHEET IS APPLICABLE TO INSTALLATIONS WITH SENIOR AEROSPACE FUEL FLOW SIGNAL CONDITIONER PC920AND SANDIA ST26 TACH-GEN ADAPTER USING STC SA01456WI-D MDL 005-00375-30 REVISION 4 AND PREVIOUSLY APPROVEDREVISIONS. SEE SHEET 47 FOR NEW INSTALLATIONS USING THE VIBRO-METER SIGNAL CONDITIONER P/N85-292-2 BEGINNING AT STC SA01456WI-D MDL 005-00375-30 REVISION 5 AND SUBSEQUENT APPROVED REVISIONS ORFIELDED INSTALLATIONS MODIFIED IN ACCORDANCE WITH GARMIN DOCUMENT 190-00682-06.
NO 2 ST 26 TACH-GEN ADAPTER, NO 2 GEARIGHT ENGINE PROP TACH/TURBINE TACH
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
24 50
11
NTS
2P712 NO 2 GEA 71 ENGINE/AIRFRAME
7431
DIGITAL IN 1ASIGNAL GROUND
7532
DIGITAL IN 2ASIGNAL GROUND
W
B
SG
W
B
SGGB89AD
W
M103 IND ENG TURB TACH - R
E7B22E8B22
M101 IND ENG PROP TACH - R
E1E22E2E22
2P711
35
20
AIRCRAFT POWER IN
AIRCRAFT GROUND
121
CFG MDL GROUNDCFG MDL POWER
1432
GNDVCC
DATACLK
BLK
RED
YEL
WHT
CFG MODULE
4060
CFG MDL DATACFG MDL CLK
BACKSHELL THERMOCOUPLEYELRED
6869
THERMOCOUPLE REF HITHERMOCOUPLE REF LO
Y
56
RS 485 1ARS 485 1B
78
RS 485 2ARS 485 2B
X
9 SYSTEM ID PROGRAM 1
G77104A22
G77105A22
G77106A22N
G77107A22NG77108A22N
REF SHEET 11
REF SHEET 14
W
B
SG
W
B
SG
G34102B22
G34131B22
(NO 1 GIA)
(NO 2 GIA)
G77118A22REF SHEET 41
13
15
1(TURB TACH) ANALOG IN 1 HI(TURB TACH) ANALOG IN 1 LO 2
12POWER GROUND
25AIRCRAFT POWER IN13AIRCRAFT POWER IN
NO 2 ST 26 TACH-GEN ADAPTER J1
15DIGITAL OUT 1 HI14DIGITAL OUT 1 LO
18DIGITAL OUT 2 HI17DIGITAL OUT 2 LO
HP
P116
G
W
B
O
4(PROP TACH) ANALOG IN 2 HI(PROP TACH) ANALOG IN 2 LO 5
HP
P147
G
W
B
O
AB
P147
45
REF CHPTR61-41-01
REF CHPTR61-41-01
REF CHPTR77-11-01
REF SHEET 41
TACH-GEN FILTER ASSY 2P261
1514
1817
W
B
W
B
12
2513
44
12
45
45
AB
P116
12
REF CHPTR77-11-01
12
(TURB TACH) ANALOG IN 1 HI(TURB TACH) ANALOG IN 1 LO
(PROP TACH) ANALOG IN 2 HI(PROP TACH) ANALOG IN 2 LO
ORAPPLICABLE TO AC S/N LJ-1361, LJ-1363 AND AFTER5
APPLICABLE TO AC S/N LJ-1063 - LJ-1360 AND LJ-13625
G77117A22
M103 IND ENG TURB TACH - R
W138
M101 IND ENG PROP TACH - R
W136
THIS SHEET IS APPLICABLE TO INSTALLATIONS WITH SENIOR AEROSPACE FUEL FLOW SIGNAL CONDITIONER PC920AND SANDIA ST26 TACH-GEN ADAPTER USING STC SA01456WI-D MDL 005-00375-30 REVISION 4 AND PREVIOUSLY APPROVEDREVISIONS. SEE SHEET 48 FOR NEW INSTALLATIONS USING THE VIBRO-METER SIGNAL CONDITIONER P/N85-292-2 BEGINNING AT STC SA01456WI-D MDL 005-00375-30 REVISION 5 AND SUBSEQUENT APPROVED REVISIONS ORFIELDED INSTALLATIONS MODIFIED IN ACCORDANCE WITH GARMIN DOCUMENT 190-00682-06.
FFLOW IN LOFLOW IN HI E
PPOWER GROUND
RAIRCRAFT POWER IN
NO 1 GEA 71 ENGINE/AIRFRAME
5859
ANALOG IN 4A HI (FF)ANALOG IN 4A LO (FF)
PC 920 SIGNAL CONDITIONER P9201
HFUEL RATE OUT HI (LH)JFUEL RATE OUT LO (LH)
W
B
W
B
SG
GB89AN
Y
M110 IND FUEL FLOW - L
CD
P131
APPLICABLE TO AC S/N LJ-1283 -LJ-1360 AND LJ-1362
W
B
OW125
REF CHPTR73-31-01
1P712
OR
6
PC920 SIGNAL CONDITIONERLEFT/RIGHT ENGINE FUEL FLOW
MCHASSIS GROUND
CTEMP IN LOTEMP IN HI
D
W
B W133FE
FFLOW IN LOFLOW IN HI E
M110 IND FUEL FLOW - L
CD
P131
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTER
REF CHPTR73-31-01
6C
TEMP IN LOTEMP IN HI
D
W
B W133FE
W
B W125
PPOWER GROUND
RAIRCRAFT POWER IN
P9202
HJ
W
B
MCHASSIS GROUND
NO 2 GEA 71 ENGINE/AIRFRAMEW
B
SG
2P712
FFLOW IN LOFLOW IN HI E
M111 IND FUEL FLOW - R
CD
P132
APPLICABLE TO AC S/N LJ-1283 -LJ-1360 AND LJ-1362
W
B
OW126
REF CHPTR73-31-01
OR
6C
TEMP IN LOTEMP IN HI
D
W
B W134FE
FFLOW IN LOFLOW IN HI E
M111 IND FUEL FLOW - R
CD
P132
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTER
REF CHPTR73-31-01
6C
TEMP IN LOTEMP IN HI
D
W
B W134FE
W
B W126
P9202
P9202
P9201
P9201
LEFT
ENGINE
ENGINE
RIGHT
GB89AD
V
G77109A22
G77110A22NSHLD GND
G77111A22N
G77113A22
G77114A22NSHLD GND
G77112A22N
FUEL RATE OUT HI (RH)FUEL RATE OUT LO (RH)
5859
ANALOG IN 4A HI (FF)ANALOG IN 4A LO (FF)
G77119A22
G77120A22
RGND
RGND
REF SHEET 41
REF SHEET 41
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
25 50
11
NTS
NO 1 GEA 71 ENGINE/AIRFRAME
5859
ANALOG IN 4A HI (FF)ANALOG IN 4A LO (FF)
1P712
CB
D
A
P131
E83A22E85A22
E46B22N
E84A22
REF CHPTR73-31-01
APPLICABLE TO AC S/N LJ-1063 THROUGH LJ-1282
25
NO 2 GEA 71 ENGINE/AIRFRAME
5859
ANALOG IN 4A HI (FF)ANALOG IN 4A LO (FF)
2P712
CB
D
A
P132
E71A22E70A22
E49C22N
E72A22
REF CHPTR73-31-01
APPLICABLE TO AC S/N LJ-1063 THROUGH LJ-1282
25
THIS SHEET IS APPLICABLE TO INSTALLATIONS WITH SENIOR AEROSPACE FUEL FLOW SIGNAL CONDITIONER PC920AND SANDIA ST26 TACH-GEN ADAPTER USING STC SA01456WI-D MDL 005-00375-30 REVISION 4 AND PREVIOUSLY APPROVEDREVISIONS. SEE SHEETS 47 & 48 FOR NEW INSTALLATIONS USING THE VIBRO-METER SIGNAL CONDITIONER P/N85-292-2 BEGINNING AT STC SA01456WI-D MDL 005-00375-30 REVISION 5 AND SUBSEQUENT APPROVED REVISIONS ORFIELDED INSTALLATIONS MODIFIED IN ACCORDANCE WITH GARMIN DOCUMENT 190-00682-06.
NO 1 GEA 71 ENGINE/AIRFRAME
P119 APPLICABLE TO AC S/N LJ-1063 -LJ-1360 AND LJ-1362 WITH
OR
7
LEFT & RIGHT ENGINE TORQUE PRESSURE
46ANALOG IN 5 LO (TORQ)ANALOG IN 5 HI (TORQ)
47
M104 IND ENGINE TORQUE PRESSURE - L
EF
P119
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTERREF CHPTR
77-12-01846
47HG
W129
1P711
1P711
E17A22V
W
B
O
G
E13A22
E15C22
K
L
ANALOG IN 5 LO (TORQ)ANALOG IN 5 HI (TORQ)
NO 2 GEA 71 ENGINE/AIRFRAME
B
P120REF CHPTR77-12-01
OR
946ANALOG IN 5 LO (TORQ)ANALOG IN 5 HI (TORQ)
47 C
M105 IND ENGINE TORQUE PRESSURE - R
EF
P120
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTER
REF CHPTR77-12-01
104647
HG
W130
2P711
2P711
E19A22VE18A22V
W
B
O
G
E14A22
E20C22
K
L
ANALOG IN 5 LO (TORQ)ANALOG IN 5 HI (TORQ)
LEFT
ENGINE
ENGINE
RIGHT
CENTEX AEROSPACE STCSA 10339SC INSTALLED
APPLICABLE TO AC S/N LJ-1063 -LJ-1360 AND LJ-1362 WITHCENTEX AEROSPACE STCSA 10339SC INSTALLED
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
26 50
11
NTS
OR
CENTEXAEROSPACEDRAWING008-7713-3026
A
D
E20A22E14B22V
E14A22V
E20C22N
B
C
AD
E15A22E13B22V
E13A22V
E15B22N
E16A22V
EXISTING
RC
RH TORQUEMETER
5CB 189
X
RH FIREWALL
AB
EXISTINGRH FIRESEAL
DCAB
E19B20VE18B20V
E20B20E14C20V
CDBA
E19C20VE18C20V
E20D20E14D20V
RH TORQUEPRESSURE TRANSMITTER
WIRE NUMBERS (OF EXISTING WIRES) ARE SHOWNFOR REFERENCE ONLY. INSTALLER MUST ENSURE
EE
LH TORQUEMETER
5CB 188
EXISTING
CR
LH FIREWALL
AB
EXISTINGLH FIRESEAL
CDAB
E19B20VE18B20VE20B20
E14C20V
CDBA
E19C20VE18C20VE20D20
E14D20V
LH TORQUEPRESSURE TRANSMITTER
EF
EF
(REF)(REF)(REF)
(REF) (REF) (REF)
(REF)
(REF)
(REF)
(REF)
OR
BLACKHAWKDRAWINGG1000-001
THAT THE CONTINUITY FROM TRANSDUCER CHECKS TO THE GEA 71 AS SHOWN REGARDLESS OFINTERMEDIATE CONNECTIONS.
REF CHPTR77-12-01
OR
CENTEXAEROSPACEDRAWING008-7713-3026
OR
BLACKHAWKDRAWINGG1000-001
WIRE NUMBERS (OF EXISTING WIRES) ARE SHOWNFOR REFERENCE ONLY. INSTALLER MUST ENSURETHAT THE CONTINUITY FROM TRANSDUCER CHECKS TO THE GEA 71 AS SHOWN REGARDLESS OFINTERMEDIATE CONNECTIONS.
NO 1 GEA 71 ENGINE/AIRFRAME
M112 IND TEMP TURBINE INTERSTAGE - L
E113APPLICABLE TO AC S/N LJ-1108 -LJ-1360 AND LJ-1362REF CHPTR
77-21-01
OR
1162
ANALOG IN 6 LO (ITT)ANALOG IN 6 HI (ITT)
63
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTER 12
6263
1P711
1P711
ALML-GRNCHROM-WHTL
EFT
ENGINE
LEFT & RIGHT ENGINE TURBINE GAS TEMPERATURE (ITT)
E112R100ALML-GRN W101
M112 IND TEMP TURBINE INTERSTAGE - L
REF CHPTR77-21-01
ALML-GRNCHROM-WHT
W101G
P237
H
NO 2 GEA 71 ENGINE/AIRFRAME
M113 IND TEMP TURBINE INTERSTAGE - R
E115APPLICABLE TO AC S/N LJ-1108 -LJ-1360 AND LJ-1362REF CHPTR
77-21-01
OR
1162
ANALOG IN 6 LO (ITT)ANALOG IN 6 HI (ITT)
63
APPLICABLE TO AC S/N LJ-1361,LJ-1363 AND AFTER 12
6263
2P711
2P711
ALML-GRNCHROM-WHTI
GHT
ENGINE
E114R101ALML-GRN W102
M113 IND TEMP TURBINE INTERSTAGE - R
REF CHPTR77-21-01
ALML-GRNCHROM-WHT
W102G
P238
HSG
ANALOG IN 6 LO (ITT)ANALOG IN 6 HI (ITT)
SG
R
ANALOG IN 6 LO (ITT)ANALOG IN 6 HI (ITT)
SG
SG
SG
SG
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
27 50
11
NTS
BYPASS TRIMMING RESISTOR BY REMOVING EITHER ALML-GRN WIRE AND CONNECTTO OTHER ALML-GRN WIRE AS SHOWN.
BYPASS TRIMMING RESISTOR BY REMOVING EITHER ALML-GRN WIRE AND CONNECTTO OTHER ALML-GRN WIRE AS SHOWN.
NO 1 GEA 71 ENGINE/AIRFRAME
APPLICABLE TO AC S/N LJ-1361 - LJ-1363 AND AFTER
REF CHPTR79-31-01
17
74ANALOG IN 10 LO (OIL PRESS)ANALOG IN 10 HI (OIL PRESS)
75
3334
1P711
ENG TEMP ANALOG IN 4 HI
LEFT & RIGHT ENGINE OIL PRESSURE/TEMPERATURE
ENG TEMP ANALOG IN 4 LO32SIGNAL GROUND
C
P123
D
FEGH
E35C22E34A22
E27A22E28A22E29A22E30D22
REF CHPTR79-32-01
NO 2 GEA 71 ENGINE/AIRFRAME
REF CHPTR79-31-01
1774
ANALOG IN 10 LO (OIL PRESS)ANALOG IN 10 HI (OIL PRESS)
75
3334
2P711
ENG TEMP ANALOG IN 4 HIENG TEMP ANALOG IN 4 LO
32SIGNAL GROUNDC
P124
D
FEGH
E39D22E40A22
E50A22E33A22E32A22E31C22
REF CHPTR79-32-01
M106 IND OIL TEMP/PRESSURE - L M107 IND OIL TEMP/PRESSURE - R
17
17
NO 1 GEA 71 ENGINE/AIRFRAME
REF CHPTR79-31-01
183334
1P711
ENG TEMP ANALOG IN 4 HIENG TEMP ANALOG IN 4 LO
32SIGNAL GROUND
C
P123
DREF CHPTR79-32-01
NO 2 GEA 71 ENGINE/AIRFRAME
REF CHPTR79-31-01
19
74ANALOG IN 10 LO (OIL PRESS)ANALOG IN 10 HI (OIL PRESS)
75
3334
2P711
ENG TEMP ANALOG IN 4 HIENG TEMP ANALOG IN 4 LO
32SIGNAL GROUND
P124
J
LK
REF CHPTR79-32-01
M106 IND OIL TEMP/PRESSURE - L M107 IND OIL TEMP/PRESSURE - R
18
20
APPLICABLE TO AC S/N LJ-1063 - LJ-1360 AND LJ-1362
W173W
B W174W
BCD
W
B
OW142
E50B22
74ANALOG IN 10 LO (OIL PRESS)ANALOG IN 10 HI (OIL PRESS)
75J
LM
W
B
OW141
E27B22E31A22
E30B22K
LEFT OIL TEMP/PRESS RIGHT OIL TEMP/PRESS
LEFT OIL TEMP/PRESS RIGHT OIL TEMP/PRESS
E27A22
E30C22N
E50A22
E31B22N
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
28 50
11
NTS
7
8
A191P1 (REF)
REF COP CONTROL WHEEL A192
8
7
J3 (REF) (REF) J1
J1-7-J3-8
J1-8-J3-7
(REF) 96AA
REF COIL CORD INTERFACE HARNESS
S3PITCH SYNC/CWS
BL
VT
REF PILOT CONTROL WHEEL A191
12
10
A192P1 (REF)(REF) J2
1P604
12DISCRETE IN * 4
NO 1 GIA 63W PRESS BULKHEAD
N
M
R
P
1P605
73DISCRETE IN* 17A
G*
PRESS BULKHEAD
F*
I*
H*
FWD
AUTOPILOT YOKE SWITCHES: MET & CWS
13DISCRETE IN * 5
18DISCRETE IN * 8
19DISCRETE IN * 9
39DISCRETE IN* 3A
40DISCRETE IN* 4A
41DISCRETE IN* 5A42DISCRETE IN* 6A
2P604
12DISCRETE IN * 4
NO 2 GIA 63W
2P605
73DISCRETE IN* 17A
13DISCRETE IN * 5
18DISCRETE IN * 8
19DISCRETE IN * 9
39DISCRETE IN* 3A40DISCRETE IN* 4A
41DISCRETE IN* 5A
42DISCRETE IN* 6A
GNYEOR
RDBNBK
C
F
B
D
E
A
S4MET (RH)
S5MET (LH)
NS DN
ARM
ARM
NS UPTRI
M
654
321
7
8
S3PITCH SYNC/CWS
BL
VT
GNYEOR
RDBNBK
C
F
B
D
E
A
S4MET (RH)
S5MET (LH)
NS DN
ARM
ARM
NS UPTRI
M
654
321
J2-7-J3-19
J2-8-J3-18
1918
J4 (REF)(REF) 96AB
6
1
54
32
J1-6-J4-6J1-5-J4-5J1-4-J4-4
J1-3-J4-3J1-2-J4-2J1-1-J4-1
J2-6-J4-15J2-5-J4-14J2-4-J4-13
J2-3-J4-12
J2-1-J4-10J2-2-J4-1111
131415
GB89AN
X
GB89AD
U
PRESS BULKHEADFWD
J372 (REF)(REF) 88AE
HJ
GB89AB
A
FWD
G27100B22G27100C22
G27102A22G27102B22G27103B22G27103C22
G27105B22G27105C22G27106B22G27106C22
G27111A22N
G27104C22G27104B22
G27107C22G27107B22G27109C22G27109B22G27110C22G27110B22
G27100A22
G27104A22
G27110A22
G27109A22
G27107A22
G27105A22
G27106A22
G27103A22
G27101A22NG27101B22
G27108B22
G27108A22N
GBA2 GBB2
GBA3 GBB3
GO AROUND SWEXISTING
(LH) THROTTLE
C153A22C154A22
IN-LINEJ194 (REF)(REF) P194
1C4C
BLKWHT
SHT 30 S3-GND
SHT 30 S3-GND
SIZE
SCALE
DWG. NO. REV.
SHT. OF
005-W0022-00
29 50
11
NTS
30
30
30
43
A191P1 (REF)
REF COP CONTROL WHEEL A192
J3 (REF)(REF) J1
(REF) 96AA
REF COIL CORD INTERFACE HARNESS
REF PILOT CONTROL WHEEL A191
A192P1 (REF)(REF) J2
1P604NO 1 GIA 63W
H*
PRESS BULKHEAD
F*D*
T
V
J*
11AP DISC IN
2P604NO 2 GIA 63W
11AP DISC IN
1314
2215
9
1314
2215
9
J1-9-J3-2
J1-13-J3-1
2
1
J2-9-J3-13
J2-13-J3-12
13
12
9
7
J4 (REF)(REF) 96ABJ1-14-J4-9
J1-22-J4-8J1-15-