c:documents and settingsschankdesktop -w0022-00...

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



DESIGNATORSHTQTY

(NOSE)QTY

(CABIN)QTY

(TAIL)VENDOR


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



DESIGNATORSHTQTY

(NOSE)QTY

(CABIN)QTY

(TAIL)VENDOR


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



6789


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



10111213

RS 232 OUT 2 4630SIGNAL GROUND

RS 232 IN 2 47


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


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


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


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


POWER GROUND 17

AIRCRAFT POWER 1 55

POWER GROUND 18

GB89AN

BBCC

CFG MODULE

1432

GNDVCCDATACLK

BLK

RED

YEL

WHT




CFG MODULE CLOCK


W

B

SG

(GIA 1) RS 232 OUT 1 11


(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


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


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)


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



23

45

POWER GROUND 27

AIRCRAFT POWER 1 35

POWER GROUND 29

GB89AD

KKLL

AIRCRAFT POWER 1 37


W

B

SG




67

89


2P13472 NO 2 GMA 1347D

3637


W

B

SG

W

B

SG


REF SHEET 15



10111213


RS 232 IN 2 47


RS 232 IN 1 45

P15001 GDU 1500 (MFD)

12131011


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


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


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



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




67

89

2P13472 NO 2 GMA 1347D

5657


W

B

SG

W

B

SG




1011

1213


RS 232 IN 2 47


RS 232 IN 1 45

P4751 GCU 475 (FMS CTLR)

261


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


W

B

SG

W

B

SG


W

B

O

SG

5 AIRCRAFT GROUND

7 AIRCRAFT POWER 1 INJJ


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


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 RS-232 IN 1 41



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


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


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


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


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


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


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


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


G22108C20

G22102A20N


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



23

7677

2P10401 NO 2 GDU 1040A (COP PFD)

4523


W

B

O

G

SG SG


MAIN RS-232 IN 6 56

REF SHEET 15


SIGNAL GROUND 57


MAIN RS-232 IN 1 41



GEA RS-485 2A 2526GEA RS-485 2B

MAIN RS-232 IN 5 53SIGNAL GROUND 54


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


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


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 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


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


NO 2 GRS 77 AHRS

NO 2 GRS 77 2P771


POWER GROUND 22

AIRCRAFT POWER 1 18

POWER GROUND 24

GB89AE

DDEE

CFG MODULE

1432

GNDVCCDATACLK

BLK

RED

YEL

WHT

W

B

SG



W

B

SG

MAG RS 485 IN A 2539


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


W

B

SG

W

B

(GIA 2) RS 232 OUT 1 26


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


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


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


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


NO 2 GDC 74B 2P74B1


POWER GROUND 17

AIRCRAFT POWER 1 55

POWER GROUND 18

BLK

RED

YEL

WHT




CFG MODULE CLOCK


W

B

SG

(GIA 2) RS 232 OUT 1 11


(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) 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


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


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


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


NO 2

XPDR

5 SEE SHT 38


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


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


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


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



W

B

O

G

SG

W

B

O

G

W

B

O

G

VUTS

23222524


REF SHEET 10

31303332


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


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



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

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


NO 1 ST 26 TACH-GEN ADAPTER J1

15DIGITAL OUT 1 HI14DIGITAL OUT 1 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


7532


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



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


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


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


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


D

W

B W134FE


M111 IND FUEL FLOW - R

CD

P132


REF CHPTR73-31-01

6C


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


G77119A22

G77120A22

RGND

RGND

REF SHEET 41

REF SHEET 41

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-W0022-00

25 50

11

NTS


5859


1P712

CB

D

A

P131

E83A22E85A22

E46B22N

E84A22

REF CHPTR73-31-01

APPLICABLE TO AC S/N LJ-1063 THROUGH LJ-1282

25


5859


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.


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)


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


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.


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


M113 IND TEMP TURBINE INTERSTAGE - R

E115APPLICABLE TO AC S/N LJ-1108 -LJ-1360 AND LJ-1362REF CHPTR

77-21-01

OR

1162


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


SG

R


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.


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


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


REF CHPTR79-31-01

183334

1P711


32SIGNAL GROUND

C

P123

DREF CHPTR79-32-01


REF CHPTR79-31-01

19


75

3334

2P711


32SIGNAL GROUND

P124

J

LK

REF CHPTR79-32-01

M106 IND OIL TEMP/PRESSURE - L M107 IND OIL TEMP/PRESSURE - R

18

20


W173W

B W174W

BCD

W

B

OW142

E50B22


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


S3PITCH SYNC/CWS

BL

VT


12

10


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

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