notes rev description date ecostatic.garmin.com/pumac/g1000:beechcraftbonanzaa36_g36...ar...

11
NOTES TITLE SIZE SCALE DWG. NO. REV. SHT. OF DATE DRWN. CHKD. RLS'D. PROJ. MGR. BY HARNESS INSTALLATION, GTS 820 OPTION HAWKER BEECHCRAFT G36 005-00620-09 3 11 1 NONE DER REVIEW REQ'D DWH 6/9/10 NOTES SHIELDED TWISTED 3 CONDUCTOR W B O SHIELDED TWISTED 2 CONDUCTOR W B SHIELDED SINGLE CONDUCTOR ? SPECIFIC NOTE SOLDER SLEEVE SPLICE ENVIRONMENTAL CRIMP SPLICE NEW WIRING GARMIN: 1200 E 151ST STREET OLATHE, KS 66062 1-888-606-5482 www.GARMIN.com HAWKER BEECHCRAFT CORPORATION: 888.727.4344 or 316.676.3100 www.hawkerbeechraft.com/RAPID SHIELDED TWISTED 4 CONDUCTOR ETHERNET PRIMARY COLOR/DASH COLOR W/B B/W O/W W/O 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 EXCEED M22759/16 SPECIFICATION OR M81044/12 SPECIFICATION. UNLESS OTHERWISE SPECIFIED, ALL SHIELDED WIRE IS 24 AWG MINIMUM AND SHALL MEET OR EXCEED M27500 SPECIFICATION. THE FOLLOWING SYMBOLS ARE USED IN THIS DRAWING: 10. 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 THE BEST AVAILABLE SOURCE. VENDOR CONTACT INFORMATION: 11 15. CONNECT THE COAXIAL CABLES ACCORDING TO THE FOLLOWING TABLES. CONNECTOR ID IS SPECIFIED IN GARMIN DWG. 320-00609-XX: REV DESCRIPTION DATE ECO 1 INITIAL RELEASE 6/9/10 ----- 12 USE HEATSHRINK TUBING M23053/5-104-Y FOR INSULATING FLOATING SHIELDS ON SINGLE-CONDUCTOR. USE HEATSHRINK TUBING M23053/5-105-Y FOR INSULATING FLOATING SHIELDS ON TWISTED PAIR CONDUCTORS AND TWISTED TRIPLE CONDUCTORS. USE HEATSHRINK TUBING M23053/5-106-Y FOR INSULATING FLOATING SHIELDS ON ETHERNET CABLE. USE HEATSHRINK TUBING M23053/5-103-Y AS REQUIRED FOR ISOLATING MULTIPLE ADJACENT SHIELD BRAIDS. THE LAST "-Y" IN THE PART NUMBERS REFERENCED REPRESENTS COLOR. COLOR USED IS INSTALLER/FABRICATOR'S PREFERENCE. SOLDER SLEEVE AS83519/1-2 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED SINGLE CONDUCTOR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-14 OR S2974-2 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-2 SOLDER SLEEVES. SOLDER SLEEVE AS83519/1-3 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF TWISTED PAIR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-15 OR S2974-3 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-3 SOLDER SLEEVES. SOLDER SLEEVE AS83519/1-4 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED TWISTED TRIPLE CABLES AND ETHERNET CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-23 OR S2974-4 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-4 SOLDER SLEEVES. TOLERANCE .XX ± .010 .XXX ± .005 HOLES ± .003 ANGLES +/- 0.5° UNLESS NOTED OTHERWISE ENGLISH UNITS 3. ROUTE HARNESS ASSEMBLY AS SHOWN. IN AREAS WHERE THE NEW WIRING IS ROUTED WITH OR IN PLACE OF EXISTING WIRING, THERE MAY BE SOME VARIANCE BETWEEN AIRCRAFT. ANY DIFFERENCES TO WIRE ROUTING SHOWN MUST BE ROUTED IN ACCORDANCE WITH SAE AS50881, PARA. 3.10.6 AND/OR AC 43.13-1B CHAPTER 11, SECTIONS 9 THRU 11. 4. ELECTRICAL EQUIPMENT AND SUPPORTING BRACKETS SHALL BE ELECTRICALLY BONDED. SURFACE PREPARATION SHALL BE PER SAE ARP 1870, SECTION 5. THE ELECTRICAL BOND SHALL ACHIEVE 2.5 MILLIOHMS OR LESS BETWEEEN EACH FAYING INTERFACE AND AIRCRAFT STRUCTURE. COMPLIANCE SHALL BE VERIFIED BY INSPECTION USING A CALIBRATED MILLIOHMETER. ELECTRICAL BOND OF EQUIPMENT SHALL BE PERFORMED WITH THE HARNESS CONNECTOR DISCONNECTED. 5. SECURE NEW HARNESS TO EXISTING HARNESS. REMOVE EXISTING ZIPTIES, TIE STRING, AND INSTALL NEW ZIPTIES. 6. ROUTE THROUGH LIGHTENING HOLE WITH EXISTING HARNESS. ENSURE HARNESS IS NOT IN CONTACT WITH STRUCTURE AND HARNESS IS PROTECTED BY GROMMET M22529/2-4R-25. 7. ROUTE COAX ASSEMBLY AND HARNESS AS SHOWN. WHERE HARNESS ROUTES BEHIND FLOOR STRUCTURE (NOT SHOWN), PROTECT WITH ITEM 30. 8. COAX LENGTH SPECIFIED IN GARMIN DRAWING 320-00609-XX MUST BE MAINTAINED. DO NOT SHORTEN COAX CABLES, INSTALL AS SHOWN. 9. REFER TO GENERAL ARRANGEMENT DRAWING 005-00620-06 FOR COMPONENT LOCATIONS AND INSTALLATION DRAWING REFERENCES. TWO TERMINALS MAX PER GARMIN CONNECTOR SHIELD BLOCK STUD. 13. TABLE OF CONTENTS: 320-00609-05 COAX ASSY. CONNECTOR ID LRU MATING CONNECTOR GTSP1T-GPAP1-YEL GTS 820 J1 (TOP) GTSP2T-GPAP2-BLK GTS 820 J2 (TOP) GTSP1T-GPAP3-BLU GTS 820 J3 (TOP) GTSP2T-GPAP4-RED GTS 820 J4 (TOP) GTSP1T-GPAP1-YEL GPA 65 J1U GTSP2T-GPAP2-BLK GPA 65 J2U GTSP1T-GPAP3-BLU GPA 65 J3U GTSP2T-GPAP4-RED GPA 65 J4U 320-00609-06 COAX ASSY. CONNECTOR ID LRU MATING CONNECTOR GPAP1-TAP1-YEL GPA 65 J1A GPAP2-TAP2-BLK GPA 65 J2A GPAP3-TAP3-BLU GPA 65 J3A GPAP4-TAP4-RED GPA 65 J4A GPAP1-TAP1-YEL TOP GA 58 J1 GPAP2-TAP2-BLK TOP GA 58 J2 GPAP3-TAP3-BLU TOP GA 58 J3 GPAP4-TAP4-RED TOP GA 58 J4 320-00609-07 COAX ASSY. CONNECTOR ID LRU MATING CONNECTOR GTSP1B-BAP1-YEL GTS 820 J1 (BOTTOM) GTSP2B-BAP2-BLK GTS 820 J2 (BOTTOM) GTSP3B-BAP3-BLU GTS 820 J3 (BOTTOM) GTSP4B-BAP4-RED GTS 820 J4 (BOTTOM) GTSP1B-BAP1-YEL BOTTOM GA 58 J1 GTSP2B-BAP2-BLK BOTTOM GA 58 J2 GTSP3B-BAP3-BLU BOTTOM GA 58 J3 GTSP4B-BAP4-RED BOTTOM GA 58 J4 SHEET DESCRIPTION 1 NOTES 2 B.O.M. 3 WIRE ROUTING TOP VIEW 4 WIRE ROUTING, SIDE VIEW 5 VIEW A-A, AFT CABIN LOOKING RIGHT 6 VIEW E-E, 320-00609-01 HARNESS, DETAIL F, FRAME STATION FEEDTHRU & DETAIL G, HARNESS TIE DOWN DETAIL 7 VIEW D-D, COAX ROUTING UNDER FLOOR 8 DETAIL J - GIA63W TERMINATIONS & DETAIL K - GDL69A TERMINATION 10 VIEW B-B, BACK OF INSTRUMENT PANEL 11 VIEW C-C - CABIN OVERHEAD 16. INSTALLL CIRCUIT BREAKER (ITEM 28) IN EXISTING TRAFFIC ALERT POSITION AS SHOWN. ROUTE NEW WIRE WITH EXISTING CIRCUIT BREAKER PANEL WIRING. DETAIL L - P651 TERMINATION & DETAIL M - CIRCUIT BREAKER TERMINATION 14 17. FOR THOSE STANDOFFS LOCATED AT A FRAME STATION, POSITION THE STANDOFF ALONG EDGE OF FEEDTHRU, MAINTAINING MINIMUM 2D FROM EDGE OF FEEDTHRU CUTOUT AND INSTALL GROMMET (ITEM 15) AROUND FEEDTHRU. 18. COIL EXCESS COAX IN BAY AS SHOWN. DO NOT ADJUST THE LENGTH OF THE COAXIAL CABLE ASSEMBLIES IN ANY WAY. 9 2 ADDED NOTE 19 7/22/10 73725 DWH 6/9/10 DWH 6/9/10 DWH 6/9/10 3 ADDED ALTERNATE PART NUMBERS 8/25/10 74607

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Page 1: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

NOTES

TITLE

SIZE

SCALE

DWG. NO. REV.

SHT. OF

DATE

DRWN.

CHKD.

RLS'D.

PROJ.MGR.

BY

HARNESS INSTALLATION, GTS 820 OPTIONHAWKER BEECHCRAFT G36

005-00620-09 3

111NONE DER REVIEW REQ'D

DWH 6/9/10

NOTES

SHIELDED TWISTED 3 CONDUCTOR

W

B

O

SHIELDED TWISTED 2 CONDUCTORW

B

SHIELDED SINGLE CONDUCTOR

? SPECIFIC NOTE

SOLDER SLEEVE SPLICE

ENVIRONMENTAL CRIMP SPLICENEW WIRING

GARMIN: 1200 E 151ST STREETOLATHE, KS 660621-888-606-5482www.GARMIN.com

HAWKER BEECHCRAFT CORPORATION:888.727.4344 or 316.676.3100www.hawkerbeechraft.com/RAPID

SHIELDED TWISTED 4 CONDUCTORETHERNETPRIMARY COLOR/DASH COLOR

W/B

B/W

O/W

W/O

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 EXCEED M22759/16 SPECIFICATION OR M81044/12 SPECIFICATION. UNLESS OTHERWISE SPECIFIED, ALL SHIELDED WIRE IS 24 AWG MINIMUM AND SHALL MEET OR EXCEED M27500 SPECIFICATION. THE FOLLOWING SYMBOLS ARE USED IN THIS DRAWING:

10. 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 THE BEST AVAILABLE SOURCE. VENDOR CONTACT INFORMATION:

11

15. CONNECT THE COAXIAL CABLES ACCORDING TO THE FOLLOWING TABLES. CONNECTOR ID IS SPECIFIED IN GARMIN DWG. 320-00609-XX:

REV DESCRIPTION DATE ECO1 INITIAL RELEASE 6/9/10 -----

12 USE HEATSHRINK TUBING M23053/5-104-Y FOR INSULATING FLOATING SHIELDS ON SINGLE-CONDUCTOR.

USE HEATSHRINK TUBING M23053/5-105-Y FOR INSULATING FLOATING SHIELDS ON TWISTED PAIR CONDUCTORS AND TWISTED TRIPLE CONDUCTORS.

USE HEATSHRINK TUBING M23053/5-106-Y FOR INSULATING FLOATING SHIELDS ON ETHERNET CABLE.

USE HEATSHRINK TUBING M23053/5-103-Y AS REQUIRED FOR ISOLATING MULTIPLE ADJACENT SHIELD BRAIDS.THE LAST "-Y" IN THE PART NUMBERS REFERENCED REPRESENTS COLOR. COLOR USED IS INSTALLER/FABRICATOR'S PREFERENCE.

SOLDER SLEEVE AS83519/1-2 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED SINGLE CONDUCTOR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-14 OR S2974-2 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-2 SOLDER SLEEVES.

SOLDER SLEEVE AS83519/1-3 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF TWISTED PAIR CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-15 OR S2974-3 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-3 SOLDER SLEEVES.

SOLDER SLEEVE AS83519/1-4 ALONG WITH BRAID WIRE IS USED TO TERMINATE SHIELDS OF SHIELDED TWISTED TRIPLE CABLES AND ETHERNET CABLES. BRAID WIRE LENGTH SHOULD NOT EXCEED 4 INCHES. NAS1745-23 OR S2974-4 ARE ACCEPTABLE ALTERNATIVES TO AS83519/1-4 SOLDER SLEEVES.

TOLERANCE

.XX ± .010 .XXX ± .005HOLES ± .003

ANGLES +/- 0.5°

UNLESS NOTED OTHERWISE

ENGLISH UNITS

3. ROUTE HARNESS ASSEMBLY AS SHOWN. IN AREAS WHERE THE NEW WIRING IS ROUTED WITH OR IN PLACE OF EXISTING WIRING, THERE MAY BE SOME VARIANCE BETWEEN AIRCRAFT. ANY DIFFERENCES TO WIRE ROUTING SHOWN MUST BE ROUTED IN ACCORDANCE WITH SAE AS50881, PARA. 3.10.6 AND/OR AC 43.13-1B CHAPTER 11, SECTIONS 9 THRU 11.

4. ELECTRICAL EQUIPMENT AND SUPPORTING BRACKETS SHALL BE ELECTRICALLY BONDED. SURFACE PREPARATION SHALL BE PER SAE ARP 1870, SECTION 5. THE ELECTRICAL BOND SHALL ACHIEVE 2.5 MILLIOHMS OR LESS BETWEEEN EACH FAYING INTERFACE AND AIRCRAFT STRUCTURE. COMPLIANCE SHALL BE VERIFIED BY INSPECTION USING A CALIBRATED MILLIOHMETER. ELECTRICAL BOND OF EQUIPMENT SHALL BE PERFORMED WITH THE HARNESS CONNECTOR DISCONNECTED.

5. SECURE NEW HARNESS TO EXISTING HARNESS. REMOVE EXISTING ZIPTIES, TIE STRING, AND INSTALL NEW ZIPTIES.

6. ROUTE THROUGH LIGHTENING HOLE WITH EXISTING HARNESS. ENSURE HARNESS IS NOT IN CONTACT WITH STRUCTURE AND HARNESS IS PROTECTED BY GROMMET M22529/2-4R-25.

7. ROUTE COAX ASSEMBLY AND HARNESS AS SHOWN. WHERE HARNESS ROUTES BEHIND FLOOR STRUCTURE (NOT SHOWN), PROTECT WITH ITEM 30.

8. COAX LENGTH SPECIFIED IN GARMIN DRAWING 320-00609-XX MUST BE MAINTAINED. DO NOT SHORTEN COAX CABLES, INSTALL AS SHOWN.

9. REFER TO GENERAL ARRANGEMENT DRAWING 005-00620-06 FOR COMPONENT LOCATIONS AND INSTALLATION DRAWING REFERENCES.

TWO TERMINALS MAX PER GARMIN CONNECTOR SHIELD BLOCK STUD.

13. TABLE OF CONTENTS:

320-00609-05 COAX ASSY.

CONNECTOR ID LRUMATING

CONNECTORGTSP1T-GPAP1-YEL GTS 820 J1 (TOP)

GTSP2T-GPAP2-BLK GTS 820 J2 (TOP)

GTSP1T-GPAP3-BLU GTS 820 J3 (TOP)

GTSP2T-GPAP4-RED GTS 820 J4 (TOP)

GTSP1T-GPAP1-YEL GPA 65 J1U

GTSP2T-GPAP2-BLK GPA 65 J2U

GTSP1T-GPAP3-BLU GPA 65 J3U

GTSP2T-GPAP4-RED GPA 65 J4U

320-00609-06 COAX ASSY.

CONNECTOR ID LRUMATING

CONNECTORGPAP1-TAP1-YEL GPA 65 J1A

GPAP2-TAP2-BLK GPA 65 J2A

GPAP3-TAP3-BLU GPA 65 J3A

GPAP4-TAP4-RED GPA 65 J4A

GPAP1-TAP1-YEL TOP GA 58 J1

GPAP2-TAP2-BLK TOP GA 58 J2

GPAP3-TAP3-BLU TOP GA 58 J3

GPAP4-TAP4-RED TOP GA 58 J4

320-00609-07 COAX ASSY.

CONNECTOR ID LRUMATING

CONNECTORGTSP1B-BAP1-YEL GTS 820 J1 (BOTTOM)

GTSP2B-BAP2-BLK GTS 820 J2 (BOTTOM)

GTSP3B-BAP3-BLU GTS 820 J3 (BOTTOM)

GTSP4B-BAP4-RED GTS 820 J4 (BOTTOM)

GTSP1B-BAP1-YEL BOTTOM GA 58 J1

GTSP2B-BAP2-BLK BOTTOM GA 58 J2

GTSP3B-BAP3-BLU BOTTOM GA 58 J3

GTSP4B-BAP4-RED BOTTOM GA 58 J4

SHEET DESCRIPTION1 NOTES

2 B.O.M.

3 WIRE ROUTING TOP VIEW

4 WIRE ROUTING, SIDE VIEW

5 VIEW A-A, AFT CABIN LOOKING RIGHT

6 VIEW E-E, 320-00609-01 HARNESS, DETAIL F, FRAME STATION FEEDTHRU & DETAIL G, HARNESS TIE DOWN DETAIL

7

VIEW D-D, COAX ROUTING UNDER FLOOR8

DETAIL J - GIA63W TERMINATIONS & DETAIL K - GDL69A TERMINATION10

VIEW B-B, BACK OF INSTRUMENT PANEL

11

VIEW C-C - CABIN OVERHEAD

16. INSTALLL CIRCUIT BREAKER (ITEM 28) IN EXISTING TRAFFIC ALERT POSITION AS SHOWN. ROUTE NEW WIRE WITH EXISTING CIRCUIT BREAKER PANEL WIRING.

DETAIL L - P651 TERMINATION & DETAIL M - CIRCUIT BREAKER TERMINATION

14

17. FOR THOSE STANDOFFS LOCATED AT A FRAME STATION, POSITION THE STANDOFF ALONG EDGE OF FEEDTHRU, MAINTAINING MINIMUM 2D FROM EDGE OF FEEDTHRU CUTOUT AND INSTALL GROMMET (ITEM 15) AROUND FEEDTHRU.

18. COIL EXCESS COAX IN BAY AS SHOWN. DO NOT ADJUST THE LENGTH OF THE COAXIAL CABLE ASSEMBLIES IN ANY WAY.

9

2 ADDED NOTE 19 7/22/10 73725

DWH 6/9/10

DWH 6/9/10

DWH 6/9/10

3 ADDED ALTERNATE PART NUMBERS 8/25/10 74607

Page 2: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

GTS 820 OPTION BILL OF MATERIALS (B.O.M.)

QTY DESIGNATOR PART NUMBER DESCRIPTION VENDOR ITEM

1 320-00609-04 WIRE HARNESS, GTS 820 (LOOSE WIRES) FIELD FABRICATED 1

1 320-00609-01 WIRE HARNESS, GTS 820 FIELD FABRICATED 2

1 320-00609-02 WIRE HARNESS, GTS 820 (GPA 65) FIELD FABRICATED 31 320-00609-03 WIRE HARNESS, GTS 820 (CABIN) FIELD FABRICATED 41 320-00609-05 GTS TO PA COAX ASSYS. FIELD FABRICATED 51 320-00609-06 PA TO TOP ANTENNA COAX ASSYS. FIELD FABRICATED 61 320-00609-07 GTS TO BOTTOM ANTENNA COAX ASSYS. FIELD FABRICATED 7

AR GROMMET M22529/2-4R-25 GROMMET BEST SOURCE 15AR MS3367-1-9 ZIPTIE BEST SOURCE 16AR MS3340-1-9 STANDOFF BEST SOURCE 17AR MS35206-231 SCREW, #6 BEST SOURCE 18AR NAS1149FN632P WASHER BEST SOURCE 19AR MS21044N06 NUT, #6 BEST SOURCE 201 P651 330-00437-01 CONNECTOR GARMIN 21

AR M39029/5-115 CONTACT BEST SOURCE 228 336-00021-00 CONTACT GARMIN 23

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

2 11

3

NTS

11

12

1 770421-1 CONNECTOR HAWKER BEECHCRAFT 241 350550-1 CONTACT HAWKER BEECHCRAFT 251 MS25036-108 TERMINAL LUG BEST SOURCE 26

1MS3320-5 or

7277-2-5CIRCUIT BREAKER, 5 AMP BEST SOURCE 28

P191

2 TM2S6 TIE DOWN HAWKER BEECHCRAFT 29

AR SWTF12X orHT1/4T SPIRAL WRAP HAWKER BEECHCRAFT 30

8

8

8

AR MS35206-229 SCREW, #6 BEST SOURCE 31

ARMS25036-149 or

115110-D8RING TERMINAL, #8 18-22 AWG BEST SOURCE or

HAWKER BEECHCRAFT11

AR SHIELDSAA59569F36T0062 orS03-0X-R-9035-100

FLAT BRAID, 1/16 INCH BEST SOURCE orHAWKER BEECHCRAFT

12

ARAA59163-1II0020 or

S2672TAPE, SILICONE FUSION BEST SOURCE or

HAWKER BEECHCRAFT13

AR MIL-T-43435B TAPE, LACING/TYING, NYLON BEST SOURCE 14

ARAS83519/1-X or

M83519/1-X SOLDER SLEEVE BEST SOURCE 8

ARM23053/5-10X-Y or

RNF-100-3/8 HEATSHRINKBEST SOURCE or

HAWKER BEECHCRAFT9

2M81824/1-X or

D-436-009XSPLICE, ENVIRONMENTAL BEST SOURCE or

HAWKER BEECHCRAFT10

ARM22759/16-16-9 or

131681AA16-916 GA STRANDED

BEST SOURCE orHAWKER BEECHCRAFT

27

B.O.M.

19. THE FOLLOWING PARTS ARE CONSIDERED INTERCHANGABLE AS SPECIFIED BELOW:

P/N: 320-00587-07 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-09P/N: 320-00587-08 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-10P/N: 320-00587-09 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-11P/N: 320-00587-10 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-12P/N: 320-00587-11 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-13P/N: 320-00587-12 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-14P/N: 320-00587-13 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-15P/N: 320-00587-14 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-16P/N: 320-00587-15 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-17P/N: 320-00587-16 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-18P/N: 320-00587-17 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-19P/N: 320-00587-18 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-20P/N: 320-00587-00 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-04P/N: 320-00587-01 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-01P/N: 320-00587-02 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-02P/N: 320-00587-03 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-03P/N: 320-00587-04 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-05P/N: 320-00587-05 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-06P/N: 320-00587-06 IS AN ACCEPTABLE ALTERNATIVE TO P/N: 320-00609-07

NOTES (CONT'D.)

19

19

19

19

AR MS35206-242 SCREW BEST SOURCE 32AR MS35338-42 WASHER, SPLIT 33AR NAS1149FN832P WASHER, FLAT 34

BEST SOURCEBEST SOURCE

AR MS25036-153 TERMINAL LUG BEST SOURCE 35

AR MS25036-102 TERMINAL LUG BEST SOURCE 36AR MS25036-107 TERMINAL LUG BEST SOURCE 3720

20 IF MIL-SPEC PART NUMBER MS3320-5 CIRCUIT BREAKER IS UTILIZED, USE ITEM 26.IF PART NUMBER 7277-2-5 CIRCUIT BREAKER IS UTILIZED, USE ITEM 37.

Page 3: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

3 11

3

NTS

WIRE ROUTING OVERVIEW (VIEW LOOKING DOWN)

GTS 820(REF.)

320-00609-03HARNESS

5

AA

B

B

GPA 65(REF.)

320-00609-02HARNESS

320-00609-07COAX ASSYS.

320-00609-06COAX ASSYS.

320-00609-05COAX ASSYS.

6

GA 58(REF.)

GA 58(REF.)

19

19

1919

19

Page 4: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

INSTRUMENT PANEL(EXIST.)

WL100.00

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

4 11

3

NTS

WIRE ROUTING OVERVIEW (VIEW LOOKING RIGHT)

FS190.00

FS131.00

FS83.00

FS39.00

FS155.00

FS124.75

BOTTOM GA58 (REF.)

UPPER GA58 (REF.)

CC

DD

320-00609-03HARNESS

5

320-00609-07COAX ASSYS.

320-00609-03HARNESS

320-00609-02HARNESS

320-00609-05 COAX ASSYS. & 320-00609-02 HARNESS

320-00609-06COAX ASSYS.

5

6

320-00609-01HARNESS

GPA 65(REF.)

GTS 820 (REF.)

19

19

19

19

19

19

19

Page 5: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

5 11

3

NTS

VIEW A-A - AFT CABIN LOOKING RIGHT

SEE DETAIL F SH. 6

FWD

UP

FS179.00

FS190.00

STATIC LINE (EXIST.)

320-00609-05COAX ASSYS.

320-00609-07COAX ASSYS.

GTS 820(REF.)

J8001

J8002

J8003

15

FS170.00

320-00609-02HARNESS

FS207.00

3445J5

3445P63445P12

3445P5

3445J63445J12

320-00609-03HARNESS (SEE SH. 3 FOR CONTINUATION)

5

6

E

ESEE VIEW D-D SH. 8

SEE VIEW C-C SH. 7

TIE DOWN (ITEM 29) 2 PLS. SEE DETAIL G

SECURE HARNESS TO TIE DOWN WITH ZIPTIE

AS SHOWN

GTSJ1 GTSP1

GTSP2GTSJ2

320-00609-02HARNESS

320-00609-01HARNESS

7

19

19

19

19

19

19

Page 6: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

DETAIL F - FRAME STATION FEEDTHRU & DETAIL G - HARNESS TIE DOWN DETAIL

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

6 11

3

NTS

FS190.00

J1

T

B

J3

B

J8001

J8002

J8003

USB CONNECTOR

FS207.00

GTS 820(REF.)

MS21044N06 NUT

NAS1149FN632P WASHER

MS35206-231SCREW

AIRCRAFT STRUCTURE (REF.)

MS3340-1-9 STANDOFF

MS21044N06 NUT

NAS1149FN632P WASHER

MS35206-229SCREW

FRAME STATION (REF.)

TM2S6 STANDOFF

SECURE HARNESS (NOT SHOWN) TO STANDOFF WITH ZIPTIE

SECURE HARNESS (NOT SHOWN) TO STANDOFF WITH ZIPTIE

320-00609-01HARNESS

320-00609-05COAX ASSYS.

320-00609-07COAX ASSYS.

TIE DOWN HARNESSTO SHELF AS SHOWN(SEE DETAIL F)

15

3445J5

3445P6

3445P12

GTSP1

GTSJ2

USE EXISTING HOLE

VIEW E-E - 320-00609-01 HARNESS

3.25

17

DRILL Ø.156 HOLE, MAINTAINING 2 E.D. MINIMUM

19

19

19

4.325

Page 7: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

7 11

3

NTS

VIEW C-C- CABIN OVERHEAD

FS155.00

FS170.00

FS179.00

B.L.0.00

FS140.00

FS124.75

FS106.25

STR.(REF.)

STR.(REF.)

GPA 65(REF.)

GA 58 UPPER ANT. (REF.)

SEE DETAIL F SH. 5 (5 PLS.)

ROUTE COAXES OVERF.S. 124.75 AS SHOWN AND

PROTECT WITH ITEM 30

320-00609-02HARNESS

320-00609-05COAX ASSYS.

320-00609-06COAX ASSYS.

SEE DETAIL L(SHEET 11)

FWD

ACFT. LEFT

15

15

15

HARNESS IS PARTOF GPA 65 ASSYS.

19

1919

Page 8: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

8 11

3

NTS

FWD

ACFT. RIGHT

VIEW D-D - COAX ROUTING UNDER FLOOR

5

FS179.00

FS190.00

FS190.00

B.L.0.00

FS170.00

FS151.00

FS131.00

STR.(REF.)

STR.(REF.)

320-00609-07COAX ASSYS.

EXISTINGWIRING

ROUTE COAXALONG WITH EXISTINGWIRE AND SECUREAS SHOWN

EXIST. WIRING

5

SEE VIEW A-A SH. 5

GA 58 LOWER ANT. (REF.)

15

18

19

Page 9: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

9 11

3

NTS

VIEW B-B - BACK OF INSTRUMENT PANEL

EXISTING WIREHARNESS (REF.)

SEE DETAIL J(SHEET 10)

5

P191

DATALINK

AP SERVOS

STORMSCOPE

DME AVIONICSFAN

TRAFFIC ALERT

SEE DETAIL M, SH. 11

3310J7(EXIST.)

3445-021-16

16

SEE SH. 3FOR CONT.

19

19

Page 10: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

.35" MAX WINDOW SIZE

.75 " MIN LENGTH (2 PLS.)ITEM 9

SOLDER SLEEVEITEM 8

12

11

SIGNAL WIRE SPLICEITEM 10

TERMINALITEM 11

TAPEITEM 13

CONNECTORS 2321P4 AND 2322P4, AND ASSOCIATED HARDWARE SHOWN IS EXISTING, SHOWN FOR REF. ONLY

HEATSHRINK TUBING,

320-00609-03HARNESS (REF.)

CONNECTOR 2320P1 AND ASSOCIATEDHARDWARE SHOWN IS EXISTING, SHOWN FOR REF. ONLY

END OF SHIELD BLOCK

SHRINKABLE0.75" M

IN

TUBINGWINDOW SIZE0.35" M

AXBEGINNING OF SHIELD

BACKSHELL COVER

EDGE OF

1.5" MAX.

OUTER SOLDER SLEEVE EDGE

4" MAX.

HEATSHRINKITEM 9 12

11

BRAIDITEM 12

SOLDER SLEEVEITEM 8

TERMINALITEM 11

TAPEITEM 13

CONTACT P/N: 336-00021-00

SEE DWG. 320-00609-XXCONTACT P/N:

336-00021-00

31303332

38

7

38

7

G34102B24

G34103B22

G34104B22

G34103C22

G34104C22

(SG)

SEE DWG. 320-00609-XX

SEE DWG. 320-00609-XX

CONTACT P/N: 336-00021-00

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

10 11

3

NTS

& DETAIL K - GDL 69A TERMINATION

BRAIDITEM 12

PART OF 320-00609-04HARNESS

DETAIL J - GIA 63W TERMINATIONS

14

14

12

12

19

WASHERITEM 34

WASHERITEM 33

SCREWITEM 32

WASHERITEM 34

WASHERITEM 33

SCREWITEM 32

Page 11: NOTES REV DESCRIPTION DATE ECOstatic.garmin.com/pumac/G1000:BeechcraftBonanzaA36_G36...AR MS25036-102 TERMINAL LUG BEST SOURCE 36 20 AR MS25036-107 TERMINAL LUG BEST SOURCE 37 20 IF

.35" MAX WINDOW SIZE

11

12

TAPEITEM 13

HEATSHRINKITEM 9

TERMINAL ITEM 11

G34108B22

G34110B22

G34111B22

G34112B22

G34109B22

P651

(SG)

(SG)

(SG)

(SG)

(SG)

JH

GF

MBA

PLK

ESC

SEE DWG. 320-00609-XX

CONNECTOR P/N: 330-00437-01CONTACT P/N: M39029/5-115

SEE DWG. 320-00609-XX

SIZE

SCALE

DWG. NO. REV.

SHT. OF

005-00620-09

11 11

3

NTS

& DETAIL M - CIRCUIT BREAKER TERMINATION

BRAID ITEM 12

SOLDER SLEEVE ITEM 8

CONTACTP/N: 350550-1

CONNECTOR P/N: 770421-1

CRIMP SOCKETONTO WIRE

CIRCUIT BREAKER ITEM 28

10" OF 16 GA. WIRE

ITEM 37

SECURE TO C.B. USINGSUPPLIED HARDWARE

P191 3310J7

TRAFFIC

BUSAVIONICS

28VDC

5

ALERT

(16) 3445-021-16CB 73

1

DETAIL L - P561 TERMINATION

12