1. G500H SYSTEM ARRANGEMENT SHOWN IS APPLICABLE TO BELL 206L, 206L-1, 206L-3, AND 206L-4 MODEL ROTORCRAFT.2. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

WL59.5

FS21

9.6

WL70.1

FS24

3.0

FS32

.8

WL37.6

WL21.7

FS38

.6

WL43.3

FS60

.4

FS17

2.8

WL54.7

FS0.

0

WL0.0

FS1.

0

FS62

.0

FS83

.0

21.0

GDU 620 DISPLAY[SHEET 3]

GDC 74H AIR DATA COMPUTER[SHEET 4]

GRS 77H AHRS SECONDARY LOCATION[SHEET 5]

GTP 59 OAT PROBE[SHEET 7]

GRS 77H AHRSPRIMARY LOCATION [SHEET 5]

GMU 44 MAGNETOMETERPRIMARY LOCATION [SHEET 6]

GMU 44 MAGNETOMETERSECONDARY LOCATION [SHEET 6]

FIGURE 3 (C4 SHEET 1)

G500H SYSTEM OVERVIEW - SIDE VIEWSCALE 1:40

FIGURE 1 (D4 SHEET 1)

G500H SYSTEM OVERVIEW - TOP VIEWSCALE 1:40

BL10.3LH

BL2.5LH

BL0.0

BL18.6LH

BL6.3RH

WIRE HARNESS[SHEET 8]

FIGURE 2 (B7 SHEET 1)

G500H SYSTEM OVERVIEW - FRONT VIEWSCALE 1:40

WL21.7

WL37.6

WL43.3

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

DATE ECO NO.DESCRIPTIONREVZONE

REVISIONS

A

B

C

D

8 7 6 5 4 3 2 1

CONFIDENTIALThis drawing and the specifications contained herein are the property of Garmin Ltd. or its subsidiaries and may not be reproduced or used in whole or in part as the basis for manufacture or sale of products

without written permission.

TOLERANCE(UNLESS NOTED OTHERWISE)

.X ± .100

.XX ± .010

.XXX ± .005HOLES ± .003

.X ± .25

.XX ± .13HOLES ± .08

ANGLES ± 0.5°

DRAWN

CHECKED

PROJ. MGR.

RELEASED BY

TITLE

SIZE

SCALE

DWG. NO.

PART NO.

REV.

8 7 6 5 4 3 2 1

A

B

C

D

ADB

02/28/2010MKD

02/23/2010SGSBELL 206L ROTORCRAFT

1:40

02/23/2010

190-01150-421 8

2

RK

DER REVIEW REQUIRED

02/23/2010

-----INITIAL RELEASE 02/23/201070689CHANGED GMU 44 SECONDARY LOCATION 03/31/2010

12

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

NONE

190-01150-422 8

2

ITEMPART NUMBER WEIGHT (LB)

ARM (IN) [2] MOMENT ARM (IN-LB) [2]011-01264-50 [5] 6.38 246.3GDU 620 (Unit Only)

1

GDC 74H (Unit Only)

38.6ARM (IN) [2] MOMENT ARM (IN-LB) [2]

40.26.3

LONGITUDINAL [3] LATERAL [4]

Table 1: Weight and Balance Bell 206L [1][2]

[1] A ROTORCRAFT WEIGHT AND BALANCE IS REQUIRED AFTER INSTALLATION OF THE G500H SYSTEM. REFER TO STC INSTALLATION MANUAL P/N 190-01150-06 FOR ADDITIONAL INFORMATION, INCLUDING OVERALL SIZE AND CENTER OF GRAVITY LOCATION OF ALL LRUs.

[2] ARM AND MOMENT VALUES LISTED IN THIS TABLE ARE FOR REFERENCE ONLY. THE ARM AND MOMENTS MUST BE VERIFIED FOR EVERY INSTALLATION.

[3] THE LONGITUDINAL ARM IS MEASURED IN TERMS OF THE FUSELAGE STATION (FS) NUMBER.[4] THE LATERAL ARM IS MEASURED IN TERMS OF THE BUTT LINE (BL). THE CENTERLINE OF THE HELICOPTER IS BL0.00. THE MOMENT ARMS TO

THE LEFT SIDE (LOOKING FORWARD) ARE NEGATIVE (-) AND THE MOMENT ARMS TO THE RIGHT SIDE ARE POSITIVE (+).[5] EITHER 011-01264-50 OR 011-01264-60 UNITS ARE ACCEPTABLE.[6] GRS 77H UNIT MAYBE INSTALLED UNDER EITHER PILOT OR CO-PILOT SEAT. CO-PILOT SEAT MOMENT ARM SHOWN.

011-00882-11 1.702

55.832.8 0.00.0

GRS 77H (Unit Only) [Primary Location] 011-00868-20

3

172.8 -28.8-10.3

011-01264-50 [5] 7.04 271.7GDU 620 (Installed with rack and connector) 38.6 44.46.3

GDC 74H (Installed with connector) 011-00882-11 1.92 63.032.8 0.00.02.80 483.8

GRS 77H (Installed with rack and connector) [Primary Location] 011-00868-20 172.8 -35.6-10.33.46 597.9

GMU 44 (Unit Only) [Primary Location] 011-00870-10

4

219.60.35 76.9GMU 44 (Installed with rack and connector) [Primary Location] 011-00870-10 219.60.50 109.8

0.00.00.00.0

GMU 44 (Unit Only) [Secondary Location] 011-00870-10 243.00.35 85.1GMU 44 (Installed with rack and connector) [Secondary Location] 011-00870-10 243.00.50 121.5

-0.9-2.5-1.3-2.5

GRS 77H (Unit Only) [Secondary Location] 011-00868-20 60.4 -52.1-18.6 [6]2.80 169.1GRS 77H (Installed with rack and connector) [Secondary Location] 011-00868-20 60.4 -64.4-18.6 [6]3.46 209.0

011-00978-00 -5 -- --GTP 59 (Installed with connector)

109

45678

301302

33002

100 FEET

180200

160

140120 100

4020

AIRSPEED

KNOTS 80

6010

2010

20

20

2010

10

63

N33

30

W 2421

S15

12

E

TURBINE

percent

010

20

30

40

5060 70

80

90

100

110120

HOOK LOADd.c. voltage

davtron

510 15

20

0

510 15

20

VERTICALSPEED

PER MIN100 FEET

UP

DN

5040

3020

10

0 100

9080

70

60

torque

percent

temp

13

5 6

7

89

turbout

gasproducer

010

20

30

40

5060

70

809090

chronometer

davtron

ENGOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

xmsnOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

fuel

qty

e

25 50

75

gals

load fuel

0

5

10

0

12

X10

P dc psi p

3

hobbsquartz

flight hours

min2

d.c.elec.

L R

BARO

V/S

ALT

CRS

HDG

ENT

CLR

MENU

DFLT

RNG

109

45678

301302

33002

100 FEET

180200

160

140120 100

4020

AIRSPEED

KNOTS 80

60

0

10

20

30

40

50607080

90

100

110

120

1

2

3

4

5

%RPMROTORRPM 100

R

HOOK LOADX 10

SetupUN-ZERO ZERO

load fuel

0

5

10

0

12

X10

P dc psi p

3D.C. VOLTAGE

DAVTRONM450

gasproducer

010

20

30

40

5060

70

809090

fuel

qty

e

25 50

75

gals

temp

13

5 6

7

89

turbout

ENGOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

xmsnOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

5040

3020

10

0 100

9080

70

60

torque

percent

chronometer

davtron

hobbsquartz

flight hours

D.C. VOLTAGE

DAVTRONM450

chronometer

davtron

109

45678

301302

33002

100 FEET

180200

160

140120 100

4020

AIRSPEED

KNOTS 80

6010

2010

20

20

2010

10

63

N33

30

W 2421

S15

12

E

TURBINE

percent

010

20

30

40

5060 70

80

90

100

110120

510 15

20

0

510 15

20

VERTICALSPEED

PER MIN100 FEET

UP

DN

5040

3020

10

0 100

9080

70

60

torque

percent

temp

13

5 6

7

89

turbout

gasproducer

010

20

30

40

5060

70

809090

chronometer

davtron

ENGOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

xmsnOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

fuel

qty

e

25 50

75

gals

load fuel

0

5

10

0

12

X10

P dc psi p

3

min2

d.c.elec.

L R

10

2010

20

20

2010

10

63

N33

30

W 2421

S15

12

E

109

45678

301302

33002

100 FEET

180200

160

140120 100

4020

AIRSPEED

KNOTS 80

60

63

N33

30

W 2421

S15

12

E

TURBINE

percent

010

20

30

40

5060 70

80

90

100

110120

5040

3020

10

0 100

9080

7060

torque

percent

temp

13

5 6

7

89

turbout

gasproducer

010

20

30

40

5060

70

809090

chronometer

davtron

ENGOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

xmsnOIL

0

5

10

15

0

5

10

15

X10

P PSI C T

fuel

qty

e

25 50

75

gals

load fuel

0

5

10

0

12

X10

P dc psi p

3

CDI OBS MSG FPL PROCVNAV

C

V

C

D

MENU

CLR

ENT

NAVDEFAULT

RNG

V

PUSHC/V

PUSHCRSR

VLOCCOM

VOLID

PUSH

SQPUSHVOL

PWR

GNS 530

CDI OBS MSG FPL PROCVNAV

C

V

C

D

MENU

CLR

ENT

NAVDEFAULT

RNG

V

PUSHC/V

PUSHCRSR

VLOCCOM

VOLID

PUSH

SQPUSHVOL

PWR

GNS 530

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

1:40

190-01150-423 8

2

FS0.

0

FS38

.6

WL0.0

WL43.3

FIGURE 4 [D6 SHEET 3]

GDU 620 LOCATION - SIDE VIEWSCALE 1:40

FIGURE 5 [D2 SHEET 3]

EXAMPLE - WIDE INSTRUMENT PANEL LAYOUT

SCALE 1:8ORIGINAL CONFIGURATION AND GDU 620 INSTALLED

FIGURE 6 [B2 SHEET 3]

EXAMPLE - INSTRUMENT PANEL LAYOUT

SCALE 1:8ORIGINAL CONFIGURATION AND GDU 620 INSTALLED

GDU 620 UNIT

SYS - AIRFRAME CONFIG (AIRSPEEDS):VS0 0

Table 2: System Configuration Settings

VS1 0VFE 0VNO 130

GLIDE 0

GDC - FILTERING TIME CONSTANTSGDU AIRSPEED

0.9000.600LOW

HIGH

GDU AIRSPEED TRANS TO

25 KTS20 KTSLOW

HIGH

GDU VERTICAL SPEED 1.35

VR 0VX 0VY 57VLE OFFVMCA OFFVYSE 100

VNE 130

1. LOCATE GDU 620 UNIT ON THE INSTRUMENT PANEL. REFER TO STC INSTALLATION MANUAL, P/N 190-01150-06 FOR UNIT MOUNTING CONSIDERATIONS, AND TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206L ROTORCRAFT DRAWING FOR DETAILS.

2. GDU 620 WEIGHT AND BALANCE VALUES LISTED IN TABLE 1 MUST BE ADJUSTED FOR ANY WEIGHT AND LOCATION CHANGES.3. GDU 620 UNIT MUST BE ELECTRICALLY BONDED TO ROTORCRAFT METALLIC STRUCTURE. REFER TO 190-01150-43 INSTALLATION, G500H

SYSTEM, BELL 206L ROTORCRAFT DRAWING FOR DETAILS.4. UPON COMPLETION OF THE G500H SYSTEM INSTALLATION, GDU 620 HAS TO BE CONFIGURED USING SYSTEM CONFIGURATION SETTINGS

DEFINED IN TABLE 2.5. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

A

DETAIL A [B4 SHEET 3]

GDU 620 LOCATION DETAILSCALE 1:10

VNE (Power Off) 0

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

1:40

190-01150-424 8

2

FS0.

0

FS32

.8

WL0.0

WL37.6

B

1. LOCATE GDC 74H UNIT ON TOP OF SUPPORTING STRUCTURE FORWARD OF THE INSTRUMENT PANEL. REFER TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206L ROTORCRAFT DRAWING FOR DETAILS.

2. GDC 74H UNIT MUST BE ELECTRICALLY BONDED TO ROTORCRAFT METALLIC STRUCTURE.3. GDC 74H UNIT LOCATION REQUIRES FABRICATION OF A SUPPORT BRACKET. 4. GDC 74H WEIGHT AND BALANCE VALUES LISTED IN TABLE 1 MUST BE ADJUSTED FOR ANY WEIGHT AND LOCATION CHANGES.5. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

GDC 74H UNIT

REF. ENGINE INSTRUMENTSHYDRAULIC FITTINGS

REF. INSTRUMENT PANEL SUPPORTSTRUCTURE/CENTER CONSOLE

FIGURE 7 [D6 SHEET 4]

GDC 74H LOCATION - SIDE VIEWSCALE 1:40

DETAIL B [B4 SHEET 4]

GDC 74H LOCATIONSCALE 1:10

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

1:40

190-01150-425 8

2

1. GRS 77H UNIT MUST BE ELECTRICALLY BONDED TO ROTORCRAFT METALLIC STRUCTURE.2. GRS 77H UNIT MUST BE MOUNTED RIGIDLY TO THE ROTORCRAFT PRIMARY STRUCTURE. REFER TO STC INSTALLATION MANUAL, P/N 190-01150-06 FOR UNIT

MOUNTING CONSIDERATIONS.3. PRIMARY GRS 77H UNIT LOCATION REQUIRES FABRICATION OF A SUPPORTING STRUCTURE. REFER TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206L

ROTORCRAFT DRAWING FOR DETAILS.4. SECONDARY GRS 77H UNIT LOCATION MAY REQUIRE FABRICATION OF AN ADAPTER BRACKET AND/OR INSTALLATION OF POTTED INSERTS PER BELL STRUCTURAL

REPAIR MANUAL BHT-206-SRM-1.5. GRS 77H WEIGHT AND BALANCE VALUES LISTED IN TABLE 1 MUST BE ADJUSTED FOR ANY WEIGHT AND LOCATION CHANGES.6. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

FIGURE 8 [D5 SHEET 5]

GRS 77H LOCATION - SIDE VIEWSCALE 1:40

FS0.

0

FS60

.4

FS17

2.6

WL0.0

WL21.7

WL54.7

C

D

DETAIL C [B7 SHEET 5]

GRS 77H SECONDARY LOCATIONSCALE 1:12

DETAIL D [B2 SHEET 5]

GRS 77H PRIMARY LOCATIONSCALE 1:12

REF. FABRICATED BRACKET SUPPORTSTRUCTURE [MAY INCLUDE 115-00922-00 TOP BRACKETAND 115-00909-00 ANGLE BRACKET (2X), PARTS OF GRS 77H UNIVERSAL MOUNT,GARMIN P/N 011-01780-00]

FUSELAGE FRAMEFS167.33 REF.

FUSELAGE FRAMEFS179.66 REF.

GRS 77H UNIT

REF. CO-PILOT SEATSUPPORT STRUCTURE

GRS 77H UNIT

GRS 77H AHRSSECONDARY LOCATION

GRS 77H AHRSPRIMARY LOCATION

1. LOCATE GMU 44 UNIT CHOOSING PRIMARY OR SECONDARY LOCATION. REFER TO STC INSTALLATION MANUAL, P/N 190-01150-06 FOR UNIT MOUNTING CONSIDERATIONS. REFER TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206L ROTORCRAFT DRAWING FOR DETAILS.

2. GMU 44 UNIT MUST BE ELECTRICALLY BONDED TO ROTORCRAFT METALLIC STRUCTURE.3. PRIMARY GMU 44 UNIT LOCATION REQUIRES FABRICATION OF A SUPPORT BRACKET FOR ATTACHING GMU 44 UNIVERSAL MOUNT, GARMIN

P/N 011-01779-01.4. SECONDARY GMU 44 UNIT LOCATION REQUIRES FABRICATION OF A MOUNTING BRACKET. 5. GMU 44 WEIGHT AND BALANCE VALUES LISTED IN TABLE 1 MUST BE ADJUSTED FOR ANY WEIGHT AND LOCATION CHANGES.6. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

1:40

190-01150-426 8

2

TAILBOOM FRAMEBS42.59 REF.

REF. GMU 44 MOUNTING BRACKET[FABRICATED]

REF. GMU 44 UNIT

FRAME FS 217.84 REF.

REF. GMU 44 UNIT

REF. GMU 44 MOUNTING PLATE[FABRICATED]

REF. GMU 44 UNIVERSAL MOUNTGARMIN P/N 011-01779-01

FS0.

0

FS21

9.6

FS24

3.0

WL0.0

WL20.6

WL59.5

WL70.1

GMU 44 MAGNETOMETERPRIMARY LOCATION

GMU 44 MAGNETOMETERSECONDARY LOCATION

FIGURE 9 [D5 SHEET 6]

GMU 44 INSTALLATION LOCATION

SCALE 1:40SIDE VIEW

EF

DETAIL E [B7 SHEET 6]

GMU 44 PRIMARY LOCATIONSCALE 1:10

DETAIL F [B3 SHEET 6]

GMU 44 SECONDARY LOCATIONSCALE 1:10

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

1:40

190-01150-427 8

2

FS0.

0

FS62

.0

FS83

.0

FS1.

0

WL0.021.0

G H

1. LOCATE GTP 59 OUTSIDE TEMPERATURE PROBE ON THE BOTTOM OF A ROTORCRAFT FUSELAGE. PROBE LOCATION MAY VARY WITHIN INDICATED AREA. GTP 59 SHOULD BE KEPT AWAY FROM HEAT SOURCES. REFER TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206 L ROTORCRAFT DRAWING FOR DETAILS.

2. GTP 59 TEMPERATURE PROBE MUST BE ELECTRICALLY BONDED. 3. GTP 59 TEMPERATURE PROBE LOCATION MAY REQUIRE FABRICATION OF A DOUBLER.4. DIMENSIONS ARE IN INCHES UNLESS OTHERWISE NOTED.

1 FIGURE 10 [D6 SHEET 7]

GTP 59 OAT PROBE LOCATION - SIDE VIEWSCALE 1:40

DETAIL G [B6 SHEET 7]

GTP 59 OAT PROBE - NEW INSTALLATIONSCALE 1:1

DETAIL H [B3 SHEET 7]

GTP 59 OAT PROBE - INSTALLATION IN COVER PLATESCALE 1:1

FS69.8 REF.

OAT PROBE SUPPORTDOUBLER

GTP 59 OAT PROBE

FS81.5 REF.

EXISTING ANTENNACOVER PLATE REF.

GTP 59 OAT PROBE

FIGURE 12 (B4 SHEET 8]

WIRE HARNESS ROUTING - SIDE VIEWSCALE: NONE

FIGURE 11 (B4 SHEET 8]

WIRE HARNESS ROUTING - TOP VIEWSCALE: NONE

NOTES:1. REFER TO 190-01150-43 INSTALLATION, G500H SYSTEM, BELL 206 L ROTORCRAFT DRAWING FOR DETAILS OF WIRE

HARNESS FABRICATION, ROUTING, AND INSTALLATION.

GTP 59 OAT PROBE TYP.GRS 77H AHRSSECONDARY LOCATION

GDU 620 DISPLAY

GDC 74H AIRDATA COMPUTER

GRS 77H AHRSPRIMARY LOCATIONREF: 005-W0222-00, P771

GMU 44 MAGNETOMETERPRIMARY LOCATION

GMU 44MAGNETOMETERSECONDARYLOCATION

OVERHEAD CB PANEL

GDC 74H AIR DATA COMPUTERREF: 005-W0222-00, P741

GMU 44 MAGNETOMETERSECONDARY LOCATIONREF: 005-W0222-00, P441

GDU 620 DISPLAYREF: 005-W0222-00,P6201, P6202, P6203

GRS 77H AHRS PRIMARY LOCATIONREF: 005-W0222-00, P771

GRS 77H AHRSSECONDARY LOCATIONREF: 005-W0222-00, P771

GTP 59 OAT PROBE TYP.REF: 005-W0222-00

GMU 44 MAGNETOMETERPRIMARY LOCATIONREF: 005-W0222-00, P441

GTP 59 OAT PROBEDISCONNECT JG01/PG01

(OPTIONAL)

FS 1

79.7

FS 1

67.3

FS 2

41.9

FS 0

.0

WL 0.0

FS 1

92.0

FS 2

04.9

FS 2

17.8 IND

FUEL

RIGHT

QTY

VALVE TEMP

ENG GOV

OVSP CONT IGNTR

ENGINE

START

PITOT DEFOG

& ATT HEAT BLOWER

OFF

BAT

O

GEN

HEAT

OFF

COLL LT

OFF

POS LT

OFF

ANTIOFF BRT

INST LT

FF

IND

GEN

FIELD

GEN

RESET

IND

ENG PAR

SEP PRG

AUX

RECP

PASS

MIKEHAND

CONTCUTPOWER

CARGOCABIN LT

ENC

TURN

ADCAHRS

SYSTEM

LDG INST COCKPITCAUTION

TOT

IND

BOOST

LEFT

XMSN

TEMP

ANTI-ICING

DIR GYRO PITOT DEFOG

& ATT HEAT BLOWER

OFF

BAT

O

GEN

VENT

HEATCOLL LT

OFF

POS LT

OFF

ANTIOFF BRT

INST LT

FF

IND

START

GEN

FIELD

GEN

RESET

INDPRESS

ENG

HOOK

HANDHOISTCABLEHOIST

INDCUTPOWER

HTR

OFF

AHRSPFD NAV COM

LIGHTS

HYDR

XPNDR AUDIO

ALT

R

OFSHT.

B

Garmin Ltd. or its subsidiariesc/o Garmin International, Inc.

1200 E. 151st StreetOlathe, Kansas 66062 U.S.A.

SIZE

SCALE

DWG. NO.

PART NO.

REV.

A

B

C

D

8 7 6 5 4 3 2 1

8 7 6 5 4 3 2 1

A

B

C

D

NONE

190-01150-428 8

2