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VAN'S AIRCRAFT, INC.

PAGE:

REVISION:

DATE:

01/19/19

0

RV-12iS

42PiS-04

F-00206

AV-532L

ANTENNA

2X AN3-13A

MATCH DRILL #30

ES-00301
LP4-5
NAS1149FN432P

Step 1: Position the ES-00301 on the aft-most lightening hole as shown in Figure 1, then match-drill #30 the rivet hole into the

VS-1205.

Step 2: Rivet the ES-00301 to the VS-1205 with the hardware shown in Figure 1. A small dab of superglue can be used to hold the

washer to the bottom of the VS-1205 if necessary.

Step 3: Rivet the F-00205 Shim and the nutplate onto the VS-1205 as shown in Figure 1.

Step 4: Temporarily secure the F-00206 and AV-532L Antenna on to the VS-1205 with the fasteners shown in Figure 1.

Step 5: Mark the longitudinal position of the AV-532L Antenna elements on the VS-1201 as
shown in Figure 1.

Step 6: Measure the vertical height of the AV-532L Antenna element
above the top edge of the VS-1201 as shown in Figure 1 and record
the value.

Remove the AV-532L from the V-Stab Assembly.

Step 7: Temporarily install the VS-1213 onto the V-Stab

Assembly with #6 screws as shown in Figure 1.

Step 8: Transfer the positioning marks made in Step 5 from
the VS-1201 to the VS-1213.

Measure and mark the height of the AV-532L Antenna

element onto the VS-1213.

NOTE: The notch cut in Step 9 should be smoothly
radiused at the top (approx 1/8 in. [1.6 mm] radius).

Step 9: Remove the VS-1213 from the V-Stab

Assembly and cut a notch in the VS-1213 from the
antenna element positioning marks, down to the

lower edge of the VS-1213.

Ensure adequate clearance around the antenna

elements to allow for vibration of the elements
as shown in the Detail View in Figure 1.

F-00205 SHIM

2X CCR264SS-3-2

K1000-3

VS-1213

VS-1201

VS-1213

VS-1201

AV-532L

NOTCH FOR 1/32-1/16 [.8-1.6 mm]
CLEARANCE ALL SIDES

FIGURE 1: NOTCHING THE FAIRING

VS-1205

Summary of Contents for G3X

Page 1: ...NCE SYSTEM GMA 245 GARMIN AUDIO PANEL GTN 650 GARMIN GPS NAV COM GEA 24 GARMIN ENGINE INDICATION SYSTEM GA 36 OR GA 37 GARMIN GPS ANTENNA F 00214 GARMIN AFT PITOT LINE F 00212 GARMIN AOA LINE F 00216...

Page 2: ...de all 40 holes just match drilled into the VS 1213 for an AN426AD3 rivet See Figure 2 Step 5 Final drill 27 then machine countersink all 30 holes in the VS 1213 See Figure 2 Step 6 Rivet the nutplate...

Page 3: ...own in Figure 2 Step 7 Rivet the nutplates to the bottom of the F 00203 as shown in Figure 2 Step 8 Using the marks made in Step 3 as a starting point trim away the inside edge of the lightening hole...

Page 4: ...tical height of the AV 532L Antenna element above the top edge of the VS 1201 as shown in Figure 1 and record the value Remove the AV 532L from the V Stab Assembly Step 7 Temporarily install the VS 12...

Page 5: ...the F 00204 through the aft most set of lightening holes in the ribs of the V Stab Assembly See Figure 2 Step 4 Secure the F 00204 to the ES 00301 on the top of the V Stab Assembly The F 00204 should...

Page 6: ...Step 2 Use a step drill to enlarge the 30 hole in the F 1278 to 5 8 Step 3 Install the snap bushing into the F 1278 as shown in Figure 1 Step 4 Cut strips of MS21266 Grommet to the length shown in Fig...

Page 7: ...dge of of the F 1279 R Upper Right Skin stiffener and is clear of all control cables Step 2 Route the AV 532L cable through the snap bushing in the F 1278 Step 3 With the AV 532L cable extending outsi...

Page 8: ...01207C L route the AV 532L cable forward through the airframe and up through the wire pass through hole in the F 01202B 1 as shown in Figure 1 Step 3 Install the F 1257Bs onto the F 1281 R stiffener...

Page 9: ...be used to pull the AV 532L cable up through the F 00204 if necessary Step 2 Connect the ring terminals on the end of the AV 532L cable onto the studs of the AV 532L antenna with the included fastene...

Page 10: ...tailcone skins as shown in Figure 2 Ensure the GMU 11 connector is facing aft Step 3 Connect the 9 pin d sub connector labeled MAGNETOMETER from the WH 00136 to the GMU 11 F 000142 FIGURE 1 GMU 11 IN...

Page 11: ...n Figure 1 This will form the ADAHRS Baggage Floor Assembly FIGURE 1 ADAHRS BAGGAGE FLOOR ASSEMBLY FIGURE 2 INSTALLING THE ADAHRS Step 4 Bolt the GSU 25 to the ADAHRS Baggage Floor Assembly as shown i...

Page 12: ...bricate the F 00214 Garmin Aft Pitot line Step 8 Route one end of the F 00214 through the lightening hole in the F 01207B 1 as shown in Figure 2 then insert the end of the F 00214 into the FLF 00007 i...

Page 13: ...ong its length and does not interfere or chafe against fuel lines brake lines engine and fuel control cables etc The F 00214 will be connected to the FF 1216 Pitot Line later in this section Step 3 Lo...

Page 14: ...ole noted in Figure 2 into the F 00063 This hole is not used for the G3X Touch installation NOTE The two upper screw holes in the F 00063 will make notches in the F 01202B 1 flange See Figures 2 and 3...

Page 15: ...00063 R MS21051 L06 2X AN426AD3 3 5 MS21051 L06 2X AN426AD3 4 6X K1000 06 2X AN426AD3 4 AN426AD3 3 5 Step 1 Rivet the F 00063 L and nutplates to the forward side of the F 01202B 1 Panel Base flange a...

Page 16: ...rsink the nutplate rivet holes in the F 00054 1 L 1 R then install the nutplates as shown in Figure 3 6X MS21055 L06 2X AN426AD3 3 5 8X K1000 06 2X AN426AD3 3 5 F 00054 1 R F 00054 1 L REMOVE HATCHED...

Page 17: ...ep 4 Cleco the F 00132 R to the F 01201A 1 as shown in Figure 1 Step 5 Match drill 30 the holes in the F 00132 R and the F 00132 L Drill Guide as shown in Figure 1 Step 6 Match drill 11 the holes in t...

Page 18: ...oute the WH 00136 main wire harness branches through the slotted holes in the F 00130 L R Step 6 Split the snap bushings then place the snap bushings over each branch of the WH 00136 Secure the snap b...

Page 19: ...l the P1001 P1003 and P1004 connectors part of the WH 00136 on to the backplate Connect the COM NAV and GPS Coaxial cables part of the WH 00136 to the respective connectors on the backplate Step 2 Ins...

Page 20: ...ion Manual and Figure 1 Step 2 Install the Garmin GMA 245 backplate in the GMA245 mounting rack as shown in the GMA 245 Installation Manual and Figure 1 Step 3 Fasten the GMA 245 mounting rack to the...

Page 21: ...apter Plate onto the F 01201A 1 Firewall Top with the hardware called out in Figure 1 Step 3 Apply a thin coating of fuel tank sealant over the heads of the screws on the forward side of the firewall...

Page 22: ...port labled GPS on the GA 36 Step 4 Secure the GA 26C Garmin GPS Antenna to the F 00196 with the included fasteners as shown in Figure 2 Step 5 XM Only Connect the TNC Connector labeled XM from the WH...

Page 23: ...3 Connect the d sub connector labeled XPNDR and the BNC connector labeled XPNDR from the WH 00136 to the GTX 35R Backplate Assembly as described in the GTX 35R Installation Manual See the detail view...

Page 24: ...5 pin d sub connector labeled BATT from the WH 00136 to the IBBS 12V 3AH See Figure 1 Step 3 Gather the WH 00136 near the inboard aft corner of the ES CPU Fan using the clamp as shown and install the...

Page 25: ...Figure 3 Step 10 Repeat and mirror Steps 1 through 9 with the F 00065S for the right side of the aircraft F 1202D L MS21051 L06 3X MATCH DRILL 40 CENTER NUTPLATES ON FLANGE 4X AN426AD3 3 5 LOCATE NUTP...

Page 26: ...ure the switch orientation matches the detail view in Figure 1 Step 3 Purchase then install the internal battery in the E 04 5 Cockpit Remote Refer to the instructions provided with the AV E 04 ACK 40...

Page 27: ...the F 00043S F 00129 and F 00065S with screws Step 2 Locate the co pilot push to talk switch labeled PTT from the WH 00136 Discard the hex nut and star washer included with the switch then attach the...

Page 28: ...6 to the AV 60007 Step 2 Connect the three ES 421 0108 connectors from the WH 00136 to the ES SW K1 AABAAAAA as shown Step 3 Connect the 50 pin d sub connector labeled PFD from the WH 00136 to the GDU...

Page 29: ...README file NOTE Functional checks of the system will be conducted as a part of the Production Acceptance Procedures NOTE Completion of the avionics installation is a good time to start gathering the...

Page 30: ...VAN S AIRCRAFT INC PAGE REVISION DATE 01 19 19 0 RV 12iS 42PiS 30 THIS PAGE INTENTIONALLY LEFT BLANK...

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