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GA 36 OR GA 37
GARMIN GPS ANTENNA
GEA 24
GARMIN ENGINE
INDICATION
SYSTEM
GAD 29
GARMIN DATA
INTERFACE
ADAPTER
AV-60007
IGNITION
MODULE
2X GDU 460
G3X TOUCH
FLIGHT DISPLAY
F-00214
F-00212
GARMIN AFT PITOT LINE
GARMIN AOA LINE
GTX 35R
GARMIN TRANSPONDER
GMA 245
GARMIN AUDIO PANEL
GTN 650
GARMIN GPS/NAV/COM
GMC 307
GARMIN CONTROL PANEL
GSU 25
GARMIN AIR DATA
ATTITUDE HEADING
REFERENCE SYSTEM
SECTION 42PiS:
GARMIN G3X
NAV/COM SYSTEM
GMU 11
GARMIN
MAGNETOMETER
F-00216
GARMIN STATIC LINE
VAN'S AIRCRAFT, INC.
AV-532L
VOR/LOC/GS ANTENNA
(AV-532L CABLE)
DATE OF COMPLETION:
PARTICIPANTS:
01/19/19
0
RV-12iS
DATE:
REVISION:
PAGE:
42PiS-01
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Summary of Contents for Van's Aircraft G3X
- Page 1 VAN'S AIRCRAFT, INC. GA 36 OR GA 37 GTX 35R GARMIN GPS ANTENNA GARMIN TRANSPONDER SECTION 42PiS: GEA 24 GMA 245 GARMIN ENGINE GARMIN AUDIO PANEL INDICATION SYSTEM GTN 650 GARMIN GPS/NAV/COM GARMIN G3X GMC 307 GARMIN CONTROL PANEL NAV/COM SYSTEM...
- Page 2 VAN'S AIRCRAFT, INC. NOTE: If the VS-1213 V-Stab Tip Fairing has already been riveted to the top of the V-Stab Assembly, it be will necessary to drill out the rivets securing the fairing. Step 1: Separate the F-00205 Nutplate Spacer...
- Page 3 VAN'S AIRCRAFT, INC. Step 1: Locate the F-00203 Nav Antenna Doubler on the VS-1205 as shown in Figure 1. F-00203 4X MACH CSK MS21051L3 Step 2: Match-Drill #30 the forward and aft-most holes in the F-00203 into the web of the VS-1205. Cleco each hole before drilling...
- Page 4 VAN'S AIRCRAFT, INC. 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 NOTCH FOR 1/32-1/16 [.8-1.6 mm] VS-1205. CLEARANCE ALL SIDES 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.
- Page 5 VAN'S AIRCRAFT, INC. Step 1: Drill #19 a hole in the VS-1208 Rib at the location shown in Figure 1. Step 2: Fabricate the F-00204 Nav Antenna Conduit by cutting a piece of NT Duct 5/8 to a length of of 44 1/2 in. [113 cm].
- Page 6 VAN'S AIRCRAFT, INC. Step 1: Drill #30 a hole in the F-1278 Top Skin at the location shown in Figure 1. 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.
- Page 7 VAN'S AIRCRAFT, INC. Step 1: Drill #30 a hole in the center of the inboard flange of the F-1238-R as the location shown in Figure 1. NOTE: When positioning and securing the AV-532L cable in the following steps, ensure that the AV-532L cable is not rubbing on the sharp edge of of the F-1279-R Upper Right Skin stiffener, and is clear of all control cables.
- Page 8 VAN'S AIRCRAFT, INC. Step 1: Route the AV-532L cable up the F-1281-R stiffener, passing through the lightening holes in each of each fuselage frame as shown in Figure 1. NOTE: Airframes with dual pass through holes in the F-01202B-1 should route the AV-532L cable through the foremost DAB OF RTV OR hole.
- Page 9 VAN'S AIRCRAFT, INC. Step 1: Reinstall the V-Stab Assembly to the airframe, while simultaneously routing the AV-532L cable through the F-00204. See Figure 1. A piece of safety wire passed through the F-00204 prior to reassembly can be used to pull the AV-532L cable up through the F-00204 if necessary.
- Page 10 VAN'S AIRCRAFT, INC. Step 4: If necessary, disconnect and discard the F-00013 Static Line Tee-ADAHRS from the F Plastic Tee and F-00014 Static Line Tee Upsize. See Section 10iS/U and the detail view in Figure 3. Step 5: Connect the Aft Pitot Line to the F Plastic Tee using the F-00014 as described in Section 10iS/U. If necessary, trim the Aft Pitot Line as required to prevent interference or chafing on the surrounding structure.
- Page 11 VAN'S AIRCRAFT, INC. Step 1: Remove the F-01206E-1 Baggage Floor Cover, previously installed in Section 38iS/U. Step 4: Bolt the GSU 25 to the ADAHRS Baggage Floor Assembly as shown in Figure 2. Step 2: Cleco the F-00082 ADAHRS Stiffener to the F-01206E-1. Final-Drill #11 the four holes indicated in Figure 1. Disassemble and debur.
- Page 12 VAN'S AIRCRAFT, INC. Step 9: Loosely secure the F-00212, F-00214, and F-00216 to the ES-00301 using a tie wrap as shown in Figure 2. Leave the tie wrap loose enough to allow the lines to slide through when the ADAHRS Baggage Floor Assembly is removed.
- Page 13 VAN'S AIRCRAFT, INC. Step 1: Route the F-00214 forward through the fuselage, following the CT-01204 Fuel Cable Assembly through the snap bushings as shown in Figure 1. Step 2: Route the forward end of the F-00214 through the center snap bushing in the F-12103 Tunnel Brace as shown in Detail A in Figure 1.
- Page 14 F-00063 NOTE: Do not match-drill the #27 hole 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 VAN'S AIRCRAFT, INC. Step 1: Rivet the F-00063-L and nutplates to the forward side of the F-01202B-1 Panel Base flange as shown in Figure 1. Step 2: Mirror Step 1 for the right side of the aircraft to rivet the F-00063-R to the F-01202B-1.
- Page 16 VAN'S AIRCRAFT, INC. Step 5: Separate the F-00054-1 Inst Stack Angle Nav/Com by removing the hatched areas shown in Figure 3. Step 6: Machine countersink the nutplate rivet holes in the F-00054-1-L & -1-R, then install the nutplates as shown in Figure 3.
- Page 17 VAN'S AIRCRAFT, INC. NOTE: Check both sides of the firewall for clearance before match-drilling holes to prevent inadvertent damage. 4X TEMPORARY #10 SCREWS Step 1: Temporarily remove the Rotax Fuse Box from the forward side of the F-01201A-1 Firewall Top. See GEA 24 DRILL GUIDE Section 46iS.
- Page 18 VAN'S AIRCRAFT, INC. GARMIN GTN 650 MOUNTING RACK NOTE: Refer to Figure 1 for all steps on this page. (INSTALLED ON NEXT PAGE) Step 1: Rivet the F-00130-L & -R GTN 650 Support Bracket and the F-00054-1-L & -1-R to the F-01202B-1, placing the manufactured rivet heads below the F-01202B-1.
- Page 19 VAN'S AIRCRAFT, INC. NOTE: The COM, NAV, and GPS coax cables use solid-core conductors which are prone to overstraining. They should be the last cables connected to the GTN 650 Backplate, and should not be kinked or bent tighter than 1 in. [25.4 mm] radius.
- Page 20 VAN'S AIRCRAFT, INC. Step 1: Assemble the Garmin GMA 245 backplate and the d-sub connectors labeled "J2401" and "J2402" from the WH-00136 as shown in the GMA 245 Installation 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 GTX 35R RACK Figure 1.
- Page 21 VAN'S AIRCRAFT, INC. Step 1: Apply a thin smear of fuel tank sealant around the three holes called out in Figure 1. Step 2: Install the GEA 24 Engine Indication System and F-00145 GEA24 Adapter Plate onto the F-01201A-1 Firewall Top with the hardware called out in Figure 1.
- Page 22 VAN'S AIRCRAFT, INC. NOTE: The figures and instructions below show the GA 36 antenna. The GA 37 antenna is optional for customers who plan to use XM data with their G3X system. Installation procedures are the same for both antennas.
- Page 23 VAN'S AIRCRAFT, INC. NOTE: Refer to Figure 1 for all steps on this page. Step 1: Install the GAD 29 onto the F-01202B-1 using screws, washers, and nuts as shown. Step 2: Install the IBBS-12V-3AH Back-Up Battery onto the F-01202B-1 using screws, washers, and nuts. Connect the P7211, P7213, and P7251 ground terminals from the WH-000136 to the corners of the IBBS-12V-3AH as shown.
- Page 24 VAN'S AIRCRAFT, INC. Step 1: Connect the 9-pin and 25-pin d-sub connectors labeled "GAD 29" from the WH-00136 to the GAD 29 as shown in Figure 1. Step 2: Connect the 15-pin d-sub connector labeled "BATT" from the WH-00136 to the IBBS-12V-3AH.
- Page 25 VAN'S AIRCRAFT, INC. Step 1: Temporarily install the F-00043S onto the Upper Forward Fuselage Skin Assembly. See Section 29iS/U and Figure 1. Step 6: Use two screws to temporarily attach nutplates to the aft side of the F-1202D-L as shown in Figure 2. Use the hole drilled in Step 2 to locate Step 2: Match-drill #27 the hole indicated in Figure 1 into the F-1202D-L Panel Attach Strip.
- Page 26 VAN'S AIRCRAFT, INC. Step 1: Attach the AV-60007 Ignition Module Assembly to the F-00043S with screws as shown in Figure 1. Step 2: Remove the ES SW K1-AABAAAAA switch from the WH-00136, then install the switch and ES-807039-1 Gasket into the F-00043S. Ensure the switch orientation matches the detail view in Figure 1.
- Page 27 VAN'S AIRCRAFT, INC. NOTE: Refer to Figure 1 for all of the steps on this page. NOTE: Some of the fasteners used to install the instrument panels are not shown on this page. Replace fasteners previously used in Section 29iS/U (to install the F-12133 Instrument Panel Jig) with fasteners called out on this page.
- Page 28 VAN'S AIRCRAFT, INC. NOTE: Refer to Figure 1 for the following steps. Step 1: Connect the 25-pin d-sub connector labeled "IGNITION" from the WH-00136 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.
- Page 29 Ensure all unused optional connectors from the Main Wire harness are securely stowed and restrained from movement. [25.4 mm] overlap. Step 6: After you have completed all remaining sections of the KAI, download the RV-12iS G3X configuration files from the Van's Step 3: Ensure the lines are free of debris, then website and update the software configuration as described in the README file.
- Page 30 VAN'S AIRCRAFT, INC. THIS PAGE INTENTIONALLY LEFT BLANK 42PiS-30 RV-12iS 01/19/19 PAGE: REVISION: DATE:...