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WIRING DIAGRAMS XL-2 AIRPLANE
P/N 135A-970-100 Chapter 91 REVISION C Page 1 of 80
CHAPTER 91
WIRING DIAGRAMS
WIRING DIAGRAMS XL-2 AIRPLANE
Chapter 91 P/N 135A-970-100 Page 2 of 80 REVISION C
Copyright © 2009 All rights reserved. The information contained herein is proprietary to Liberty Aerospace, Incorporated. It is prohibited to reproduce or transmit in any form or by any means, electronic or mechanical, including photocopying, recording, or use of any information storage and retrieval system, any portion of this document without express written permission of Liberty Aerospace Incorporated.
WIRING DIAGRAMS XL-2 AIRPLANE
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Table of Contents SECTION 91-00 GENERAL 5
SECTION 00-01 WIRING STANDARDS 5 SECTION 00-02 WIRE NUMBERING 6 SECTION 00-03 WIRE COLOR CODE DESIGNATION 7
SECTION 91-01 AIRPLANE BLOCK DIAGRAM 9 SECTION 91-02 SCHEMATIC DIAGRAMS 13
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Section 91-00 General This chapter contains the wiring diagrams, schematics, and wire lists for the Liberty Aerospace, Inc. XL-2 airplane. These drawings are up-to-date as of the release of this chapter and are for general information only. Table 91-1 has the list of Liberty Aerospace, Inc. drawings and their current versions and forms a part of this chapter by reference. However, the most current version levels available from Liberty Aerospace, Inc. of these drawings should be used as the definitive source for information.
Part Number Description Revision135A-81-001 Schematic, Electric System General Layout B 135A-81-010 Schematic, Power Generation and Distribution P 135A-81-011 Schematic, Starting System H 135A-81-012 Schematic, Fuel System J 135A-81-013 Schematic, FADEC System Cable Harness P 135A-81-014 Schematic, VM1000FX K 135A-81-015 Schematic, Annunciation J 135A-81-016 Schematic, Flap System L 135A-81-017 Schematic, Pitch Trim System L 135A-81-018 Schematic, Interior Lighting M 135A-81-019 Schematic, Exterior Lighting M 135A-81-020 Schematic, Electric Gyro Instruments K 135A-81-023 Schematic, Facility Socket E 135A-81-024 Schematic, Emergency Locator Transmitter (121.5/243MHz) A 135A-81-026 Schematic, M803 OAT/ Clock C 135A-81-027 Schematic, Avionics System Garmin Layout A 135A-81-028 Schematic, Stall Warning F 135A-81-029 Schematic, Hour Meter C 135A-81-031 Schematic, EDI-200 Interface Harness A 135A-81-034 Schematic, Garmain Avionics Full Stack Interconnect H 135A-81-037 Schematic, Pitot Heat B 135A-81-044 Schematic, Artex Emergency Locator Transmitter (121.5/406MHz) A
Section 00-01 Wiring Standards Wiring used in the Wiring Diagrams for non-shielded wires are per MIL-W-22759. All non-shielded wires are 22 AWG unless otherwise noted. Wiring used in the Wiring Diagrams for shielded wires are per MIL-W-27500.
Table 91-1 Liberty Aerospace, Inc. XL-2 Airplane Schematic Drawings
WIRING DIAGRAMS XL-2 AIRPLANE
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Section 00-02 Wire Numbering Each wire in the XL-2 airplane has a unique number. The number defines what circuit or system the wire belongs to, the route for the wire, the route subsection, the gauge of the wire, and if the wire is a travelling ground.
Table 91-2 gives the system description for the subsystem designation on the wire number. The route subsection designation for the route from source to termination.
Sub System Designation System Description
A Antenna
AP Autopilot
C Clock and Facility socket
E Fuel System
EGND Earth Ground – ground to aircraft frame
F FADEC
G Gyro Instrumentation
H Pitot Heat, Hour Meter, Outside Air Temperature
IGND Instrumentation Ground – ground path isolated from Earth Ground
JPR Jumper Wire
L Lighting
P Power Distribution
R Avionics General
Figure 91-1 Wire Number Coding Standard
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Sub System Designation System Description
RD Avionics Display Systems (glass cockpit)
RG Avionics Garmin
RU Avionics UPS Aviation Technologies
SP Splice
ST Solder Sleave
T Trim Flaps
V VM1000FX
W Annunciation, Stall Warning
Section 00-03 Wire Color Code Designation Table 91-3 defines the abbreviations used in the schematics for various wire colors. If a wire has multiple colors, the different colors are separated by a forward slash ( / ) between each color. The base color is first, followed by the second significant color then the third significant color and so on.
For example, a wire that has a blue base color, then red then green, would have the designation BLU/RED/GRN.
Color Code Color
BLK Black
BRN Brown or Tan
RED Red
ORG Orange
YEL Yellow
GRN Green
BLU Blue or Azure
VIO Violet or Purple
SLT Grey or Slate
WHT White
SLD Shield
TIP Center conductor of a Coax Cable
Table 91-2 Subsystem Prefix Designation for Wire Numbers
Table 91-3 Wire Color Code Abbreviations
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Section 91-01 Airplane Block Diagram This section has the block diagram of the airplane’s electric system. Figure 91-2 shows the block diagram.
Figure 91-2 Block Diagram of the Liberty XL-2 Airplane
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Figure 91-3 through Figure 91-5 shows the hierarchy of the schematic drawings. The numbers shown within the dashed boxes are Liberty Aerospace, Inc. drawing numbers. Use this diagram as an aid to locate the correct drawings for a given system.
Figure 91-3 Drawings For the Two Battery Systems
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Figure 91-4 Drawing Hierarchy of the Main Power Distribution Bus
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Figure 91-5 Drawing Hierarchy
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Section 91-02 Schematic Diagrams This section contains schematic diagrams for the Liberty Aerospace, Inc. XL-2 airplane. These diagrams are for reference only and can be used for basic troubleshooting. The Liberty Aerospace, Inc. drawings called out in Figure 91-3 through Figure 91-5 and Table 91-1 are the most up-to-date and should be used as the most accurate. Differences between these drawings and a specific airplane are due to updates and changes that occurred after production of the airplane.
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Figure 91-6 Power Generation and Distribution
See Figure 91-23 See Figure 91-7
See Figure 91-12
See Figure 91-14
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Figure 91-7 Starting System
See Figure 91-6
See Figure 91-14
See Figure 91-11
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Figure 91-8 Fuel System
See Figure 91-10
See Figure 91-10
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Figure 91-9 FADEC System Cabin Harness (1 OF 3)
See Figure 91-13
See Figure 91-13
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Figure 91-10 FADEC System Cabin Harness (2 OF 3)
See Figure 91-8
See Figure 91-13
See Figure 91-8
See Figure 91-13
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Figure 91-11 FADEC System Cabin Harness (3 OF 3)
See Figure 91-7
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Figure 91-12 VM1000FX Engine Instrument System (1 OF 2)
See Figure 91-6
See Figure 91-17
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Figure 91-13 VM1000FX Engine Instrument System (2 of 2)
See Figure 91-10
See Figure 91-9
See Figure 91-10
See Figure 91-9
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Figure 91-14 Annunciator System
See Figure 91-38
See Figure 91-7
See Figure 91-6
See Figure 91-16
See Figure 91-15
Figure 91-23
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Figure 91-15 Flap System
See Figure 91-14
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Figure 91-16 Trim System
See Figure 91-14
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Figure 91-17 Interior Lighting
See Figure 91-23
See Figure 91-28
See Figure 91-12
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Figure 91-18 Exterior Lighting
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Figure 91-19 Electric Gyro Instrument System
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Figure 91-20 Facility Socket
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Figure 91-21 121.5/243 Mhz ELT Interconnect
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Figure 91-22 406/121.5 Mhz ELT Interconnect
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Figure 91-23 Outside Air Temperature Sensor and Clock System
See Figure 91-14
See Figure 91-26
See Figure 91-6
See Figure 91-17
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Figure 91-24 Avionics Power Distribution System
See Figure 91-28 MODEL COM C B NAV CBELIGIBLE
STACK POSITION S
GARMIN GNS 430 10 5 1, 2GARMIN GNS 530 10 5 1GARMIN SL30 5 2 1,2GARMIN SL40 5 2 1,2
RADIO OPTION CB RATINGS
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Figure 91-25 Stall Warning System
See Figure 91-36
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Figure 91-26 Hobbs Hour Meter
See Figure 91-23
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Figure 91-27 EDI-200 Interface Harness
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Figure 91-28 Avionics Stack
See Figure 91-24 See Figure 91-17
See Figure 91-24
See Figure 91-29, Figure 91-30, Figure 91-31, Figure 91-32, Figure 91-33, Figure 91-34, or Figure 91-35
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Figure 91-29 Avionics (Dual GNS System) 1 of 2
See Figure 91-30
See Figure 91-30 See Figure 91-30
See Figure 91-28
See Figure 91-36
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Figure 91-30 Avionics (Dual GNS System) 2 of 2
Figure 91-29 See Figure 91-29 See Figure 91-29
See Figure 91-36
See Figure 91-28
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Figure 91-31 Avionics (Single GNS/Single SL System)1 of 2
See Figure 91-32See Figure 91-32 Figure 91-31Figure 91
See Figure 91-36
See Figure 91-28
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Figure 91-32 Avionics (Single GNS/Single SL System) 2 of 2
Figure 91-31 See Figure 91-31 See Figure 91-31
See Figure 91-36
See Figure 91-28
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Figure 91-33 Avionics (Dual SL System) 1 of 2
See Figure 91-34 See Figure 91-34 See Figure 91-34
See Figure 91-36
See Figure 91-28
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Figure 91-34 Avionics (Dual SL System) 2 of 2
Figure 91-31Fi 91
See Figure 91-33 See Figure 91-33
See Figure 91-36
See Figure 91-28
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Figure 91-35 Avionics (GNS to SL Adapter)
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Figure 91-36 Avionics (Audio Panel)
See Figure 91-25 See Figure 91-29, Figure 91-30, Figure 91-31, Figure 91-32, Figure 91-33, Figure 91-34, or Figure 91-35
See Figure 91-28
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Figure 91-37 Avionics (Antenna Connections)
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Figure 91-38 Pitot Heating System
See Figure 91-14
QD55