Wiring Diagram for the Cessna Citation V
Cessna Citation V · Wiring Diagram
Overview
This document serves as a wiring diagram for the Cessna Citation V, providing detailed electrical schematics and connections for the aircraft's systems. It is intended for use by maintenance personnel and technicians who require a comprehensive understanding of the electrical layout and wiring configurations. The diagrams included in this document are essential for troubleshooting, repairs, and modifications to the aircraft's electrical systems. The wiring diagram outlines the various components, their locations, and the interconnections necessary for proper functionality of the aircraft's avionics and electrical systems.
- The wiring diagram is essential for understanding the electrical layout of the Cessna Citation V.
- Diagrams include connections for avionics, lighting, and power distribution.
- Component locations are crucial for maintenance and troubleshooting.
- Troubleshooting guidelines help identify common electrical issues.
Document
Source
Originally published by 560wiringdiagrams.z13.web.core.windows.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Wiring Diagram
- Pages
- 12
- File size
- 2.0 MB
- Publisher
- 560wiringdiagrams.z13.web.core.windows.net
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation V.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Cessna Citation V for sale now
Free — save the Citation V to your watchlist and track it in one place.
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- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
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- 1990 CESSNA CITATION V Specifications and SummarySpecifications
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In this document
Electrical System Overview
This section provides a general overview of the electrical system in the Cessna Citation V, including the main power sources, distribution systems, and circuit protection mechanisms. It highlights the importance of understanding the electrical architecture for effective maintenance.
Wiring Diagrams
Detailed wiring diagrams are presented, illustrating the connections between various electrical components such as avionics, lighting, and power distribution units. Each diagram is labeled for easy identification and reference.
Component Locations
This section lists the locations of key electrical components within the aircraft, including circuit breakers, relays, and connectors. Knowing these locations is crucial for efficient troubleshooting and repairs.
Troubleshooting Guidelines
Guidelines for troubleshooting common electrical issues are provided, including flowcharts and diagnostic steps to identify and resolve problems within the electrical system.
Safety notes
- Always disconnect power before servicing electrical components.
- Refer to the wiring diagram to avoid incorrect connections that could lead to system failures.
Full document text
Installation Notes: 1. Document must be printed in color. 2. 3. 4. 5. 6. Install, secure, and maintain separation of wiring in accordance with Cessna standard wiring practices manual Chapter 20. Where no other reference exist, use methods as described in this document. The typical clamping details as described on page 2 and page 3 of this document may be used. Where possible, maintain original Cessna wire routing design and philosophy. Maintain a minimum of 6 Inches separation distance from all critical Fuel Quantity Indicating System (FQIS) wiring. Where 6 Inches cannot be maintained, a minimum or 2 Inches must be maintained and rigidly supported and tied at intervals such that contact with the FQIS wiring would not occur assuming a broken wire and a missing wire tie or clamp. If the separation requirements of Installation Note 2 are not achievable in certain areas of the aircraft, then route all wires in those areas inside a protective sleeving (p/n ROUNDIT 2000 NX 5-5 OR equivalent). If the separation between FQIS wiring is less than 2 Inches, but greater than 1.0 Inch, then apply protective sleeving to either the new wiring or the FQIS wiring, not both. If the separation is less than 1.0 Inch, then apply protective sleeving to both new wiring and FQIS wiring. RF coax cable must be separated from all aircraft harnesses. Coaxial cable may be secured to the existing bundle, provided that the coax is separated from the main harness with closed cable tie connector rings (p/n CR4H-M/CR2-M) as applicable. Ensure that coaxial cable is bent at a radius of no less than 6 times (6X) the outside diameter of the cable. Ensure that the existing wiring being followed meets the separation requirements of Installation Note 2. Refer to Silverhawk Aviation drawing no. 17-23089-1 for complete details on electrical integration of wiring to aircraft. Rev. Revision Note: Date: IR hitial Release 4/30/2018 Silver Hawk AVIATION ENGINEER CJH CHECKED: APPROVED: Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 DATE: 4/30/2018 TITLE: GOGO AVANCE IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM DWG NO. Rev. IR AIRCRAFT MAKE: CESSNA CRS# 17-23089-WR YQSR759U SHEET: MODEL: CITATION 560 (CITATION V, ULTRA, ENCORE, ENCORE PLUS) 1 OF 4 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. WIRE ROUTING DETAIL EXISTING SECONDARY AIRCRAFT STRUCTURE (REF.) TIE WRAP P/N MS3367() TYPICAL CLAMPING DETAILS (TO EXISTING STRUCTURE) NEW OR EXISTING TIE MOUNT P/N TM3S10-M OR EQUILAVENT TIE MOUNT MAY BE RIVETED OR MECHANICALLY FASTENED IN PLACE AS REQUIRED STANDOFFS MAY BE USED IF REQUIRED TO CLEAR EXISTING STRUCTURE P/N NAS43()-() OR EQUIVALENT TYPICAL CLAMPING DETAILS (TO EXISTING STRUCTURE) EXISTING OR NEW CUSHION CLAMP P/N MS219190)() OR SIMILAR HARDWARE STANDOFFS MAY BE USED IF REQUIRED TO CLEAR EXISTING STRUCTURE P/N NAS43()-() OR EQUIVALENT TYPICAL CLAMPING DETAILS (TO EXISTING STRUCTURE) CUSHION CLAMP P/N MS2191900) Rev. Revision Note: IR hitial Release EXISTING SECONDARY AIRCRAFT STRUCTURE (REF.) Date: 4/30/2018 GROMMET P/N MS35489-()() OR MS21266-(0) MAY BE USED IF REQUIRED TYPICAL MOUNTING BRACKET FABRICATE LOCALLY NEW CUSHION CLAMP P/N MS2191900) NEW WIRES (REF.) NEW WIRES (REF.) 2 POINT FASTENING (MIN) SCREWS, WASHERS, AND NUTS OR RIVETS MAY BE USED TYPICAL CLAMPING DETAILS (THROUGH BULKHEAD) NAS430)-() SPACER OR EQUIVALENT NEW WIRES (REF.) EXISTING HARDWARE MAY BE RE-USED, INCREASE FASTENER LENGTH AS REQUIRED EXISTING WIRES (REF.) NEW CUSHION CLAMP P/N MS219190)() NEW WIRES (REF.) EXISTING HARDWARE MAY BE RE-USED, INCREASE FASTENER LENGTH AS REQUIRED EXISTING WIRES (REF.) Installation Notes: SUITABLE MS3367()() OR EQUIVALENT EXISTING WIRES (REF.) TYPICAL CLAMPING DETAILS SYSTEMS WIRING MAY USE ANY OF THE ABOVE LISTED CLAMPING DETAILS AS APPLICABLE FOR INSTALLATION. (TO EXISTING WIRING) Silver Hawk AVIATION ENGINEER: Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM CJH DATE: 4/30/2018 CHECKED: APPROVED MEETS THE SEPARATION REQUIREMENTS OF NOTE 2 (PAGE 1). ENSURE THAT THE EXISTING WIRING BEING FOLLOWED DWG NO. Rev. IR CRS# 17-23089-WR YQSR759U SHEET: 2 OF 4 AIRCRAFT MAKE: CESSNA MODEL: CITATION 560 (CTATION V, ULTRA, ENCORE, ENCORE PLUS) THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 11 WIRE ROUTING DETAIL USE NON MOISTURE ABSORBENT MATERIAL AS FILL FOR CLAMPS IF NEEDED NEW BUNDLE (REF.) NEW BUNDLE (REF.) 1/2" (MIN) STANDOFF BLOCK LACING CORD OR TIE WRAP USED AT ENDS NEW WIRE BUNDLE MAINTAINED ALONE 3" MAX 6" MAX EXISTING BUNDLE (REF.) ANTI-CHAFING MATERIAL USED (REF.) -6" MAX- EXISTING BUNDLE (REF.) B NEW WIRE BUNDLE MAINTAINED BELOW EXISTING BUNDLE NEW WIRE BUNDLE MAINTAINED ABOVE EXISTING BUNDLE EXISTING BUNDLE (REF.) NEW BUNDLE (REF.) 2" MAX 8" MAX Rev. Revision Note: IR hitial Release NEW WIRE BUNDLE MAINTAINED ALONE IN ANTI-CHAFING MATERIAL 8" MAX -16" MAX- -16" MAX- Date: 4/30/2018 NEW COAX CABLE MAINTAINED BELOW EXISTING BUNDLE EXISTING BUNDLE (REF.) NEW COAX MAINTAINED ABOVE EXISTING BUNDLE NEW COAXIAL CABLE (REF.) 1/2" (MIN) STANDOFF BLOCK -8" MAX- -8" MAX- -6" MAX- -6" MAX- 1/2" (MIN) STANDOFF BLOCK EXISTING BUNDLE (REF.) NEW COAXIAL CABLE (REF.) 1/2" (MIN) STANDOFF BLOCK
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CLAMPING AND SUPPORTING WITH "D" BLOCKS TO EXISTING BUNDLE WHERE IDEAL SEPARATION CANNOT BE MAINTAINED. Installation Notes: SYSTEMS WIRING MAY USE ANY OF THE ABOVE LISTED WIRE ROUTING DETAILS AS APPLICABLE FOR INSTALLATION. ENSURE THAT THE EXISTING WIRING BEING FOLLOWED MEETS THE SEPARATION REQUIREMENTS OF NOTE 2 (PAGE 1). Silver Hawk AVIATION ENGINEER CJH CHECKED: APPROVED: Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 DATE: 4/30/2018 TITLE: GOGO AVANCE IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM DWG NO. Rev. IR AIRCRAFT MAKE: CESSNA CRS# 17-23089-WR YQSR759U SHEET: MODEL: CITATION 560 (CITATION V, ULTRA, ENCORE, ENCORE PLUS) 3 OF 4 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 10 12 2.4 GHz Wifi ARINC 429 Source Circuit Breaker Panel ATG Antenna Antenna 1 ATG Antenna WiFi Switch 'J-BOX 5 GHz Wifi Antenna Terrestrial Modem Antenna \LRU and ACM 2.4 GHz Wifi Antenna Mount Λ 000000 Rev. IR Revision Note: hitial Release Silver Hawk AVIATION ENGINEER CHECKED CJH DATE: 4/30/2018 Date: 4/30/2018 Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM DWG NO. ARINC 429 Terrestrial APPROVED: Circuit Breaker Loc: Aft Bulkhead Rev. Source Modem Antenna Panel ATG Antenna Fuselage Station: 365.00" ATG Antenna IR AIRCRAFT MAKE CESSNA CRS# 17-23089-WR YQSR759U SHEET: 4 OF 4 MODEL: CITATION 560 (CITATION V, ULTRA, ENCORE, ENCORE PLUS) THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 10 12 Date: Rev. Revision Note: C Updated L3 Antenna connections tomatchounentdata andfinal productionofLRU 10/19/2018 26 GoGo Biz 2 ATG 3G Antenna (Ci-5500 for L3 Install Only) P12949 25 TE Connectivity 1 Cabin Entertainment Relay FCA125-34 1. 24 Vivisun 1 Switch, Panel Mount, DPDT, Annunciator 95-52-14-E6-E28DA 2. 23 Vivisun 1 Switch, Panel Mount, DPDT, Annunciator 95-52-14-E6-E28DB ITT Cannon A/R 9/37 pin Clip with Long Screw D20419-16 3. ②1 ITT Cannon A/R Screw and Hex Nut assembly D20418-2 20 ECS 32 TNC coax connector, Straight CTS122 4. Acceptable alternates listed in Installation Instructions. A/R TNC coax connector, 90 deg (ALTERNATE) CTR122 5. All wires are 22 AWG unless otherwise noted. 19 ECS 16 SMA coax connector, Straight CSS122 6. All diodes are 1N4007 unless otherwise noted. Acceptable alternates listed in Installation Instructions. A/R SMA coax connector, 90 deg (ALTERNATE) CSR122 7. "A/R" = As Required 18 Pasternack Enterprises 8 TNC Male to TNC Female Extension PE9270 8. Pasternack Enterprises 8 SMA Female to SMA Female Adapter, Standard PE9070 9. 16 AMP 21 Backshell Strain Relief, 9 pin 5207908-1 15 TE Connectivity 1 Connector, 9 pin receptacle (female) 205203-8 TE Connectivity 1 Connector, 9 pin plug (male) 205204-9 13 AMP 2 Backshell Strain Relief, 15 pin 5207908-4 (12) TE Connectivity A/R Contact, socket (female) 205090-1 11 TE Connectivity A/R Contact, pin (male) 205089-1 10. Installation Notes: All wire and wire routing in accordance with AC43-13-1B Chapter 11 and component manufacture Recommendations. All shielded wire to be MIL-C-27500 or equivalent. Non- shielded wire to be MIL-W-22759/16 or equivalent unless otherwise noted. All Ethernet cable to be PIC p/n E51424 or equivalent unless otherwise noted. All Coax cable to be ECS p/n 311201 or equivalent unless otherwise noted. * next to letter signifies the letter is lower case Illustration Key: New Wire / New Equipment: Existing Wire / Existing Equipment: Flag note: A BOM Item Reference note: Information omitted for clarity: Cap and Stow wire: Relocate wire as shown: All equipment is configured and ground tested per the manufactures installation manual. Total cumulative length of IFE402A24 USB Cable shall not exceed 17 feet maximum length 16 connection to ANNUNCIATOR TEST GND OUT. OPTIONAL CONNECTION - Use any available open pin listed for OPTIONAL CONNECTION - Use any available open pin listed for connection to GROUND ON GROUND. OPTIONAL CONNECTION: Use any available open pin. Bus to existing load shed capable entertainment bus located AFT interior J box. Applicable to Avance L5/L5i Installations ONLY. 21 Applicable to Avance L3 Installations ONLY. OPTIONAL CONNECTION - Use any available ARINC connection available on aircraft. Verify ARINC output offers sufficient data in accordance with Installation Instructions. Default ARINC 429 inputs on Port 1. Wire according to aircraft equipment available. OPTIONAL CONNECTION - Use any available open pin listed for connection to 28/14V ANNUNCIATOR POWER. (10 TE Connectivity 1 Connector, 15 pin receptacle (female) 205205-7 11. TE Connectivity 1 Connector, 15 pin plug (male) Wire Number Key: 205206-9 -GTX001A20N- L-Com 1 Type A USB Panel Mount with Wire Leads ECJ504B-UA # OF WIRE CONDUCTORS L-Com 1 RJ45 Panel Mount with Wire Leads ECJ504-8 ⑥ Klixon 2 Circuit Breaker, 10 Amp ⑤ GoGo Biz 21 TM Antenna P18350-001 7277-2-10 2 = SHIELDED PAIR 4 = SHIELDED QUAD WIRE NUMBER WIRE SEGMENT WIRE CONDUCTOR AWG OPTIONAL INDICATOR 0 = SINGLE 1 = SHIELDED SINGLE SYSTEM 3 = SHIELDED TRIPLE N = GND V = POWER L = LIGHTING GoGo Biz 6 WIFI Antenna P16917-001 Silver 12. GoGo Biz 2 ATG4G 900 MHz Quad Mode Antenna P35500 All USB cable to be PIC p/n USB2422 or equivalent unless Hawk otherwise noted. AVIATION ENGINEER HENDRIX DATE: 5/17/2017 GoGo Biz 1 Configuration Module Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. P14126 CHECKED 13. GoGo Biz 1 Avance L5/L5i/L3 Air-To-Ground 4G Transceiver P34110-XXX ITEM VENDOR QTY DESCRIPTION PART NUMBER Perform EMI/EMC source victim testing in accordance with paragraph 11-107D of AC43.13-1B. Verify that the installed APPROVED: equipment does not interfere with or is not interfered with by any other aircraft system. This testing should include but is not limited to all navigation, flight guidance, auto-pilot and communication systems. CESSNA MODEL: CITATION C560 17-23089-1 YQSR759U SHEET: 1 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. K. OWEN 3/8/2018 DWG NO. Rev. CRS# AIRCRAFT MAKE: 12 ACM ACM1 2 POWER GND 15 -IFEODIA20N- 28V DC AIRCRAFT POWER 8 -IFE002A20- GND Loc: Aft Partitian GOGO BIZ AVANCE L5/ L5; /L3 4GP1 40 Ft 28V DC AIRCRAFT POWER A -IFE002B16- CHASSIS GND B -IFED03AIGN- CHASSIS GND с -IFE004AIGN- POWER GND D -IFED05AIGN- Loc: Lav Baggage Floor CABIN ENT B OFF ON A В XB C 0 D G AN4 24 GND GND GND P1 Rev. Revision Note: с Updated 13 Antenna comedionstomatchounentdata andfinal productionofLRU Date: 10/19/2018 CABIN BUS CTL 30 -BUSODIA14 25 25A A2 A3 -BUSO03A14- A1 ATG X2 A R1 X1 10A CABIN ENTERTAINMENT BUS Loc: Adjacent to RH CB Panel -BUSO02A18- 10A 28V DC BUS 2A J10 Loc: Pilot Side Wall Reference: CESSNA 560 WDM: 33-10-03 IFE007822 7 -IFE007A22- IFE008822 8 -IFE008A22- Reference: CESSNA 560 WDM: 31-50-01 { A3 A A1 A4 FARM A2 B4 B3 B -FEB0BB22- 5 -IFEO06A22- B2 B1 IFE009822N 6 -IFE009A22N- GND As BF ANNUN +28/DIM --- J1A 16 Loc: Pilot Side Wall 17 ANNUN. TEST OPTIONAL CONNECTION - use any available open pin listed for connection to 28/14V ANNUNCIATOR POWER. OPTIONAL CONNECTION - Use any available open pin listed for connection to ANNUNCIATOR TEST GND OUT. Add Diode P/N: 1N4007 as shown Silver Hawk AVIATION ENGINEER HENDRIX Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 DATE: 5/17/2017 CHECKED K. OWEN 3/8/2018 APPROVED: Rev. AIRCRAFT MAKE: CESSNA TITLE: GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. DWG NO. CRS# MODEL: CITATION C560 17-23089-1 YQSR759U SHEET: 2 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 11 GOGO BIZ AVANCE L5/ L5i /L3 Loc: Lav Baggage Floor 4GP2 ARINC 429 IN 1A ARINC 429 IN 1B 33 (w) 23 IFE 202A 22= (b) ARINC 429 IN 1A 33 (w). ARINC 429 IN 1B 23 (b) 40f+ CIFE 201A22 Rev. Revision Note: Date: C Updated L3 Antenna connectionstomatchcument data and final production ofLRU 10/19/2018 P7501 GARMIN TOUCHSCREEN NAVIGATOR GTN750 2322 (w) 10 ARINC 429 OUT 1A (b) 29 ARINC 429 OUT 1B 2322 PF703 (w) (b) (w)-- (b) JJ (b)- Loc: FMS CDU DISC. Loc: Center Instr. Panel P1711 # 1 UNS-1 CSP CDU P2 (w) 21 ARINC 429 OUT 2A (b) 22 ARINC 429 OUT 2B Loc: Pedestal Universal Configuration Select Label: DEFAULT Select Label: DEFAULT Select Label: DEFAULT OPTIONAL CONNECTION - Use any available ARINC connection available on aircraft. Verify ARINC output offers sufficient data in accordance with Installation Instructions. Default ARINC 429 inputs on Port 1. Wire according to aircraft equipment available. Silver Hawk ARINC Label Name Attitude Attitude Rate Computed Airspeed Time to Go Garmin Configuration Select Label :76 Select Label: 212 Select Label: 206 Change Config to: 352 AVIATION ENGINEER HENDRIX DATE: 5/17/2017 Change Config to: 352 CHECKED K. OWEN 3/8/2018 APPROVED: ETA Change Config to: Calculated Change Config to: Calculated Rev. AIRCRAFT MAKE CESSNA Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. DWG NO. CRS# MODEL: CITATION C560 17-23089-1 YQSR759U SHEET: 3 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. GOGO BIZ AVANCE L5/ L5/L3 4GP2 ETHERNET PORT 10 TX + 41 (red). ETHERNET PORT 10 TX- 42 (blu) IFE401A24: ETHERNET PORT 10 RX + 53 (yel) ETHERNET PORT 10 RX-30 (grn). Rev. Revision Note: C Updated L3 Antenna connections tomatchaunentdata andfinal productionofLRU Date: 10/19/2018 4GP7 (red) 1 -BLUE- (blu) 2 -ORANGE- Ꮎ (yel). 3 -BLACK- L-COM (grn) 6 -YELLOW- 4 -RED- 5 -GREEN- 7 -BROWN- 8 -WHITE- USB VBUS POWER 21 (red). (red). 11 -RED- L.COM USB GND USB DATA + 32 USB DATA 56 (blk) (blk) 12 -BLACK- 1FE402A24: (grn) (grn) 13 -GREEN- 44 (wht). (wht) 14 -WHITE- 15 -GRAY- Loc: Lav Baggage Floor ACM Loc: Aft Partitian 4GP3 LAN_MDI TX1 +110 (red) LAN_MDI TX1-87 (blu) LAN_MDI RX1 + 109 (yel) LAN_MDI RX1-88 (grn) ACM1 (2) ETHERNET RX + 9 (red) ETHERNET RX- 1 ETHERNET TX + ETHERNET TX - 2 (blu) FE403A24 10 (yel) (grn) CHASSIS GND 7 CHASSIS GND 11 CHASSIS GND 3 14131 Loc: LH AFT Lavatory Equipment Bay Silverhawk Aviation Inc. Total cumulative length of IFE402A24 USB Cable shall not exceed 17 feet maximum length Silver Hawk AVIATION ENGINEER DATE: HENDRIX 5/17/2017 CHECKED K. OWEN 3/8/2018 DWG NO. APPROVED: Rev. AIRCRAFT MAKE: CESSNA KLNK 1751 West Kearney Ave. Lincoln, NE 68524 MODEL: TITLE: GOGO AVANCE L3/L5/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. CRS# CITATION C560 17-23089-1 YQSR759U SHEET: 4 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 10 Loc: Pilot Side Wall J10 BF J1A Loc: Pilot Side Wall ANNUNCIATOR TEST: 17 GOGO BIZ AVANCE L5/ L5/L3 4GP2 WIFI # 1 ENABLE 70 WIFI # 2 ENABLE 104 TM ENABLE 69 (GND WOW) WEIGHT ON WHEELS 78 POWER ENABLE 71 HEATER ENABLE 55 FAN ENABLE 57 GND 84 ATG4G DATA ENABLE 79 SBB DATA ENABLE 77 Loc: Lav Baggage Floor 母 } Reference: CESSNA 560 WDM: 33-10-03 -IFEDIDA22- -IFEDIA22- } Reference: CESSNA 560 WDM: 31-50-01 30 Ft -IFEO12A22- 30f7 -IFEOI5A22- -IFEO13A22N- -IFED14A22N- H GND GND 411 GND 161412 IFE012022N- 4GP8 Rev. Revision Note: C Updated 13 Antenna.connections tomatchounentdata andfinal productionofLRU AN5 1 FEDI0822 ABC G B B IFEDH022 0 WIFI 3 IFEO12822- -IFED12C22N- Loc: Behind Pilot's Instr. Panel ++ J349 D ON OFF Gi G - F A4 A3 A A2 A1 B4 B3 B B2 B1 Loc: Pilot's Instr. Panel Loc: Pilot Side Wall (LH Console Disconnect) Reference: CESSNA 560 WDM: 32-60-02 C* GROUND ON GROUND Date: 10/19/2018 A OPTIONAL CONNECTION - Use any available open pin listed for connection to 28/14V ANNUNCIATOR POWER. OPTIONAL CONNECTION - Use any available open pin listed for connection to ANNUNCIATOR TEST GND OUT. OPTIONAL CONNECTION - Use any available open pin listed for connection to GROUND ON GROUND. Silver Hawk AVIATION ENGINEER Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE L3/LS/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. HENDRIX DATE: 5/17/2017 CHECKED K, OWEN 3/8/2018 DWG NO. APPROVED: Rev. AIRCRAFT MAKE: CESSNA 17-23089-1 YQSR759U SHEET: 5 OF 8 MODEL: CRS# CITATION C560 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. GOGO BIZ AVANCE L5/ L5i /L3 4GP1 2.4 GHz 5 GHz WIFI 1 WIFI 1 WLAN ANTENNA 1 WLANIA-311201: WIFI 2 WIFI 1 WLAN ANTENNA 2 WLAN 2A-311201: WIFI 3 WIFI 1 WLAN ANTENNA 3 WLAN 3A-311201: W1C 19174 1914 WIFI 4 W4C WIFI 2 WLAN ANTENNA 4 WLAN 4A-311201 WIFI 5 WIFI 2 WLAN ANTENNA 5 WLAN 5A-3112013 WIFI 6 WIFI 2 WLAN ANTENNA 6 WLANGA-311201: Loc: Lav Baggage Floor TM 1 TM ANTENNA 1 TM 2 TM ANTENNA 2 19 (8 plcs) CTMIA-311201: CTM 2A-311201: Rev. Revision Note: C Updated 13 Antenna connections tomatchounentdata and final productionofLRU W2C WIFI CH1 ANT 1 FWD F.S. 221.7 3-3-8 1914 W3C 1914 WIFI CH1 ANT 2 MID F.S. 242.8 WIFI CH1 ANT 3 AFT 1914 W5C TM1C 1915 WIFI CH2 ANT 1 FWD F.S. 282.7 WIFI CH2 ANT 2 MID F.S. 303.0 WIFI CH2 ANT 3 AFT 1914 W6C 19 17 5 TM2C FWD TM ANT 1 Date: 10/19/2018 F.S. 262.6 F.S. 323.7 F.S. 303.5 AFT TM ANT 2 F.S. 323.7 Silver Hawk AVIATION ENGINEER HENDRIX Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 DATE: 5/17/2017 TITLE: GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. CHECKED K. OWEN 3/8/2018 DWG NO. APPROVED: Rev. 17-23089-1 AIRCRAFT MAKE: CESSNA CRS# MODEL: CITATION CS60 YQSR759U SHEET: 6 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 10 11 12 GOGO BIZ AVANCE L5/L5¡ 4GP1 H1 ATG ANTENNA 1 FWD H1 ATGIJ1-311201: H2 ATG ANTENNA 1 RIGHT H2 CATGIJ2-311201: V1 ATG ANTENNA 2 FWD V1 AT GIJ3-311201: V2 ATG ANTENNA 2 RIGHT V2 ATGIJ4-311201: H3 ATG ANTENNA 1 AFT H3 CAT 62J1-311201: H4 ATG ANTENNA 1 LEFT H4 ATG2J2-311201: V3 ATG ANTENNA 2 AFT V3 AT G2J3-311201: V4 ATG ANTENNA 2 LEFT V4 AT G2J4-311201: (21 (8 plcs) AFT BLKHD F.S. 365 Loc: Lav Baggage Floor 2J4 2J3L 2J2 2J1 18 20 (4 pics) F.S. 392 Rev. Revision Note: C Updated L3 Antenna connectionstomatchounentdataandfinal productionofURU Date: 10/19/2018 1J4 18 20 (4 pics) F.S. 188 20 Applicable to Avance L5/L5i Installations ONLY. Silver Hawk AVIATION ENGINEER Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 HENDRIX DATE: 5/17/2017 TITLE: CHECKED K. OWEN 3/8/2018 GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. DWG NO. APPROVED: Rev. AIRCRAFT MAKE: CESSNA CRS# MODEL: CITATION C560 17-23089-1 YOSR759U SHEET: 7 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 12 GOGO BIZ AVANCE L3 L3P1 ATG ANTENNA 1 FWD V1 ATG ANTENNA 1 FWD H1 ATG ANTENNA 2 AFT V1 ATG ANTENNA 2 AFT H1 Loc: Lav Baggage Floor Blic 37 CAT GIJI-3112013 CAT GIJ 2-311201: ATG2J1-311201: ATG2J2-311201: AFT BLKHD F.S. 365 Red. U 18 20 F.S. 392 Rev. Revision Note: C Updated 13 Antenna connections tomatchounentdata andfinal production ofLRU P F.S. 188 Date: 10/19/2018 ✓ Applicable to Avance L3 Installations ONLY. Silver Hawk AVIATION Silverhawk Aviation Inc. KLNK 1751 West Kearney Ave. Lincoln, NE 68524 TITLE: GOGO AVANCE L3/15/L51 IN-FLIGHT ENTERTAINMENT AND WIFI CONNECTIVITY SYSTEM. ENGINEER HENDRIX DATE: 5/17/2017 CHECKED K. OWEN 3/8/2018 DWG NO. APPROVED: Rev. AIRCRAFT MAKE CESSNA MODEL: CRS# CITATION C560 17-23089-1 YQSR759U SHEET: 8 OF 8 THIS DOCUMENT DISCLOSES SUBJECT MATTER IN WHICH SILVERHAWK AVIATION INC. HAS PROPRIETARY RIGHTS, NEITHER RECEIPT NOR POSSESSION THEREOF CONFERS OR TRANSFERS ANY RIGHT TO REPRODUCE OR DISCLOSE THE DOCUMENT, ANY PART THEREOF, ANY INFORMATION CONTAINED THEREIN, OR ANY PHYSICAL ARTICLES OR DEVICE, OR TO PRACTICE ANY METHOD OR PROCESS EXCEPT BY WRITTEN PERMISSION FROM OR WRITTEN AGREEMENT WITH SILVERHAWK AVIATIONINC. 10