Wsi Av-200 Installation Manual
Jul 29, 2003 Commercial Biz-Av; Feature Stories. 'WSI InFlight' Cockpit Weather System Certified by FAA. Plus installation. WSI also offers the WSI InFlight.
From Pacific Coast Avionics the WSI INFLIGHT™ provides a continuous stream of airspace and weather information directly to the cockpit during flight via satellite. Co-developed with NASA, WSI InFlight’s data link and automatic update service keeps pilots aware of situations as they unfold, increasing flight decision confidence. Intuitive information displays designed specifically for aviation with high “glance-value” Flexible display options compatible with numerous hand-held, portable and panel-mounted avionic displays Reliable & accurate with 24 x 7 quality control monitoring by WSI staff meteorologists Award winning aviation weather continuously updated every 5 minutes via satellite broadcast Complete coverage in the air and on the ground anywhere in the continental U.S. And most of Canada WSI InFlight AV200 system (Certified to DO-160D) also comes with InFlight Receiver, software and Antenna.
Affordable, flat-rate subscription plans make WSI InFlight a ‘must have’ for serious pilots.Co-developed with NASA, WSI InFlight™ is a patented system that provides a continuous stream of mission-critical weather information to your portable or panel-mounted display with complete coverage and content for the continental U.S. At any altitude. WSI InFlight™ TECHNICAL SPECIFICATIONS System: Satellite: Geosynchronous Satellite Connectors: Included Cabling: Not included Antenna: Manufactured By: Comant Profile: Low-Profile Teardrop Weight: 4.20 oz Height: 0.7 in Connector: TNC Certification: DO-160D Receiver: Dimensions: 1.49 in x 5.42 in x 8.47 in Weight: 1.5 lbs (excluding mounting tray and connectors) Power Requirement: 10.0 to 32 VDC, Low Power.
Read Microsoft Word - 600-00174-001 MLB WSI 970-0300 Install Manual.doc text version INSTALLATION MANUAL INSTALLATION MANUAL AV- 300 /350 Broadcast Datalink Receiver Document Number: Revision: Date: 970-0300-IM 01 26 July 2007 ©2007 WSI Inc. 400 Minuteman Road Andover, MA 01810 +1 (978) 983-6300 SPECIAL NOTE TO INSTALLERS The following important issues regarding the WSI Broadcast Datalink Receiver AV-300/350 installation should be noted during the planning stages. See Section 2 for additional information: 1. The WSI AV-300/350 conforms to the requirements of Technical Standard Order (TSO) Authorization, TSO-C157. The AV-300/350 receiver may be mounted in either a vertical or horizontal orientation.
The AV-300/350 is mounted with integral flanges. The AV-300/350 receiver needs to be well grounded to the airframe. Section 2 has detailed instructions about proper connection. The AV-300/350 supports up to 2 independent displays using RS-232 ports COM1 and COM2. A third listen-only display may be connected to the RS-422 transmit port, and Electronic Flight Bags (EFBs) may be connected to the Ethernet port. Do not connect this device to the essential electrical bus. These installation instructions assume that the receiver and antenna can be installed in a structurally sound manner in accordance with the installation manual and AC 43.13.
All the aircraft certification requirements must remain in compliance. The Electrical Load Analysis, Functional Hazard Assessment and other certification requirements for the aircraft must remain in compliance. An Electrical Load Analysis must be accomplished to determine that the electrical limits of the specific aircraft are not exceeded. Mounting the satellite antenna on composite and pressurized aircraft requires engineering guidance beyond the scope of this manual. The remote control antenna is mounted within the cabin at a location with an unobstructed line of sight to the location(s) where the remote control will be used. An obstruction would consist of parts or surfaces that might interfere with radio frequency communications such as metallic parts or surfaces. The remote control will NOT function with the AV-300/350 receiver until it has been 'paired' with the receiver.
See Remote Control Pairing on page 8 for additional information. The receiver also needs to be authorized for audio product for the remote control to function. Please refer to page 8 for the activation instructions.
970-0300-IM Rev. 011, 26 July 2007 ii WSI AV-300/350 Installation Manual TABLE OF CONTENTS Special Note to Installers. Ii Table of Contents.
Iii List of Figures. V List of Tables. V Revision Index. Vi Section 1 GENERAL INFORMATION.7 Introduction. 7 Product Description. 7 Intended Function.
8 Radio Activation. 8 Remote Control Pairing. 8 List of the Major Components.
9 Installed System Configuration. 9 Units and Accessories Supplied. 10 Units and Accessories Required, But Not Supplied. 11 Installation and Approval Basis. 12 Sources of Industry Guidance.
13 Installation Requirements and Limits for the Proposed Modification. 13 Physical Location of Installed Equipment. 14 Human Factors. 14 Interface to Existing Equipment. 14 Instructions for Continued Airworthiness. 15 Hardware / Software Compatibility Matrix.
15 Location of Data Required by TSO. 15 Installation Limitations. 17 Environmental Qualifications AV-300/350 Receiver. 18 Environmental Qualifications Remote Control. 20 Section 2 INSTALLATION.22 General.
22 RS-232 Connections. 22 RS-422 Connections.
22 Satellite Antenna Installation. 22 Remote Control Antenna Placement Evaluation. 22 Receiver Antenna Connections.
23 Power Input Line and Ground Return. 23 Audio. 23 Installation in a Severe EMI Environment. 23 General Installation Considerations. 23 Getting Started. 24 Clamping and Routing Wires.
24 Receiver Grounding. 24 Cable Shields. 24 Satellite Antenna Placement. 24 970-0300-IM Rev. 011, 26 July 2007 iii WSI AV-300/350 Installation Manual Remote Control Antenna Placement. 25 Receiver Installation. 26 Receiver Mounting.
26 Equipment Interfaces. 28 Discrete Interfaces.28 Audio Panel Interface.29 Display Interface.29 Electronic Flight Bag Interface.29 Receiver Connections. 29 Communication and Power Connector (P1).29 Satellite Antenna Connector (J1).36 Remote Control Antenna Connector (J2).36 Ethernet Connector (J3).37 USB Connector (J4).37 Satellite Antenna Installation. 37 Evaluating Satellite Antenna Location on the Aircraft. 37 Satellite Antenna Mounting. 37 Satellite Antenna Connections and Wire Routing. 38 Remote Control Antenna Installation.
38 Evaluating Remote Control Antenna Locations. 38 Remote Control Antenna Mounting. 38 Remote Control Antenna Connections and Wire Routing. 38 Section 3 INSTALLATION CHECKOUT.39 General. 39 Power up. 39 Remote Control Pairing Procedure.
39 Replacing Batteries in the RC70. 40 Installation Checkout Procedures. 40 Audio Suppression Input. 40 Interference Checks. 40 Interference Check AV-300/350 and Remote Control as Offender.40 Interference Check AV-300/350 and Remote Control as Victim.41 Section 4 FACTORY SERVICE POLICIES.42 TECHNICAL SUPPORT.
42 GENERAL SERVICES PROCEDURES. 42 Documentation. 43 Return Authorization. 43 Warranty Service. 43 Section 5 TROUBLESHOOTING GUIDE.44 970-0300-IM Rev. 011, 26 July 2007 iv WSI AV-300/350 Installation Manual LIST OF FIGURES Figure 1: Front Panel of the AV-300/350 Receiver.
26 Figure 2: Dimensions of the AV-300/350 Receiver. 27 Figure 3: AV-300/350 Receiver Wiring Diagram Communications Connections. 33 Figure 4: AV-300/350 receiver Wiring Diagram Audio, Power and Discrete Connections. 34 LIST OF TABLES Table 1-A: Equipment specifications.
7 Table 1-B: Major components comprising the equipment system complying with TSO-C157. 9 Table 1-C: Standard AV-300/350 System with part numbers. 10 Table 1-D: Units and accessories required but not supplied.
11 Table 1-E: Certification data. 12 Table 1-F: Sample Description of Work Accomplished. 12 Table 1-G: Certification data. 15 Table 1-H: Environmental Qualifications of the AV-300/350 Receiver. 18 Table 1-I: Environmental Qualifications of the Remote Control. 20 Table 2-A: Connector (P1) Pin Assignments.
30 Table 5-A: Failure and Warning Conditions and Possible Solutions. 44 970-0300-IM Rev.
011, 26 July 2007 v WSI AV-300/350 Installation Manual REVISION INDEX Revision 00 01 Date 29 June 2007 26 July 2007 Remarks Initial Release Update to define Remote Pairing with MLB 970-0300-IM Rev. 011, 26 July 2007 vi WSI AV-300/350 Installation Manual Section 1 INTRODUCTION GENERAL INFORMATION This manual contains detailed instructions for the installation and checkout of the WSI Broadcast Datalink Receiver AV-300/350. For maintenance and repair information, contact WSI Customer Support. Installation tips are found in Section 2, Installation. PRODUCT DESCRIPTION The WSI AV-300/350 receives broadcast data and audio content from the Sirius Radio satellite network, and conforms to the requirements of TSO-C157. The AV-300 model is capable of receiving WSI InFlight weather content only.
Software Installation Manual
The AV-350 is capable of receiving WSI InFlight weather content as well as Sirius audio programming. Aviation data content received via this datalink, such as graphical weather products, is made available to display devices via RS-232, RS-422, and Ethernet communications ports. Audio content is available for entertainment purposes, and may be controlled by a wireless RF remote control or from a connected display device with audio control capability. The AV-350 also supports discrete inputs for volume, muting, and channel control (see the wiring diagam and pinout table for further information). Table 1-A: Equipment specifications. Receiver Mass: Antenna Mass: Cooling: Receiver Dimensions: (See Figure 2 on page 27) Operating Voltage Current Audio Output 1.6 lbs. (726 g.) 4 ounces (114 g) Convection 6.0 inches (152 mm) x 8.0 inches (203 mm) x 1.5 inches (38 mm) 10-32 Volts DC 0.3 Amp @ 28VDC; 0.6 Amp @ 14VDC 600 ohm, 1 RMS 970-0300-IM Rev.
011, 26 July 2007 7 WSI AV-300/350 Installation Manual INTENDED FUNCTION The intended function of the AV-300/350 is to provide reception of weather and other data products that will assist the flight crew in assessing whether current conditions are suitable to the flight characteristics of their aircraft. The AV-300/350 Broadcast Datalink Receiver is an aircraft Flight Information Services Broadcast (FIS-B) receiver that meets the requirements of TSO-C157. Additional related features in the form of broadcast audio content are also made available. RADIO ACTIVATION The AV-300/350 must be activated to enable reception of data and audio content. If the AV300/350 is audio-enabled, then the Sirius Radio preview channel will be available prior to activation, and will be automatically tuned upon initial power-on. The preview channel may be used for installation checkout. An active subscription to the Sirius Radio service will be required in order for the aircraft owner or passengers to listen to audio content other than the preview channel.
The aircraft owner can find instructions for activating the Sirius radio service in the pilot's guide, part number 970-0350-PG. REMOTE CONTROL PAIRING For installation of audio-enabled receivers, the RF remote control must be 'paired' with the receiver. This allows the remote control to recognize and communicate with the installed receiver.
Once paired the remote control and receiver will remember the pairing even after power is removed from the receiver; however there may be some circumstances that require the remote control and receiver to be paired again. See Remote Control Pairing Procedure on page 39 for additional information on the pairing process.
970-0300-IM Rev. 011, 26 July 2007 8 WSI AV-300/350 Installation Manual LIST OF THE MAJOR COMPONENTS The following is a list of the major components that make up the equipment system complying with the standards prescribed in TSO-C157. The WSI Broadcast Datalink Receiver AV-300/350 System consists of a receiver, antenna, and a compatible Display. The receiver must be combined with an appropriate display that accepts the AV-300/350 protocol.
Table 1-B: Major components comprising the equipment system complying with TSO-C157 Component AV-300/350 Receiver Remote Control (optional) Aircraft Antenna Remote Control Antenna (optional) Adapter Cable (optional) Part Number 420-0300-RC 420-0350-RM 420-ANTS-TD 420-0350-AN 891-0300-IA INSTALLED SYSTEM CONFIGURATION The receiver can serve multiple external displays. Each display interfaces to the receiver through its own bi-directional RS-232 port. One of the two RS-232 ports (COM1) is also available as an RS-422 port. The RS-422 transmit port may always be used to support a single receive-only display; however the RS-422 receive port should only be used when the COM1 RS232 port is not used.
Either of the RS-232 ports may be used asynchronously, but the COM1 RS-232 port may also be used synchronously. Contact WSI for information regarding compatible displays. The AV-300/350 also supports electronic flight bags (EFB) through the 10/100 Base-T Ethernet port. Refer to the installation instruction provided with the EFB for additional details. 970-0300-IM Rev. 011, 26 July 2007 9 WSI AV-300/350 Installation Manual UNITS AND ACCESSORIES SUPPLIED The components supplied as part of the AV-300/350 system are shown in Table 1-C.
The receiver must be combined with an appropriate display that accepts the AV-300/350 protocol. Table 1-C: Standard AV-300/350 System with part numbers Component Receiver unit Aircraft antenna Installation kit Installation manual Warranty card Interface Adapter (optional) Remote control Remote antenna Remote connector kit Pilot Guide ICA (instructions for continued airworthiness) Part Number 420-0300-RC 420-ANTS-TD 420-0300-CN 970-0300-IM 970-0300-WA 891-0300-IA 420-0350-RM 420-0350-AN 420-0350-CN 970-0350-PG AVSSG-008 AV-300 X X X X X (X) AV-350 X X X X X X X X X X X 970-0300-IM Rev. 011, 26 July 2007 10 WSI AV-300/350 Installation Manual UNITS AND ACCESSORIES REQUIRED, BUT NOT SUPPLIED NOTE: Materials used for installation of the WSI AV-300/350 must be of a type acceptable to the regulatory agency with authority to approve installations. In the case of TSO-C157, one means of showing compliance is contained in the Federal Aviation Regulations (FAR), Part 25, Appendix F. If the materials recommended in this manual do not conform to the agency requirements, then substitute materials meeting the electrical requirements may be used.
Table 1-D: Units and accessories required but not supplied. Wiring RS-232: 22 AWG twisted, shielded pair or triple cable, length limit is 45 feet (15 meters). RS-422: 22 AWG twisted, shielded pair, length limit is 200 feet (61 meters). Power & Ground: 22 AWG twisted, shielded pair, length limit per AC 43.13-1B Figure 11-2.
Chassis Ground (if case is not grounded): 22 AWG. Other Connections: 22 AWG, length limit 30 feet (10 meters).
Antenna cables: 50 coaxial cable. RG-142 or equivalent cable is recommended, but not required. For RG-142 cable, length must be at least 3 feet and no more than 50 feet.
If other cable type is used, cable and connector losses should be no more than 9.5dB. See AC 43.13-1B Sections 5, 6 and 7 for other wire requirements.
Circuit Breaker Trip-free resettable, 2 Amp (14 or 28-volt systems). RF Connectors TNC: Two TNC plug connectors appropriate for the coaxial cable used. These will be mounted on the satellite antenna cable and will connect to the antenna on one end and J1 on the other. BNC: Two BNC plug connectors appropriate for the coaxial cable used. These will be mounted on the remote control antenna cable and will connect to the remote control antenna connector adapter on one end and J2 on the other.
The installer may optionally provide a reverse-polarity SMA (RP-SMA) connector for the remote control antenna end of the cable. Providing the cable-mounted RPSMA eliminates the need for the remote control connector adapter and one of the BNC plug connectors. 970-0300-IM Rev. 011, 26 July 2007 11 WSI AV-300/350 Installation Manual INSTALLATION AND APPROVAL BASIS The WSI AV-300/350 complies with the requirements of TSO-C157. Certification may require preparation of an FAA Form 337. See Table 1-F below for sample verbiage.
The information and wording should be modified to correctly describe the particular installation. Data that can be used as a basis for approval for return to service are identified in Table 1-E below. Table 1-E: Certification data. STC Documents.
AC 43.13-1 (Chapters 11 and 12) and 2, (Chapters 1, 2 and 3). TSO Markings. Manufacturer's installation instructions. Table 1-F: Sample Description of Work Accomplished 8.
Description of Work Accomplished (If more space is required, attach additional sheets. Identify with aircraft nationality and registration mark and date work completed.) A. The following equipment and components were installed: 1.
The WSI AV-300/350 receiver was installed in (position in the aircraft) according to instructions in Installation Manual, P/N 970-0300-IM, dated (Insert date & revision of manual), and guidance in FAA Advisory Circular 43.13-1( ). An electrical load analysis was performed and found that the continuous load on the alternator (generator or other supply) does not exceed 80% of capacity. A complete operational test was performed according to WSI AV-300/350 Installation Manual, P/N 970-0300-IM, dated (insert date & revision of manual).
The equipment performed satisfactorily and did not adversely affect existing components or systems in the aircraft as required by 14 CFR 23.1301 (or 14 CFR 25.1301, 14 CFR 27.1301, or 14 CFR 29.1301 as applicable). The aircraft equipment list was revised to reflect these changes; weight and balance data were revised and placed in the aircraft records. An WSI AV-300/350 Pilot Operating Handbook, P/N 970-0350-PG dated (insert date & revision of Handbook), and (insert associated application handbooks as appropriate) were placed in the aircraft. Equipment installation procedures do not differ significantly among various aircraft. The installation and operation of the WSI AV-300/350 does not materially affect aircraft operation or performance. Assumes no responsibility for alterations to the airframe.
970-0300-IM Rev. 011, 26 July 2007 12 WSI AV-300/350 Installation Manual With appropriate aircraft certification (such as field approval or STC), the WSI AV-300/350 is eligible to be installed in small or transport category aircraft (United States 14CFR Parts 23, 25, 27 and 29). SOURCES OF INDUSTRY GUIDANCE Advisory Circulars AC43.13-1b and 43.13-2a are two sources, but not the only sources, for industry guidance. The following sections of AC43.13-1b and 43.13-2a are pertinent to this installation. The documents are available from the FAA web site: www.faa.gov.