Installation Manual MAP-9101-10x-x Moving Maps Server Document # 540372 MAP-9101-100-x MAP-9101-101-x 7300 Industry Drive, North Little Rock, AR 72117 Phone: 501-955-2929 Fax: 501-955-2988 www.decraneaerospace.com DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual Document Revision History Rev. Level IR Date 12/2008 Description Initial Release Reference Documents (or latest revision) Description MAP-9101-100-x Outline Drawing MAP-9101-101-x Outline Drawing Document # 526167 Rev B 526371 Rev IR Service Bulletin List Service Bulletin # Subject Manual Revision Revision Date Table of Illustrations Section # 2.1 7.0 Description Block Diagram – Typical Application Reference Drawings Page # 5 22 PROPRIETARY INFORMATION NOTICE: Despite any other copyright notice, this document and information disclosed herein contains confidential, proprietary designs owned by DeCrane Aerospace Audio International. Neither this document nor the data contained herein shall be reproduced, used or disclosed to anyone without the written authorization of DeCrane Aerospace Audio International. Document # 540372, Rev IR, 12/2008 Page 1 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual Table of Contents Section 1.0 Description Page 1.1 1.2 1.3 General Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Purpose of the Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . Optional Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 3 3 4 2.1 2.2 2.3 Application . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Block Diagram – Typical Applications . . . . . . . . . . . . . . . . . Typical Equipment Interfaces . . . . . . . . . . . . . . . . . . . . . . . Additional Interfaces . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 5 5 6 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 3.10 Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Prior to Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Unpacking and Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . Cautions & Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Wiring Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Updating Logo File . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Updating Audio Briefings . . . . . . . . . . . . . . . . . . . . . . . . . . . Electrical Characteristics . . . . . . . . . . . . . . . . . . . . . . . . . . . Mating Connector Information . . . . . . . . . . . . . . . . . . . . . . . Pinout Assignment Descriptions . . . . . . . . . . . . . . . . . . . . . Post-Installation Test . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 8 8 9 10 11 12 16 17 20 24 4.0 Instructions for Continued Airworthiness . . . . . . . . . . . 24 5.0 General Troubleshooting Procedures . . . . . . . . . . . . . . . 24 6.0 Specifications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 7.0 Reference Drawings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAP-9101-100-x’s Reference Drawings. . . . . . . . . . . . . . . MAP-9101-101-x’s Reference Drawings. . . . . . . . . . . . . . . 26 26 28 2.0 3.0 7.1 7.2 Document # 540372, Rev IR, 12/2008 Page 2 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual MAP-9101-10x-x Moving Maps Server 1.0 General Information 1.1 Introduction This manual contains information for the proper application and installation of the DeCrane Aerospace Audio International (DAAI) server, Model No: MAP-9101-10x-x. The MAP-9101-10x-x is a Moving Map Server with a Single Compact Flash Hard Disk Drive and the ability to display the end user’s customized logo. The “x” in the “-10x” designates the differences between units. The MAP-9101-101-x can be used to navigate and control the interactive map screens and audio briefings (initiated via discrete inputs and/or data bus commands). The MAP-9101-100-x does not have interactive map screens or audio briefings. The “-x” suffix in both models designates the type of connector utilized; “-1” = Positronic and “-2” = DSubminiature. Also included are physical, mechanical, and electrical characteristics of the unit. 1.2 Purpose of the Equipment The MAP-9101-10x-x Onboard Server Module provides support for interactive and non-interactive moving maps via local video outputs and to remote client devices. It also contains circuitry to support special purpose applications such as HTTP Server, and Digital Media Audio Briefings. The MAP-9101-10x-x provides the following key features: Motherboard (not all functions are necessarily used) • 1.0GHz ULV Celeron M 373 Processor • Up to 512kB Level 2 Cach • Up to 1GB DDR SODIMM o Supports a single +2.5V DDR RAM SODIMM o Supports PC2700 DDR 333 (166MHz) • Frontside Bus @ 400MHz • AGP 128-bit 3D video interface with built-in dual-channel LVDS • Dual PCI-bus Enhanced Ultra DMA 33/66/100 Synchronous IDE interface supports up to four storage devices • (2) Serial TTL Level Interface • Single IrDA 1.1 Infrared Interface • (4) USB 2.0 • AC97 CODEC for Audio Interface Document # 540372, Rev IR, 12/2008 Page 3 of 29 DeCrane Aerospace Audio International • • • • • MAP-9101-10x-x Installation Manual 10/100 BaseT Ethernet interface Watchdog Timer Real-Time Clock Customizable Splash Screen for OEM boot logo Configuration EEPROM – 512 Bits Data / Interface / Configuration Ports • Dual 10/100Base-T Ethernet Interfaces o Full-Duplex o Half-Duplex o IEEE 802.3x Flow Control in Full-Duplex Mode o Auto-Negotiation for Speed, Duplex Mode, and Flow Control • Serial Ports o RS-232 o RS-485 for AI Standard Data Bus o ARINC 429 Receiver for Flight Management System (FMS) Interface (x2) • USB – Two (2) USB 2.0 Ports • 16 Gigabyte Industrial Grade Compact Flash Video • Composite NTSC Video Output • SMPTE-259 SDI Video Output • SVGA Video Output Audio - MAP-9101-101-x Model Only • Two (2) mono Analog Briefer Audio Outputs – 2Vrms o Both Outputs Play the Same Briefer o Briefer Pause Discrete Input o Briefer Active Key Output • Audio Briefings o Up to 100 1.3 Optional Equipment DeCrane Aerospace Audio International offers a comprehensive family of Cabin Control Modules for PC interfaces. These modules provide convenient solutions for a variety of frequently encountered interfacing needs or special requirements and are an important part of DAAI’s “building block” system for configuring total cabin management. Contact your DAAI representative for details. Document # 540372, Rev IR, 12/2008 Page 4 of 29 DeCrane Aerospace Audio International 2.0 MAP-9101-10x-x Installation Manual Application 2.1 Block Diagram – Typical Application S * * * * * Only available for model MAP-9101-101-x. 2.2 Typical Equipment Interfaces 2.2.1 Video Output (SVGA, NTSC Analog, and SDI) Typical interfaces include various video distribution and/or signal manipulation devices. The unit is capable of interfacing and providing output to all DeCrane Aerospace Audio International and standard COTS (Commercial-Off-The-Shelf) video devices and/or equipment. 2.2.2 Briefer Audio Output (Mono Analog) This interface is only available for model MAP-9101-101-x. Typical interfaces include various audio distribution and/or signal manipulation devices. The unit is capable of interfacing and providing output to all DeCrane Aerospace Audio International and standard COTS audio devices and/or equipment. Two outputs of the same signal are provided for connection to multiple devices. Document # 540372, Rev IR, 12/2008 Page 5 of 29 DeCrane Aerospace Audio International 2.3. MAP-9101-10x-x Installation Manual Additional Interfaces 2.3.1 Audio Interface This interface is only available for model MAP-9101-101-x. This unit provides for the routing of the audio briefer to two (2) audio briefer outputs to allow routing of the briefer to two separate locations. Analog Audio Outputs Output Level: 2.0Vrms 2.3.2 Video Interfaces This unit provides for four (4) independent video outputs: One (1) SVGA Video, one (1) NTSC Video, and two (2) SDI-Video. SVGA Video Output Industry standard SVGA video output in 800x600 resolution NTSC Video Output Output Level: 1.0 Vp-p Output Impedance: 75-ohm Video Formats: NTSC SDI-Video Output Serial Digital Video in SMPTE 259M format. 2.3.3 Infrared Interface Infrared interfaces are optional for this unit. Functionality relating to possible infrared capability is interfaced via one of the provided data communication interfaces. 2.3.4 Discrete Interface(s) This unit provides for two (2) discrete interfaces. The discrete output (GND active) actives the primary audio briefer. The discrete input (GND active) is used to pause the briefer. Document # 540372, Rev IR, 12/2008 Page 6 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 2.3.5 Data Communication Interface(s) 2.3.5.1 RS-232 (Serial Port) This unit incorporates one (1) RS-232 serial data bus interface for general purpose communication to external devices. Full hardware handshaking capability is provided. 2.3.5.2 ARINC 429 This unit incorporates two (2) individual and isolated receive-only ARINC 429 serial data bus interfaces to obtain flight-specific information provided via an aircraftintegrated flight management system (FMS). Each interface goes to a common program and is set for low speed. Although it can be set for high speed, both inputs must be the same speed. Each interface is configurable for either a high-speed (100 Kbps) or a low-speed (12.5 Kbps) data rate. 2.3.5.3 RS-485 (Standard) This unit incorporates one (1) RS-485 serial data bus interface for communication purposes to other DeCrane Aerospace Audio International RS-485 network-connected devices. All RS-485 serial data bus electronic interface parameters are compliant to AI document #640071. 2.3.5.4 10/100Base-T Ethernet This unit incorporates one (1) Intel 82551QM (10/100 Base-T) Ethernet network interface for communication purposes to other network-connected devices. The Ethernet interface is compliant to IEEE 802.3 specifications and requirements. 2.3.5.5 USB 2.0 This unit incorporates two (2) USB 2.0 interfaces (2 root hubs, J5 and J6 connectors). The Logo File can be updated to display the end user’s customized logo by loading the file through either of the USB connections, see Section 3.5 for instructions. Document # 540372, Rev IR, 12/2008 Page 7 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual Only model MAP-9101-101-x’s can be used to connect a USB mouse connection for map control. Either USB port will accept the mouse connection. 3.0 Installation 3.1 Prior to Installation 3.1.1 During the design and layout of the aircraft cabin, careful consideration of the location of the MAP-9101-10x-x is necessary. Some of the items to be considered include: • • • • • • • Space Proximity to other devices (i.e. source equipment) Available power supply Length of cable runs Environmental conditions (temperature, humidity, etc.) Location of other aircraft systems (i.e. oxygen delivery) Access for service repair (if applicable) 3.1.2 The MAP-9101-10x-x shall be installed to conform to the standards designated by the customer, installing agency, and existing conditions as to the unit location and type of installation. 3.1.3 Mounting provisions are provided via four (4) 0.187-inch diameter mounting holes – two (2) on each side of unit on provided mounting flanges. Refer to Section 7.0, Reference Drawings, for mounting hole diameters and configuration. 3.1.4 The unit is capable of installation/mounting in any orientation whether horizontal, vertical, inverted, or at an angle. 3.1.5 An internal fan exhausts heat from the unit. Proper ventilation must be allowed for when specifying the installation location. The closeout area of the monitor shall have a clearance of 2 inches (5.08 cm) minimum for the air inlet and exit areas. The closeout area of the monitor case shall not block the air inlet or exhaust openings of the monitor case. The fan will only run when the unit is turned on. 3.1.6 Installation requires 2-inch spacing from other equipment, modules, and structures except the mounting surface for which the unit should be in direct contact. Document # 540372, Rev IR, 12/2008 Page 8 of 29 DeCrane Aerospace Audio International 3.2 MAP-9101-10x-x Installation Manual Unpacking and Inspection 3.2.1 Carefully open the packaging and remove the unit. Verify that all components have been included in the package per the packing list. Inspect the unit for damage. Retain the packing materials and packing list. 3.2.2 If damage has occurred during shipping, a claim should be filed with DeCrane Aerospace Audio International WITHIN 24 hours and a Return Request Authorization Number shall be obtained from DAAI by contacting the Repair Department at 501.801.8101. Repackage the unit in its original packaging materials and return it to DAAI following instructions given by the DAAI representative. Refer to the front cover of this manual for address. If no return is necessary, retain the packing list and the packing materials for storage. 3.3 Cautions and Warnings 3.3.1 It is important to do a pin-to-pin power and ground check on all connectors. Ensure that power and ground are applied only where specified. Damage to the unit may result if power or ground is applied to the wrong points. 3.3.2 DO NOT connect or disconnect the module while power is applied. 3.3.3 DO NOT remove any factory-installed screws. Damage to the unit may result and void any warranties. 3.3.4 No periodic scheduled maintenance or calibration is required for continued airworthiness of the MAP-9101-10x-x. If the unit fails to perform to specifications, it must be removed and serviced by a qualified service facility. 3.3.5 ESD (Electro Static Discharge) guidelines shall be followed. 3.3.6 The chassis material and structural design of the unit is such that the unit is not capable of containing fire and/or flames within the unit. Document # 540372, Rev IR, 12/2008 Page 9 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 3.3.7 The chassis material and structural design of the unit is such that the unit is not capable of waterproof operation. Additionally, the unit provides no specific or special provisions for fluid penetration resistance to internal electronic components and/or assemblies. 3.4 Wiring Requirements 2.4.1 Introduction The installing agency must supply and fabricate all external cables and mating connectors. The length and routing of external cables must be carefully studied and planned before attempting installation of the equipment. Allow adequate space for installation of cable and connectors. Avoid sharp bends and placing cables near aircraft control cables. Maintain a minimum clearance of three (3) inches from any control cable. If wiring is run parallel to combustible fluid or oxygen lines, maintain a separation of six (6) inches between the lines. 3.4.2 Power Wires DeCrane Aerospace Audio International recommends that the chassis be electrically bonded to the airframe structure by the resistance using <50 impedance grounding lug with <0.1 cable. Power and Ground wires shall be in accordance with M22759 or equivalent. Protect power wires with circuit breakers or fuses located close to the electrical power source bus. 3.4.3 Single Signal Wires All single signal connections are recommended to use 22 AWG (minimum) in accordance with NEMA WC 27500 or equivalent. 3.4.4 Multiple and/or Differential Signal Connections All multiple and/or differential signal connections (i.e., analog audio, RS-485 data bus communication, etc) are recommended to use 22 AWG (minimum) shielded twisted pair or shielded three-conductor as necessary in accordance with NEMA WC 27500 or equivalent. 3.4.5 Analog Composite Video Connections All analog composite video connections are recommended to use shielded coaxial cable in accordance with M17/94-RG179 or equivalent. Document # 540372, Rev IR, 12/2008 Page 10 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 3.4.6 Composite and SDI Video Connections Composite and SDI video connections are recommended to use shielded coaxial cable in accordance with PIC V76261 or equivalent. 3.4.7 SVGA wiring shall be in accordance with NEMA WC 27500 or equivalent. 3.4.8 USB Connections USB connections are recommended to use shielded twisted pair in accordance with PIC USB2422 or equivalent. 3.4.9 10/100Base-TX Ethernet network connections All 10/100Base-TX Ethernet network connections are recommended to use shielded Category 5e equivalent Ethernet cabling compatible with aircraft environments. Either a 4-conductor or 8-conductor cable may be utilized. Each conductor shall be stranded with an overall conductor gauge of 24 AWG, MINIMUM. Overall conductor diameter (including jacket) shall conform to mating connector requirements. Ethernet connections shall conform to EIA/TIA 568 standards. PIC Wire & Cable P/N: E10424 (4-conductor) or E50824 (8-conductor) or equivalent cabling is recommended for 10/100Base-T Ethernet cabling requirements. Cable capable of supporting a minimum sustained data communication rate of 100 Mbps is required. 3.5 Updating Logo File This device has the ability to automatically upgrade the logo file that is displayed on the logo page to allow an end user to install their custom logo. The procedure to do this requires use of the USB flash drive that comes with the unit or an equivalent compatible USB flash drive. The logo file must be in GIF format with a resolution of 800 x 600. The file must be named logo.gif in lower case letters. This file must be stored on the USB flash drive in a directory named “logo” in lower case letters. For example, if the flash drive appears as drive F: when inserted in a laptop, the directory and file name would appear as “F:\logo\logo.gif”. The directory letter may be different on the computer that is used to copy the logo.gif file to the flash drive. When the map server is active, insert the USB flash drive into either of the USB drives (J5 or J6 connector). The map server will automatically recognize the insertion of the flash drive and will copy the logo.gif file from Document # 540372, Rev IR, 12/2008 Page 11 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual the \logo\ directory. The map server will automatically reboot after the file is copied. During the boot process, the USB flash drive must be removed. If the USB flash drive is not removed during the reboot process, the Map Server will continue to reboot as it recognizes the drive after start up and recopies the logo file. 3.6 Updating Audio Briefings 3.6.1 Installing Audio Briefings Equipment required: • • Laptop computer Ethernet cross over cable Software required: • • An SFTP over SSH2 client. (Recommended: Filezilla version 2.2.4 or later, A.I. part number 14500102 or available from http://filezilla-project.org/) A text editor 3.6.2 Playlist Creation Prepare all audio files that will be used for briefings. Since the playlists are case sensitive it is recommended that lower case be used exclusively for audio file names. However, as long as the playlist contains the exact case, no problems will result from mixed case. Each playlist is a standard text file and can be created using Notepad or any other text editor. Microsoft Word or other word processing software is not acceptable since documents created by them will contain non-visible control characters. A playlist can contain one or more audio file names listed in the order to be played. These files will be concatenated with no space between them during play. For example, if you have three files named greeting.mp3, takeoff.mp3 and close.mp3 that you desire to play in sequence then the playlist will have the following structure: greeting.mp3 takeoff.mp3 close.mp3 Document # 540372, Rev IR, 12/2008 Page 12 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual Playlist files must have specific names in order for the control software to locate and play them when they are triggered by an external command. The file name also contains a number which is used to select that list. There can be up to 100 playlists on the server. A playlist filename always starts with the characters “pl” in lower case followed by the two digit playlist number and terminated with “.m3u”, exactly as shown. For example: Playlist number 0 1 15 Filename pl00.m3u pl01.m3u pl15.m3u Playlists that are not named according to this convention will not be playable by the control software. 3.6.3 Loading Files onto Server Once the audio files and playlists have been created, they can be loaded onto the server as indicated in the following procedure: 1. Configure the laptop to access the server. The IP address of the laptop must be configured for the same subnet as the server in order to make connection. Manually configure the laptop IP address to 10.0.0.20/22 2. Attach the crossover cable to the laptop and the server. 3. Start the SFTP over SSH2 client software. Enter the user name, password and Server IP address as indicated below: Name: root Password: lazy8ball IP address: 10.0.0.1 Note: Filezilla setup is as indicated in the example below: (It is highly recommended that you use Filezilla) 4. Using the SFTP software, copy the audio files into the server directory “/data/mpd/audio” directory and the playlists into the “/data/mpd/playlist” directory. 5. Close the SFTP software, disconnect from the server and restart the map server. 6. Installation is complete. Document # 540372, Rev IR, 12/2008 Page 13 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 3.6.4 Setup for Filezilla To setup Filezilla and establish a connection, start Filezilla and press Ctrl+S to open the site manager. You will see a screen similar to the one shown below. Select “New Site” and enter the following information in the proper boxes: Host: 10.0.0.1 Servertype: select “SFTP over SSH2” User: root Password: lazy8ball Press the “Connect” button. If the connection is successful, you will be able to see the server file structure appear on the right center portion of the screen. The left center portion of the screen contains the file system of the laptop. On the left side, navigate to the folder that contains your audio and playlist files. On the right side navigate to the folder as shown in step 4 of the loading procedure above. (Note: Double click on the “..” folder to move up a level. The right side starts in the root user’s folder, you have to move up one level first in order to get to the drive’s root directory.) Document # 540372, Rev IR, 12/2008 Page 14 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual Select the desired files on the left side, then drag and drop them into the proper directory on the right. Document # 540372, Rev IR, 12/2008 Page 15 of 29 DeCrane Aerospace Audio International 3.7 MAP-9101-10x-x Installation Manual Electrical Characteristics 3.7.1 Electrical Specifications Electrical Audio Output Nominal Power Maximum Power 1 A at +28 VDC 1.5 A at +28 VDC Operating Voltage Range +18 to +32 VDC +28 VDC preferred Output Type Output Impedance Balanced, Stereo 2 VRMS (optimum) 1 VRMS (minimum) 600 Frequency Response 20 Hz to 20 kHz Signal-to-Noise Ratio Total Harmonic Distortion (THD) 85 dB or greater Output Level General Video Video Interfaces VGA Video Output Composite Video SDI Video Output Output Level Output Impedance 0.1% or less VGA, Composite Video, and SDI SVGA video output up to 800 x 600 resolution @ 32-bit color 1.0 V(p-p) 75 Video Formats NTSC Output Type SMPTE-259 Data Rate 270 Mbps 3.7.2 Input Power This unit operates at a MAXIMUM power consumption of 1.50A at +28VDC with an operating voltage range of +18VDC (minimum) to +32VDC (maximum). QUIESCENT operating power consumption, by design, should not exceed 1.00A at +28VDC. Final power consumption is at the discretion of the designer, but must not exceed the stated MAXIMUM. 3.7.3 Grounding / Bonding This unit provides for common circuit ground and chassis ground connections. Both circuit and chassis grounds are referenced to pin two (2) of connector J1. Circuit/chassis ground connection shall be bonded to an electrically conductive chassis mounting point or Document # 540372, Rev IR, 12/2008 Page 16 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual frame ground with less than 0.010-ohm resistance using less than 50-ohm impedance cable. 3.7.4 Power Interruption This unit is capable of maintaining full normal operation during power interruptions not greater than 200msec. Due to the operational application of this device, connection to an external uninterruptible power supply (UPS) may be desirable depending upon customer-specific application requirements. Any specific attempts to comply with the required power interruption time duration shall also consider minimization of in-rush current at power-up. 3.8 Mating Connector Information 3.8.1 MAP-9101-100-x Mating Connectors All wiring harnesses to the unit are supplied and fabricated by the installing agency. PART NUMBER MAP-9101-100-1 MAP-9101-100-2 PART NUMBER MAP-9101-100-1 MAP-9101-100-2 J1 CONNECTOR MATING CONNECTOR CBC25W3F14000 Female Plug or equivalent Size 8 Contact: FCC4102D (x3) (Positronic Industries) 5025W3SCK99AIOX Female Plug with male jackscrews or equivalent Size 8 Contact: D130344 (x3) (ITT Cannon) J2 CONNECTOR (RS-232 SERIAL PORT) MATING CONNECTOR RD9F10JVL0 Female Plug or equivalent (Positronic Industries) DEMA-9S with Female Plug with male jackscrews or equivalent (ITT Cannon) PART NUMBER MAP-9101-100-1 MAP-9101-100-2 Document # 540372, Rev IR, 12/2008 J5 & J6 CONNECTOR (USB PORT #1 & 2) MATING CONNECTOR USB Type A Plug USB Type A Plug Page 17 of 29 DeCrane Aerospace Audio International PART NUMBER MAP-9101-100-1 MAP-9101-100-2 PART NUMBER MAP-9101-100-1 MAP-9101-100-2 MAP-9101-10x-x Installation Manual J7 CONNECTOR (10/100BASE-T ETHERNET PORT) MATING CONNECTOR 95043-2891 (RJ45 Plug) or equivalent (Molex) 95043-2891 (RJ45 Plug) or equivalent (Molex) J8 CONNECTOR (SVGA) MATING CONNECTOR DD15M10JVL0 Male Plug or equivalent (Positronic Industries) DEMA15PK87Male Plug with male jackscrews or equivalent (ITT Cannon) 3.8.2 MAP-9101-101-x Mating Connectors All wiring harnesses to the unit are supplied and fabricated by the installing agency. PART NUMBER MAP-9101-101-1 MAP-9101-101-2 PART NUMBER MAP-9101-101-1 MAP-9101-101-2 J1 CONNECTOR MATING CONNECTOR CBC25W3F14000 Female Plug or equivalent Size 8 Contact: FCC4102D (x3) (Positronic Industries) 5025W3SCK99AIOX Female Plug with male jackscrews or equivalent Size 8 Contact: D130344 (x3) (ITT Cannon) J2 CONNECTOR (RS-232 SERIAL PORT) MATING CONNECTOR RD9F10JVL0 Female Plug or equivalent (Positronic Industries) DEMA-9S with Female Plug with male Jackscrews or equivalent (ITT Cannon) PART NUMBER MAP-9101-101-1 MAP-9101-101-2 J5 CONNECTOR (USB PORT #1) MATING CONNECTOR USB Type A Plug USB Type A Plug PART NUMBER MAP-9101-101-1 MAP-9101-101-2 J6 CONNECTOR (USB PORT #2) MATING CONNECTOR USB Type A Plug USB Type A Plug Document # 540372, Rev IR, 12/2008 Page 18 of 29 DeCrane Aerospace Audio International PART NUMBER MAP-9101-101-1 MAP-9101-101-2 MAP-9101-10x-x Installation Manual J7 CONNECTOR (10/100BASE-T ETHERNET PORT) MATING CONNECTOR 95043-2891 (RJ45 Plug) or equivalent (Molex) 95043-2891 (RJ45 Plug) or equivalent (Molex) J8 CONNECTOR (SVGA) CONNECTOR MATING CONNECTOR MAP-9101-101-1 DD15F10JV30 (Positronic Industries) DD15M10JVL0 (Positronic Industries) MAP-9101-101-2 DEMA15SK87 DEMA15PK87 PART NUMBER PART NUMBER MAP-9101-101-1 MAP-9101-101-2 Document # 540372, Rev IR, 12/2008 J9 CONNECTOR MATING CONNECTOR RD15M10JVL0 or equivalent (Positronic Industries) DEMA-15P with male jackscrews or equivalent (ITT Cannon) Page 19 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 3.9 Pinout Assignment Descriptions 3.9.1 MAP-9101-100-x Pinout Assignment Descriptions All wiring harnesses to the unit shall be supplied and fabricated by the installing agency. J1 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 A1 A2 A3 +28V IN GND RS485A RS485B RS485 Shield ARINC 429 RX A1 ARINC 429 RX B1 ARINC 429 Shield 1 ARINC 429 RX A2 ARINC 429 RX B2 ARINC 429 Shield 2 Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Composite OUT SDI OUT #1 SDI OUT #2 1 2 3 4 5 6 7 8 9 J2 Data Carrier Detect (DCD) Receive Data (RD) Transmit Data (TD) Data Terminal Ready (DTR) Signal Ground Data Set Ready (DSR) Ready To Send (RTS) Clear To Send (CTS) Ring Indicator (RI) 1 2 3 4 J5 & J6 USB +5VDC USB Data USB Data + USB Ground Document # 540372, Rev IR, 12/2008 Page 20 of 29 DeCrane Aerospace Audio International 1 2 3 4 5 6 7 8 MAP-9101-10x-x Installation Manual J7 Ethernet Transmit + Ethernet Transmit – Ethernet Receive + Reserved Reserved Ethernet Receive – Reserved Reserved J8 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Red Video Green Video Blue Video Reserved Ground Red Ground Green Ground Blue Ground Key Sync Ground Reserved Reserved Horizontal Sync Vertical Sync Reserved Document # 540372, Rev IR, 12/2008 Page 21 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 3.9.2 MAP-9101-101-x Pinout Assignment Descriptions All wiring harnesses to the unit shall be supplied and fabricated by the installing agency. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 A1 A2 A3 J1 +28V in GND RS485A RS485B RS485 Shield ARINC 429 RX A1 ARINC 429 RX B1 ARINC 429 SHIELD 1 ARINC 429 RX A2 ARINC 429 RX B2 ARINC 429 SHIELD 2 Briefer Key Output – Active Low Audio Briefer Pause Input– Active Low Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Composite OUT SDI OUT #1 SDI OUT #2 1 2 3 4 5 6 7 8 9 J2 Data Carrier Detect (DCD) Receive Data (RD) Transmit Data (TD) Data Terminal Ready (DTR) Signal Ground Data Set Ready (DSR) Ready To Send (RTS) Clear To Send (CTS) Ring Indicator (RI) 1 2 3 4 J5 & J6 USB +5VDC USB Data USB Data + USB Ground Document # 540372, Rev IR, 12/2008 Page 22 of 29 DeCrane Aerospace Audio International J7 Ethernet Transmit + Ethernet Transmit – Ethernet Receive + Reserved Reserved Ethernet Receive – Reserved Reserved 1 2 3 4 5 6 7 8 J8 Red Video Green Video Blue Video Reserved Ground Red Ground Green Ground Blue Ground Key Sync Ground Reserved Reserved Horizontal Sync Vertical Sync Reserved 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 MAP-9101-10x-x Installation Manual J9 Briefer Audio Out 1+ Briefer Audio Out 1Briefer Audio Out 1 Shield Briefer Audio Out 2+ Briefer Audio Out 2Briefer Audio Out 2 Shield Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Reserved Document # 540372, Rev IR, 12/2008 Page 23 of 29 DeCrane Aerospace Audio International 3.10 MAP-9101-10x-x Installation Manual Post-Installation Test Two (2) externally viewable status LEDs are provided for BIT capabilities. These LEDs are located together, and oriented in a vertical fashion. The LED group location is at the discretion of the designer(s) with consideration given to ease of viewable accessibility. Typical location would include viewable area in proximity to accessible connector interface area(s). • LED 1 (Top-Most) Indication: +28VDC Power Input LED Active Condition: Input power supplied to unit LED Inactive Condition: Input power not supplied to unit LED Color: RED Typical Status: Always illuminated when proper input power is supplied • LED 2 Indication: +5VDC Power Active LED Active Condition: +5VDC power is present LED Inactive Condition: +5VDC is not present. LED Color: GREEN Typical Status: Always illuminated when +5DC power is supplied 4.0 Instructions for Continued Airworthiness Airworthiness Limitations No periodic scheduled maintenance or calibration is required for continued airworthiness of the MAP-9101-10x-x. If the unit fails to perform to specifications, it must be removed and serviced by a qualified service facility. 5.0 General Troubleshooting Procedures Many problems can be isolated with the following general techniques: • Use a voltmeter or similar instrument to verify power to the unit. Confirm +28 VDC power is applied to the proper pins. • Reset by removing power from the unit for at least one minute and reapply power. Document # 540372, Rev IR, 12/2008 Page 24 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual • Recheck all connections to the unit for security. Check all harness runs for possible pinching, wire breaks, etc. Recheck all pinouts for application accuracy. • To check data bus integrity, utilizing a voltmeter, oscilloscope, or other voltage instrument, verify proper input voltage on the data bus pins. Typical measurements with no device(s) on bus transmitting are as follows: A-to-Ground : 4.0 to 4.5 VDC B-to-Ground : 0.1 to 1.0 VDC If any device is transmitting (i.e., holding bus active), then these typical measurements would be reversed for the A-to-Ground and B-to-Ground measurements. This troubleshooting tool can help indicate a data bus lockup. • 6.0 The RS-485 data bus is a bi-directional bus that does not have a ‘bus controller’. The bus uses a differential digital signal that will transmit only when commands are entered via switch selection or other system synchronizing commands. The “A” leg of the bus is HI and the “B” leg LOW. Specifications MAP-9101-10x-x’s Physical Specifications Physical Specifications Housing Weight Dimensions ( l x w x h) Document # 540372, Rev IR, 12/2008 Anodized Aluminum 1.90 lbs / 0.86 kg 5.18" x 6.76" x 2.36" 13.16 cm x 17.17 cm x 5.99 cm Page 25 of 29 DeCrane Aerospace Audio International 7.0 MAP-9101-10x-x Installation Manual Reference Drawings The following diagrams show the unit dimensions, mounting locations, and connector locations for the MAP-9101-101-x. All measurements given with a tolerance of ± 0.5". 7.1 MAP-9101-100-x’s Reference Drawings 7.1.1 Front View 7.1.2 Side View Document # 540372, Rev IR, 12/2008 Page 26 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 7.1.3 Top View 7.1.4 Back View Document # 540372, Rev IR, 12/2008 Page 27 of 29 DeCrane Aerospace Audio International 7.2 MAP-9101-10x-x Installation Manual MAP-9101-101-x’s Reference Drawings 7.2.1 Front View 7.2.2 Side View Document # 540372, Rev IR, 12/2008 Page 28 of 29 DeCrane Aerospace Audio International MAP-9101-10x-x Installation Manual 7.2.3 Top View 7.2.4 Back View Document # 540372, Rev IR, 12/2008 Page 29 of 29