FCC ID: 2AEAK8730L1-5 Aircraft Interface Device

Rosemount Aerospace Inc. 14300 Judicial Road Burnsville, MN 55306-4898 Tel: 952 892 4000 Fax: 952 892 4800 www.utcaerospacesystems.com USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series Document Number D06429976 Revision 06 Controlled electronic approvals are on file and available for review:

Reference Change Order #: SISMN067934 Prepared by Jeffery Paatela 3 NOV 2016 Prepared and Approved by Design Engineer Ryan Kollman Design Engineer NOTE: References to the company in this document will be made as Rosemount Aerospace Inc. (RMTAERO). U.S. Export Classification: EAR: 7E994 Page 1 of 13 THIS DOCUMENT IS THE PROPERTY OF UTC AEROSPACE SYSTEMS. YOU MAY NOT POSSESS, USE, COPY OR DISCLOSE THIS DOCUMENT OR ANY INFORMATION IN IT, FOR ANY PURPOSE, INCLUDING WITHOUT LIMITATION, TO DESIGN, MANUFACTURE OR REPAIR PARTS, OR OBTAIN ANY GOVERNMENT APPROVAL TO DO SO, WITHOUT UTC AEROSPACE SYSTEMSS EXPRESS WRITTEN PERMISSION. NEITHER RECEIPT NOR POSSESSION OF THIS DOCUMENT ALONE, FROM ANY SOURCE, CONSTITUTES SUCH PERMISSION.POSSESSION, USE, COPYING OR DISCLOSURE BY ANYONE WITHOUT UTC AEROSPACE SYSTEMSS EXPRESS WRITTEN PERMISSION IS NOT AUTHORIZED AND MAY RESULT IN CRIMINAL AND/OR CIVIL LIABILITY. Revision History Revision Section Change Description 02 03 All 2.1 Initial release Updated model information 3.3.4 Updated approval information CO Number SISMN059487 SISMN061700 2.5 Updated antenna recommendations with gain limits 04 3.3.3 Added instructions for retrieving R&TTE DoC SISMN064413 All 2.2 2.5 05 Formatting updates Added statement on device mounting Updated antenna info Table 2 Updated radio information 06 2.5 Updated antenna info SISMN066356 SISMN067934 USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 2 of 13 D06429976 Revision 06 Table of Contents 1 ABOUT THIS DOCUMENT 5 1.1 1.2 1.3 1.4 Purpose .................................................................................................................................................................. 5 Applicable Documents ............................................................................................................................................ 5 Abbreviations and Acronyms .................................................................................................................................. 6 Terms and Definitions ............................................................................................................................................. 7 2 AIRCRAFT INTERFACE DEVICE (AID) 8 2.1 2.2 2.3 2.4 2.5 AID Overview .......................................................................................................................................................... 8 Mechanical Interfaces ............................................................................................................................................. 9 Electrical Interfaces................................................................................................................................................. 9 Power Requirements ............................................................................................................................................ 10 Wireless Antenna Recommendations ................................................................................................................... 10 3 CERTIFICATIONS 11 3.1 3.2 3.3 DO-160 ................................................................................................................................................................. 11 DO-254 and DO-178C .......................................................................................................................................... 12 Wireless Regulatory Compliance And Industry Certification ................................................................................. 12 FCC ............................................................................................................................................................. 12 Industry Canada........................................................................................................................................... 12 3.3.3 CE ................................................................................................................................................................ 13 3.3.4 PTCRB ......................................................................................................................................................... 13 3.3.1 3.3.2 USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 3 of 13 D06429976 Revision 06 List of Tables Table 1: Applicable Documents .................................................................................................................................. 5 Table 2: Model Configurations .................................................................................................................................... 9 Table 3: Power Supply.............................................................................................................................................. 10 List of Figures Figure 1: 8730L Series AID ........................................................................................................................................ 8 USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 4 of 13 D06429976 Revision 06 1 ABOUT THIS DOCUMENT The 8730L Series Aircraft Interface Device (AID) provides an interface between various aircraft avionics systems and nontraditional avionics equipment such as Electronic Flight Bags (EFB), In-Flight Entertainment (IFE) Systems, broadband communications systems (cellular, Wi-Fi) or onboard network servers; providing both a hardware and software firewall protecting the critical aircraft systems against any adverse effect from the interfacing nontraditional equipment. The AID incorporates a variety of industry standard interfaces; including Ethernet, ARINC 429, ARINC 717, RS-

232, RS-422/485, USB, and Discrete inputs/outputs. The AID also provides a removable mass data storage device enabling local data storage to hosted applications. An optional embedded cellular or Wi-Fi radio using remote antennas is available. The AID incorporates a Linux operating system running on a PowerPC based micro-processor utilizing DDR3 memory. Software supports avionics interface data reception, transmission, concentration, and recording. Access to this data is provided to locally hosted or remote equipment applications via a built-in ARINC 834 server. 1.1 Purpose This Users Manual provides an overall guide to the 8730L AID. 1.2 Applicable Documents The following specifications, drawings, and publications, of latest issue when not specified, form a part of this document to the extent specified herein. Table 1: Applicable Documents Rosemount Aerospace Inc. Document No. Document Title 8730L1 Specification Control Drawing for the AID Industry Standards Document No. Document Title ARINC 429 ARINC 664 ARINC 717 Aircraft Mark 33 Digital Information Transfer System Aircraft Data Network Flight Data Acquisition and Recording System ANSI/TIA/EIA-232-B Interface between data terminal equipment and data circuit terminating equipment ANSI/TIA/EIA-422-B Electrical Characteristics of balanced digital interface circuits ANSI/TIA/EIA-485-B Electrical characteristics of generators and receivers for use in balanced digital multiport systems USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 5 of 13 D06429976 Revision 06 1.3 Abbreviations and Acronyms AID Aircraft Interface Device ARINC Aeronautical Radio Incorporated DDR3 Double Data Rate type 3 Synchronous Dynamic Random Access Memory DoC EFB ICD IFE lbs SIM USB VDC Declaration of Conformity Electronic Flight Bag Interface Control Document In-Flight Entertainment pounds Subscriber Identity Module Universal Serial Bus Voltage - direct current USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 6 of 13 D06429976 Revision 06 1.4 Terms and Definitions Qualification Demonstrates that the implementation meets the requirements and is suitable for operation in the airplane. Shall Expresses a binding requirement. Should/May Expresses a recommended or allowed action. Validation Identifies that the requirements for a product are sufficiently correct and complete. Verification Identifies that the implementation has been evaluated to determine that all design requirements have been met. Will Expresses a declaration of intent. USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 7 of 13 D06429976 Revision 06 2 AIRCRAFT INTERFACE DEVICE (AID) 2.1 AID Overview The 8730L AID has the following external features as shown in Figure 1:

J1, 37-pin D-sub connector providing interfaces to the following: Aircraft +28V power, Chassis Ground, ARINC 664 Ethernet 10/100 Base T, ARINC 717 Harvard Bi-Phase receiver, ARINC 429 Bipolar receivers, ARINC 429 Bipolar transmitters, RS-232, and discrete inputs J2, 37-pin D-sub connector providing interfaces to the following: ARINC 664 Ethernet 10/100/1000 Base T, ARINC 429 receivers, ARINC 429/717 Bipolar receiver, ARINC 429 Bipolar transmitters, and discrete inputs J3, 50-pin D-sub connector providing interfaces to the following: ARINC 664 Ethernet 10/100/1000 Base T, ARINC 429 receivers, ARINC 429/717 Bipolar receiver, ARINC 429 Bipolar transmitters, RS-422/485, USB, discrete inputs, and discrete outputs Access Cover for removable CFast Storage device and SIM card (SIM card supports cellular capability). Three (3) external antenna connectors (for Wi-Fi or cellular capability) Mounting provisions Weight: 2.5 lbs max for base unit, add 0.2 lbs for each cellular and/or Wi-Fi, add 0.1 lbs for CFast, add 0.15 lbs for 8730L1-5 model. Mounting Provisions Wi-Fi antenna cable connector Electrical Connectors Overall View Cellular antenna cable connectors SIM and CFast Access Cover Front View Back View Figure 1: 8730L Series AID USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 8 of 13 D06429976 Revision 06 There are five defined model configurations of the AID, each supporting different wireless needs. Model configuration is accomplished during factory build through the installation radio module internal to the AID enclosure. NOTE: The radios are not accessible and should not be removed by the User. Table 2: Model Configurations Manufacturer Model Wireless Communications UTC Aerospace Systems 8730L1-1 No Wireless (Base model) Radio Module None UTC Aerospace Systems 8730L1-2 Cellular

(LTE in North America; 2G/3G elsewhere) Sierra Wireless MC7354 UTC Aerospace Systems 8730L1-3 Cellular

(LTE in Europe, Middle East, Africa; 2G/3G elsewhere) Sierra Wireless MC7304 UTC Aerospace Systems 8730L1-4 Wi-Fi (802.11 a/b/g/n) UTC Aerospace Systems 8730L1-5 Cellular (LTE in North America and EMEA) and Wi-Fi

(802.11 b/g/n) Advantech EWM-W158F Sierra Wireless MC7455 and SparkLAN WUBA-

171GN A SIM card can be installed or removed through the Access Cover on the back of the AID. The AID has the capability to allow the user to install a CFast card; a solid-state non-volatile data storage device. The CFast card is a separate LRU (not part of the standard AID configuration) and is accessible through the Access Cover on the back of the AID for easy removal or insertion. CFast model number 8732D1-1 is available from UTC Aerospace Systems and has been qualified to operate within the AID operating environment. NOTE: The CFast and SIM card are not considered to be hot-pluggable. Ensure the AID is powered off prior to inserting or removing these devices from the AID. NOTE:

If the Access Cover on the back of the AID is removed for any reason, reinstall the cover prior to using the AID in its intended function. 2.2 Mechanical Interfaces The AID provides mounting provisions (or holes) on the sides of the unit as shown in Figure 1. The 8730L AID is mounted in the aircraft as a fixed device; it is not movable by the user. The mounting provisions are designed to interface with a simple U-bracket mounting provision with holes for screws or captive fasteners on the two sides. Two L-brackets are another potentially simple solution, one on each side. The AID is cooled by natural convection and by conduction through the mounting provisions. Sufficient clearance must be provided to permit air flow in the installation. The installation should also be designed to provide a path for heat to flow through the mounting bracket into the structure. 2.3 Electrical Interfaces The AID electrical interfaces are made through one 37-pin D-sub pins, (J1), one 37-pin D-sub socket, (J2), and one 50-pin D-sub pins (J3). The Wi-Fi antenna cable connection and the cellular antenna cable connections are made with SMA connectors. USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 9 of 13 D06429976 Revision 06 The AID provides a chassis ground electrical bonding path through a metal surface contact around its mounting holes. In addition, the AID bonds its connector shells to local chassis ground and provides a chassis ground pin in connector J1. One or more of these points should be connected to the aircraft chassis ground through a low impedance connection path. 2.4 Power Requirements The AID requires 28 VDC aircraft power as defined in Table 3. Circuit breakers should be chosen based on max current as shown. Table 3: Power Supply Power Characteristic Value Voltage Current (typical) Current (max continuous)

+28 VDC nominal (18 VDC 32.2 VDC range) 0.71A @ 28VDC 0.9A @ 28VDC Inrush Current (max) 6A @ 28VDC (<100ms) Power Consumption (typical idle) Power Consumption (max continuous) 20W 25W 2.5 Wireless Antenna Recommendations Attached cellular antennas should be Laird part number DBA6927C1-xxxxx. Alternate antennas with similar performance may be suitable. Gain should not exceed 0.5 dBi at 698-960 MHz and 2.2 dBi at 1710-2700 MHz. Cellular antennas must be connected through a coaxial cable of at least 20cm length. It is recommended that the coaxial cable attenuation characteristic is similar or better than Times Microwave Systems Maxgain-200. Attached Wi-Fi antenna should be Laird part number MAF94271. Alternate antennas with similar performance may be suitable. Gain should not exceed 2.1 dBi at 2.45 GHz, 2.4 dBi at 4.9 GHz, 2.6 dBi at 5.25 GHz, and 3.4 dBi at 5.875 GHz. The Wi-Fi antenna can be placed directly on the AID, but remote locations through a high performance coaxial cable may offer improved performance depending on location. Maxgain-200 or better cabling is recommended. Guidelines for placement of the antennas:

Antennas should be located in an area with apertures to allow transmission that is, not a fully enclosed metal structure. Maximizing spatial and orthogonal diversity is desired. Locate the antennas not near one another and rotated 90 relative to one another. Strive for at least 1 foot away from metal structure. If a mounting bracket is used to retain the radiating element portion of the antenna(s), it should be non-

metallic and RF-transparent. Avoid carbon based dyes or paint that can hinder RF transmission. Install antennas in a location where 20 cm is normally maintained between the transmitters radiating structures and the body of nearby persons. USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 10 of 13 D06429976 Revision 06 3 CERTIFICATIONS 3.1 DO-160 The 8730L AID has been certified to operate within the following environmental conditions. Test Description Temperature and Altitude DO-160G Section Test Category 4.5 4.5 4.5 4.5 4.5 4.5 Operating Low Temp., -40C, Modified Cat B2 Operating High Temp., +55C, Modified Cat B2 Short-Time Operating Low Temp., -40C, Modified Cat B2 Short-Time Operating High Temp., +70C, Cat B2 Ground Survival Low Temp., -55C, Cat B2 Ground Survival High Temp., +85C, Cat B2 4.6.1 Steady State Altitude, 25,000 ft. Cat B2 4.6.2 Decompression, 51,000 ft. Cat A1 4.6.3 Overpressure, 170kPa (-15,000 ft.), Cat A1 Temperature Variation Humidity Operational Shocks, Crash Safety Vibration Fluid Susceptibility Sand and Dust Fungus Resistance Magnetic Effect Power Input Voltage Spike Power Supply Audio Frequency Conducted Susceptibility Induced Signal Susceptibility RF Conducted Susceptibility (10kHz 400MHz) RF Radiated Susceptibility (100MHz 8GHz) RF Conducted Emissions (150kHz 152MHz) RF Radiated Emissions (100MHz 6GHz) Lightning Indirect Effects Electrostatic Discharge USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series 5 6 7 8 11 12 13 15 16 17 18 19 20 20 21 21 22 25 Category B Category A Category B 6g 11ms Shock Cat B 20g 11ms Crash Safety Impulse Cat B 20g Crash Safety Sustained Cat B Category S, Curve C Category U, Curve G Category F, as limited to a subset of fluids Category S Category F Category Z, less than 0.3 m ZXX A Z ZC T T M M A1C1X A Page 11 of 13 D06429976 Revision 06 UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 3.2 DO-254 and DO-178C The AID is developed in accordance with Design Assurance Level E per RTCA/DO-254 and DO-178C. 3.3 Wireless Regulatory Compliance And Industry Certification The AID has the following regulatory and industry approvals. 3.3.1 FCC This device complies with Part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. Consult the SCD 8730L1 for model-specific FCC ID numbers. 3.3.2 Industry Canada This device complies with Industry Canada licence-exempt RSS standard(s). Operation is subject to the following two conditions:

(1) this device may not cause interference, and

(2) this device must accept any interference, including interference that may cause undesired operation of the device. Le prsent appareil est conforme aux CNR d'Industrie Canada applicables aux appareils radio exempts de licence. L'exploitation est autorise aux deux conditions suivantes :

(1) l'appareil ne doit pas produire de brouillage, et

(2) l'utilisateur de l'appareil doit accepter tout brouillage radiolectrique subi, mme si le brouillage est susceptible d'en compromettre le fonctionnement. Under Industry Canada regulations, this radio transmitter may only operate using an antenna of a type and maximum (or lesser) gain approved for the transmitter by Industry Canada. To reduce potential radio interference to other users, the antenna type and its gain should be so chosen that the equivalent isotropically radiated power

(e.i.r.p.) is not more than that necessary for successful communication. Conformment la rglementation d'Industrie Canada, le prsent metteur radio peut fonctionner avec une antenne d'un type et d'un gain maximal (ou infrieur) approuv pour l'metteur par Industrie Canada. Dans le but de rduire les risques de brouillage radiolectrique l'intention des autres utilisateurs, il faut choisir le type d'antenne et son gain de sorte que la puissance isotrope rayonne quivalente (p.i.r.e.) ne dpasse pas l'intensit ncessaire l'tablissement d'une communication satisfaisante. Consult the SCD 8730L1 for model-specific IC ID numbers. USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 12 of 13 D06429976 Revision 06 3.3.3 CE This equipment is intended to be used as an Aircraft Interface Device which includes wireless communication. Hereby, Rosemount Aerospace Inc., declares that this device is in compliance with the essential requirements and other relevant provisions of Directive 1999/5/EC. 0682 A complete Declaration of Conformity (DoC) is available from UTC Aerospace Systems upon request. Please contact your Customer Service Representative. 3.3.4 PTCRB The 8730L1-2 AID is PTCRB certified. USER MANUAL Aircraft Interface Device Rosemount Aerospace Inc. Model 8730L Series UTC AEROSPACE SYSTEMS PROPRIETARY SUBJECT TO THE RESTRICTION ON THE TITLE OR COVER PAGE. U.S. Export Classification: EAR: 7E994 Page 13 of 13 D06429976 Revision 06