Panel-mounted level 2els class 1 extended squitter transponder (48 pages)
Summary of Contents for Appareo Systems Stratus ES
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Revision 2.1 This document and the information APPAREO SYSTEMS, LLC contained herein are the property of Appareo Systems, LLC and are FARGO, NORTH DAKOTA 58102 confidential. They may not be disseminated or redistributed without the written Stratus ES/ESG Installation Instructions...
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Unauthorized replication of this guide is prohibited. Appareo, Appareo Systems, Stratus ES, Stratus ESG, and the Appareo and Stratus logos are either registered trademarks or trademarks of Appareo Systems, LLC. All other trademarks and registered trademarks are the sole property of their respective owners.
Rev. 2.1 Last Revised: June 22, 2017 Warnings The pilot must read the Stratus ES/ESG Pilot’s Guide (600890-000049) before their first flight. Squawk codes 7500 (hijacking), 7600 (radio failure), and 7700 (emergency) are reserved for emergencies. There may be other reserved codes, depending on the region you are flying in.
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600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Record of Revision Revision Revision Change Description Inserted By Number Date Initial Release 5/29/15 CM 10281 1/06/16 CM 10323 1/13/16 CM 10633 2/09/16 CM 11303 5/10/16 CM 11511 6/08/16 Removed warranty;...
A periodic message that provides position, velocity, and time. Extended Squitter Part of the marketing name for Stratus ES. Extended Squitter Part of the marketing name for Stratus ESG. and GPS Agency of the United States Department of Transportation with...
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600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Megahertz 1,000,000 hertz. Satellite-Based System of satellites that augments existing satellite systems and SBAS Augmentation provides increased position accuracy. System Supplemental Type Certificate issued when an applicant has received FAA Type Certificate approval to modify an aircraft from its original design.
Stratus ES and Stratus ESG respond to legacy Mode A/C interrogations and Mode S interrogations from both ground radar and airborne collision avoidance systems. To support the ADS-B Out function, Stratus ESG also contains a Class Beta 1 GPS/WAAS receiver. Stratus ES receives GPS information from approved GPS position sources.
This non-TSO function does not interfere with Stratus ES/ESG’s compliance with the requirements of the TSOs listed in Section 1.2. 1.5. Environmental qualifications Stratus ES/ESG is tested to DO-160G. The Stratus ES/ESG Environmental Qualification form is found in Appendix A of this document. 1.6. Criticality level Software level determination is based on the Functional Hazard Assessment (FHA) and Preliminary System Safety Assessment (PSSA).
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 1.7. Embedded Hardware and Software The embedded hardware and software information listed below is current as of the time of publication of this document. Revision Description Part number...
0.5 A at 14 VDC 8 W Typical Power Input 59.5 W Max Table 8: Power requirements 1.9. Required tools The following tools are needed for installation of Stratus ES/ESG. Tool Part Number Used For Securing locking mechanism 3/32” hex driver through the faceplate...
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 1.10. Required hardware The following parts are required for the installation of Stratus ES/ESG. Supplied parts: Appareo Part Commercial Part Item Quantity Number Number Backplate 153510-000015 Stratus ES Transponder...
Avidyne IFD440 and IFD540 with software version 10.0.3.0 or later Connect Stratus ES to an open RS232 serial port (out) on the GPS position source and use the GPS position source to configure the port to use the ADSB+ protocol.
Regional Aircraft Certification Office (ACO). Transponder antenna Stratus ES/ESG requires a passive antenna with the specifications of TSO-C74() or TSO-C66(). The following antenna is an example of an antenna that meets these specifications. The installation is not limited to this antenna.
Stratus ES/ESG may not be acceptable for installation on all aircraft makes and models. Cooling air Stratus ES/ESG does not require an air cooling system, nor does it have a duct to port air for a system. Do not install Stratus ES/ESG near a heat source. An alternate method of cooling is required if the unit must be installed near a heat source.
2.6. Circuit protective device marking If Stratus ES/ESG is replacing an existing transponder, ensure that the circuit protective device is sufficiently marked. If Status ES/ESG is a new installation, ensure that the labeling is in accordance with AC 43.13- 2B, Chapter 2, Section 207, Sub-Section f., Paragraph (4).
Stratus ES/ESG wiring diagrams. NOTE: Previously installed equipment may have additional components inline that could impede the function of Stratus ES/ESG. Removal of those components is required. CAUTION: Remove aircraft power before wiring to avoid damaging the device.
Refer to the wiring diagrams in Stratus ES/ESG Installation and Wiring Drawings (601837- 000024) to complete wiring. The sections below describe the function of each pin in more detail. Power Stratus ES/ESG requires a 5 amp circuit breaker. A minimum of 2 ground pins should be tied. Pin # Pin Name...
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 GPS Position Source (Stratus ES only) Stratus ES requires connection to an external GPS source. The RS232 output from the GPS source requires configuration. Pin # Pin Name...
NOTE: Only one suppression may be connected. Lighting Stratus ES/ESG can be connected to the aircraft lighting bus to control the brightness with a panel control. To connect to the lighting bus, connect one of the following pins, depending if the aircraft runs at 28V or 14V.
3.3. Connecting antennas and position source Stratus ES requires input from a GPS position source, and Stratus ESG requires a GPS antenna. Both systems require a transponder antenna and altitude encoder. Use the wiring information specified in Section 1.11 to connect them to the back of the transponder, following the Stratus ES/ESG Installation and Wiring Drawings (601837-000024).
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Sometimes, a textual or non-numerical input will be required. If this is the case, press the number that is associated with the letter group you want to input, according to the graphic on the screen.
Select the measurement that most closely represents the distance from the lateral center of the aircraft to the GPS antenna to the nearest two meters. NOTE: If using Stratus ES, confirm that these offsets are not already applied to the GPS position source settings.
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 4.18. SBAS service provider (Stratus ESG only) Select the SBAS service provider: WAAS (North America) EGNOS (Europe) MSAS (Japan) GAGAN (India) SDCM (Russia) ...
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BIT failures have been resolved, press ENT to clear all codes. Failure BIT Failure Corrective Action Position GPS Failure Verify that the connection between Stratus ES and (Stratus ES only) the GPS position source is secure. Transmitter Contact Appareo Display...
Final installation checks for Stratus ES/ESG are the responsibility of the installer. The installer must ensure that Stratus ES/ESG is installed on an aircraft that coincides with the approval given within the testing performed for the TSOs held by this device:TSO-C112e, TSO-C145d (Stratus ESG only), and TSO-C166b.
NOTE: Depending on the installation, the functional tests for the following discrete inputs are optional. 1. Turn off Stratus ES/ESG and enter into configuration mode (while holding the FUNC key, press and release the PWR key). 2. Press FUNC or the arrow keys to advance to the external input diagnostics screen.
Using the cockpit intercom, verify interference-free communications between the crew while monitoring the effects of Stratus ES/ESG. (ii) Cabin paging Verify that cabin paging is functioning clearly while monitoring the effects of Stratus ES/ESG. VHF communications Set VHF communications radios to multiple frequencies and monitor the effects of Stratus ES/ESG while transmitting and receiving.
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108.000 MHZ 108.100 MHZ (ii) DME Verify the operation of each DME while monitoring the effects of Stratus ES/ESG. The same frequencies used for VOR and ILS testing may be used for this test. (iii) Marker Beacon Verify the operation of each Marker Beacon Receiver while monitoring the effects of Stratus ES/ESG.
Verify the function of the EGPWS and Terrain Display (if equipped) while monitoring the effects of Stratus ES/ESG. (ii) TCAS Verify the function of the TCAS while monitoring the effects of Stratus ES/ESG. Self-test and monitoring targets of opportunity should both be evaluated. (iii) Weather radar Verify the function of each weather radar system while monitoring the effects of Stratus ES/ESG.
EMI test is complete and passes. It is recommended that a flight test be conducted after installation to verify proper operation and installation of Stratus ES/ESG. A compliance report can be obtained by emailing 9-AWA-AFS- 300-ADSB-AvionicsCheck@faa.gov with the aircraft information. This method is controlled by the FAA and may be subject to change.
Rev. 2.1 Last Revised: June 22, 2017 6.2. Event indicators When certain events occur, an indicator will appear on your Stratus ES/ESG display. The table below describes each indicator’s meaning. Indicator Meaning ADS-B transmission contains GPS position information with a radius of containment under 1 nautical mile.
Power (PWR) key The PWR key is used to power Stratus ES/ESG on and off. When Stratus ES/ESG is powered on, it retains the last used squawk code and operation mode. Page 37 of 44...
While on any screen that the squawk code is shown, press the appropriate number keys (0 through 7) to enter the squawk code. The new digits will be shown on the display screen. Five seconds after the fourth digit is entered, Stratus ES/ESG will automatically save the entered squawk code.
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 7. Troubleshooting Use the table below to troubleshoot possible problems with Stratus ES/ESG. For a full list of BIT failures, see Section 4.19.9. Problem Troubleshooting Steps GPS information is not being...
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11 VDC and 36 VDC. The altitude displayed is incorrect Enter into configuration mode on Stratus ES/ESG and verify that the altitude source is set as the currently used altitude source. If the altitude source is a serial connection, verify that the correct encoding option was selected.
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600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 The screen displays a Built in Test The Stratus ES/ESG screen might display a warning (BIT) failure message with the instructions below. Below is guidance regarding how to assess the failure: The display screen will display a ...
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600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Appendix A Nomenclature: Stratus ES / Stratus ESG Transponder Part number: 153510-000069 / 153510-000017 TSO number: TSO-C112e, TSO-C145d (Stratus ESG only), TSO-C166b Manufacturer’s specification and/or other applicable specification: 608080-000021...
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600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Vibration Equipment tested to Category S. 8.5.1 Group 3 during, 1 after Equipment identified as Category X, no test Explosion Proofness performed. Equipment identified as Category X, no test Waterproofness 10.0...
600840-000031 Stratus ES/ESG Installation Instructions Rev. 2.1 Last Revised: June 22, 2017 Equipment identified as Category X, no test Icing 24.0 performed. Equipment tested to Category A. Electrostatic Discharge 25.0 No group test during, 2 after Flammability testing was performed utilizing the Fire, Flammability 26.0...
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