© 2017 Aveo Engineering Group, s.r.o. All rights reserved. The information contained within this document must not be disclosed, copied or reproduced in whole or in part without prior written permission from Aveo Engineering Group, s.r.o. Distribution of this document shall only be as stated in Table 02 unless otherwise agreed by Aveo Engineering Group,

Installation Manual AVE-RBCRW-001-IM Issue 05 DOCUMENT ADMINISTRATION DOCUMENT APPROVAL AMENDMENT RECORD PROCEDURE EFFECTED PAGES PROCEDURE INSTALLATION DATA REDBARON COMBO HISL™ OPERATING INSTRUCTIONS INSTALLATION SCHEMATIC / WIRING DIAGRAM CONTROL & POWER INPUTS TECHNICAL SPECIFICATION TECHNICAL DRAWING WIRING CHART EQUIPMENT LIMITATION TESTING THE LIGHTS BEFORE INSTALLATION CARE AND CLEANING OF LIGHTS CONTINUED AIRWORTHINESS INFORMATION

Installation Manual AVE-RBCRW-001-IM Issue 05 Document Administration Document Approval This document has been established in accordance with an alternative procedure to DOA approved under EASA AP429. This installation manual relates to EASA ETSO Authorization [EASA.210.10053491] and is applicable for the following part number: RedBaron Combo HISL 15 August 2017 Petr Jaroš Engineer, Aveo Engineering Group, s.r.o. 15 August 2017 Georg Hartl Head of DO, Aveo Engineering Group, s.r.o.

Installation Manual AVE-RBCRW-001-IM Issue 05 0.2 Amendment Record Procedure The master copy of this document shall be kept electronically as a read only document under the control of Aveo Engineering Group, s.r.o. as Master Copy. ALL amendments to this manual will initiate a raise of issue. The original issue will be identified by “01”, and subsequent issues will be numbered sequentially from 02 to 99 in Table 01 - Issue No. column. ALL issues of this document will be approved by Head of DO. Issue No. Effected pages Initial Issue Removing allowed failing LED Addition of FAA required statements...

Installation Manual AVE-RBCRW-001-IM Issue 05 Installation data 1.1 RedBaron Combo HISL™ The incredible and unmatched performance of the RedBaron Combo dual-color LED red and white anti-collision light makes it not only the world's brightest but also the leader in all DO-160 environmental standards compliance. Main Features: • • • • Selectable modes of two switches, white or red (RedBaron Combo HISL can be only operated in EITHER RED or WHITE MODE, not simultaneously or it will damage the unit) Unmatched strobe intensity in the industry Incorporates the world-leading lumen output LED technology...

Installation Manual AVE-RBCRW-001-IM Issue 05 1.3 Installation Schematic / Wiring Diagram Recomended interconnection schematic for RedBaron Combo HISL AVE-RBCRW-001 HISL Light Red Strobe Switch Red Strobe Power Section +Ucc (Red) Main Power Leads 18-36V DC White Strobe Power Section +Ucc (Yellow) White Strobe Switch Power Return (Black) Common Return Wire Positive Power Wire +Ucc Shielding Junctions HISL Light Copter Airframe Wire Sync wire (Blue) Red Strobe Power Section +Ucc (Red) White Strobe Switch White Strobe Power Section +Ucc (Yellow) Power Return (Black) Note: If synchronization is not...

Installation Manual AVE-RBCRW-001-IM Issue 05 1.5 Technical Specification Dimensions: Operating Voltage Range: Operating temperature: Strobe branch (white), input power: ▪ Strobe branch (red), input power: 28 V / 2.5 A : LEDs - maximum drive current: - white LEDs Repetition Flash Rate of Strobe: Over-voltage protection: Reverse polarity protection: Recommended size of mounting screw: Torque requirement for screw M5x70mm: Meets and exceeds requirements of: •

Installation Manual AVE-RBCRW-001-IM Issue 05 Dimensions in [inches] / millimeters _______________________________________________________________________________________________________________________ Page 8 of 16

Installation Manual AVE-RBCRW-001-IM Issue 05

Installation Manual AVE-RBCRW-001-IM Issue 05

Installation Manual AVE-RBCRW-001-IM Issue 05 1.8 Equipment Limitation The RedBaron Combo HISL™ light should only be powered by 18-36 V DC, typically by a 24 volt aircraft battery. This article meets the minimum performance and quality control standards required by the technical standard order ETSO C96a. Installation of this article requires separate approval. Deviations This article deviates from the ETSO C96a by the usage of newer revisions of the following standards: • 1.9 Testing the Lights before Installation All Aveo Aviation lights undergo rigorous testing prior to being released from...

Installation Manual AVE-RBCRW-001-IM Issue 05 When installed on the aircraft and using the aircraft’s power (28 volts), the light will be at its maximum intensity. If the tests are successfully completed, the light can be installed on the aircraft. IMPORTANT NOTES: 1. Under no circumstances should any power supply other than a 18-36 V DC, or a 24 volt battery be used to test the lights. Do not use: Battery chargers, battery back-up power devices, or other bench avionics testing methods to test the aviation lights. The lights are functional between 18 and 36 volts. Use of a battery charger or...

Installation Manual AVE-RBCRW-001-IM Issue 05 Continued Airworthiness Information From the webpage http://www.aveoengineering.com/ the customer can download the form FAVE-001A which shall be used by operator for reporting any occurrences to the Aveo Engineering as the ETSO holder. The form contains the Aveo Engineering telephone number and the occurrence email address ([email protected]). The operator shall report immediately as the ETSO holder is obliged to report occurrences having potential to lead to an unsafe condition within 72 hours. a. Circuit/Wiring Protection Each RedBaron...

Installation Manual AVE-RBCRW-001-IM Issue 05 Figure 1: Top White LEDs Figure 2: Top Red LEDs _______________________________________________________________________________________________________________________ Page 14 of 16

Installation Manual AVE-RBCRW-001-IM Issue 05 Figure 3: Middle White LEDs Figure 4: Middle Red LEDs