Installation Manual DOC.NO: AVE-POSW-54G-IM © 2015 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, s.r.o.

Installation Manual PosiStrobe CP Manual Administration 0.1 Table of Contents PART 0 MANUAL ADMINISTRATION DOCUMENT APPROVAL AMENDMENT RECORD PROCEDURE EFFECTED PAGES PROCEDURE DISTRIBUTION LIST OPERATING INSTRUCTIONS INSTALLATION SCHEMATIC / WIRING DIAGRAM CONTROL & POWER INPUT’S: TECHNICAL SPECIFICATION TECHNICAL DRAWING WIRING CHART EQUIPMENT LIMITATION TESTING OF THE LIGHT BEFORE INSTALLATION CARE AND CLEANING OF YOUR AVEO ENGINEERING AVIATION LIGHTS CONTINUED AIRWORTHINESS INFORMATION

Installation Manual PosiStrobe CP 0.2 Document approval This document has been established in accordance with an alternative procedure to DOA approved under EASA AP429. This installation manual is according EASA ETSO authorization EASA.21O.10053449 and applicable for part number AVE-POSW-54G. Petr Jaroš Engineer, Aveo Engineering Group, s.r.o. Georg Hartl Head of DO, Aveo Engineering Group, s.r.o. 0.3 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...

Installation Manual PosiStrobe CP 0.4 Effected Pages Procedure ALL pages affected by ANY raise of issue of this manual will be listed in Table 01 Effected Pages Column. The reason(s) for ALL raise of issue and description of change due to raise of issue will be provided for ALL raises of issue in Table 01 - Details Column. Changes from the previous issue are highlighted by YELLOW HIGHLIGHTING over new content. AND YELLOW HIGHLIGHTING AND CROSSING OUT of deleted content. Example (CROSSING OUT) As stated in 0.3 above; the master copy of this document shall be kept electronically as a read only...

Installation Manual PosiStrobe CP The PosiStrobe CP is a new generation rudder white position and strobe light. It fits almost all the standard rudder mounts of aircraft and also features an optional aluminum adapter mount plate pictured in the installation page. An extremely lightweight, aerodynamic and low-profile design makes this the light of choice for any certified aircraft requiring rear coverage light due to wingtip light coverage zone limits. The PosiStrobe series is the most imitated and copied light by our competitors, but there is ONLY one PosiStrobe, don't be fooled by competitive...

Installation Manual PosiStrobe CP OPERATING INSTRUCTIONS When installed on the aircraft, using the aircraft’s power (14 or 28 volts), the light will be at its maximum intensity. (Meet the requirement of ETSO-C30C, Aircraft Position Light and ETSO- C96A, Anticollision Light Systems) INSTALLATION SCHEMATIC / WIRING DIAGRAM CONTROL & POWER INPUT’s: +VCCP +VCCS GND SYNC positive position/nav power supply line positive strobe power supply line negative common power supply line (ground) strobe synchronization line (Mutually interconnect on all installed AveoFlash lights) TECHNICAL SPECIFICATION Dimensions...

Installation Manual PosiStrobe CP Summary of Environmental Tests Test title Temperature / Altitude Temperature Variation Humidity Operational Shock Vibration Explosive Atmosphere Waterproofness Fluid Susceptibility Sand and dust Fungus Salt Spray Magnetic Effects Power Input Voltage Spike Audio Freq. Conducted Susceptibility Induced Signal Susceptibility Radiated and conducted Susceptibility Radiated and conducted Emissions Lightening Induced Transient Susceptibility Icing Electrostatic Discharge

Installation Manual PosiStrobe CP TECHNICAL DRAWING Figure 2: Dimensions are in millimeters / inches WIRING CHART

Installation Manual PosiStrobe CP EQUIPMENT LIMITATION PosiStrobe CP™ should only be powered by 9-36 Vdc, typically a 12 or 24 volt aircraft battery. This article meets the minimum performance and quality control standards required by the technical standard order ETSO C30c and ETSO C96a. Installation of this article requires separate approval. Deviations This article deviates from the ETSO C30c and ETSO C96a by the usage of newer revisions of the following standards: • • SAE AS 8017 rev. B used instead SAE AS 8017 rev. A SAE AS 8037 rev. A used instead SAE AS 8037 initial release TESTING OF THE...

Installation Manual PosiStrobe CP connected the ground side of the power supply. Connecting the blue wires from each light together (and not to the ground or positive terminals on the battery) should show that the lights are flashing together and indicates the synchronization feature is working properly. When installed on the aircraft, using the aircraft’s power (14 or 28 volts), the lights will be at their maximum intensity. After testing, the light can be installed on the aircraft. IMPORTANT NOTES: Under no circumstances should any power supply other than a 9-32V dc, or a 12/24 volt battery...

Installation Manual PosiStrobe CP Please use tapered headed screws for installation. Spread the tightening forces evenly around the mounting hole. Screw size is a M3, stainless steel recommended. Length depends upon placement location on aircraft tail/rudder. 12. CONTINUED AIRWORTHINESS INFORMATION This product is delivered with EASA Form1 which is for the operator to report any occurrences to Aveo Engineering as the ETSO holder. The form contains the Aveo Engineering telephone number and the occurrence e-mail address ([email protected]). The operator must report immediately as the...

Installation Manual PosiStrobe CP removed and sent to Aveo Engineering for replacement under the Aveo Lifetime Warranty Program. Figure 3: Strobe LEDs Figure 4: Position Light LEDs _______________________________________________________________________________________________________________________ Page 12 of 12