INSTALLATION MANUAL © 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 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 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 21O.10055101 and applicable for part number AVE-POSW-74G-401, -402 and -403. Peter Nezval 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 to this manual...

Installation Manual 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 document under...

Installation Manual Pegatron™ is a LED position light assembly E TSO Compliant white position lights low drag and low profile designed for aircraft tail position. This powerful LED lighting system features easy installation, a fail save system, unbreakable construction, waterproof and high candela output. List of the major components (by part number) that make up the equipment complying with the standards prescribed in ETSO. • P/N: AVE-POSW-74G-401 (White) P/N: AVE-POSW-74G-402 (White) P/N: AVE-POSW-74G-403 (White) Figure 01: Features of Pegatron OPERATING INSTRUCTIONS When installed on the aircraft,...

Installation Manual CONTROL & POWER INPUT’s: POSITIVE POLE GND POLE Positive POS/NAV power supply line Negative common power supply line (ground) TECHNICAL SPECIFICATION Dimensions (mm): Dimensions (inches): Weight (g): Operating voltage: Primary input voltage: Over-voltage protection: Input current at 28V: Reverse polarity protection: Over-Voltage shut down: Operating temperature: Over-Temperature protection: Output power Waterproof: Vibration-proof: Shock-proof: Dust-proof:

Installation Manual TECHNICAL DRAWING Dimensions are in millimeters / [inches] _______________________________________________________________________________________________________________________ Page 7 of 12

Installation Manual Dimensions are in millimeters / [inches] Dimensions are in millimeters / [inches] _______________________________________________________________________________________________________________________ Page 8 of 12

Installation Manual WIRING CHART EQUIPMENT LIMITATION Pegatron™ should only be powered by 18-36 Vdc, typically a 24 volt aircraft battery. TESTING OF THE LIGHT BEFORE INSTALLATION All Aveo Aviation lights undergo rigorous testing prior to being released from our engineering manufacturing department. This testing involves a burn-in time as well as other function testing. No light is released for sale without undergoing this extensive operational testing. When you receive the Pegatron™ light, and wish to test the function of the light prior to installation on your aircraft, please note the following:...

Installation Manual 3. Testing the function of the light can be done with a regular 24V/5A dc power supply (no battery chargers). Connect the black wire to the ground (negative) leads of a power supply, then connect the yellow wire to the positive (+) leads on the power supply. The position light should start lighting. When installed on the aircraft, using the aircraft’s power (28 volts), the light will be at its maximum intensity. After testing, the light can be installed on the aircraft. IMPORTANT NOTES: 1. Under no circumstances should any power supply other than a 18-36 Vdc, or a 24 volt...

Installation Manual Spread the tightening forces evenly around the mounting hole. Stainless steel screw is recommended. Length depends upon placement location on aircraft. 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 ETSO holder must report occurrences having a potential for an unsafe condition within...

Installation Manual Figure 2: Position LEDs – all LEDs (12 pcs)