AveoEngineering - Wingtip, Navigation, Position, Strobe, Anti-collision, Landing, Taxi, Recognition LED Lights for aircraft and helicopters - AveoEngineering
Installation Guide for AVEO ENGINEERING models including: AVE-HJPDO-IM Hercules JP LED Light, AVE-HJPDO-IM, Hercules JP LED Light
Hercules JP - PAR 36 Landing or Taxi Light - AveoEngineering
File Info : application/pdf, 14 Pages, 2.32MB
DocumentDocumentINSTALLATION MANUAL
Hercules JP
AVE-HJPDO-IM
© 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.
Installation Manual AVE-HJPDO-IM Issue 01
TABLE OF CONTENTS
PART 0 DOCUMENT ADMINISTRATION .................................................. 3 0.1 DOCUMENT APPROVAL ............................................................................3 0.2 AMENDMENT RECORD PROCEDURE ..............................................................4 0.3 EFFECTED PAGES PROCEDURE ...................................................................4
PART 1 INSTALLATION DATA................................................................. 5 1.1 HERCULES JPTM ...................................................................................5 1.2 OPERATING INSTRUCTIONS ......................................................................6 1.3 INSTALLATION SCHEMATIC / WIRING DIAGRAM ..............................................6 1.4 CONTROL & POWER INPUTS .....................................................................6 1.5 TECHNICAL SPECIFICATION ......................................................................6 1.6 TECHNICAL DRAWING.............................................................................8 1.7 WIRING CHART ....................................................................................9 1.8 OPTIC SIMULATION ............................................................................. 10 1.9 EQUIPMENT LIMITATION ........................................................................ 12 1.10 CARE AND CLEANING OF LIGHTS .............................................................. 12 1.11 TESTING THE LIGHTS BEFORE INSTALLATION ................................................ 12 1.12 CONTINUED AIRWORTHINESS INFORMATION ................................................ 13 1.13 ROHS COMPLIANCE STATEMENT .............................................................. 13 1.14 EU REACH REGULATION (EC) NO. 1907/2006 ......................................... 14
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Part 0 Document Administration
Installation Manual AVE-HJPDO-IM Issue 01
0.1 Document Approval
This document has been established in accordance with an alternative procedure to DOA approved under EASA AP429. This installation manual is applicable for following part numbers:
· Hercules JP Taxi natural
- AVE-HJPDOTW-DS3
· Hercules JP Landing natural - AVE-HJPDOLW-DS3
· Hercules JP Taxi black
- AVE-HJPDOTW-DB3
· Hercules JP Landing black - AVE-HJPDOLW-DB3
· Hercules JP Taxi green
- AVE-HJPDOTW-DG3
· Hercules JP Landing green - AVE-HJPDOLW-DG3
· Hercules JP Taxi red
- AVE-HJPDOTW-DR3
· Hercules JP Landing red
- AVE-HJPDOLW-DR3
· Hercules JP Taxi blue
- AVE-HJPDOTW-DU3
· Hercules JP Landing blue
- AVE-HJPDOLW-DU3
Compiled by:
Petr Jaros Engineer, Aveo Engineering Group, s.r.o.
27 Apr 2022
Approved by:
Georg Hartl Head of DO, Aveo Engineering Group, s.r.o.
27 Apr 2022
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Installation Manual AVE-HJPDO-IM Issue 01
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.
01
Details
Initial Issue
Date of issue
27 Apr 2022
Effected Pages
ALL
Table 01: Record of Document Amendments
0.3 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 EACH raise of issue and the description of respective change will be provided in Table 01 - Details Column.
Changes from the previous issue are shown as follows: a) new text is highlighted with yellow shading: new b) deleted text is shown with yellow shading and a strike through: deleted
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Installation Manual AVE-HJPDO-IM Issue 01
Part 1 Installation data
1.1 Hercules JPTM
HERCULES JP is a high powered PAR36 LED light use in GA and transport category aircraft. It has been designed to be lightweight and with a low power draw to meet the highest requirements of all certified aircraft.
· Hercules JP Taxi natural
- AVE-HJPDOTW-DS3
· Hercules JP Landing natural - AVE-HJPDOLW-DS3
· Hercules JP Taxi black
- AVE-HJPDOTW-DB3
· Hercules JP Landing black - AVE-HJPDOLW-DB3
· Hercules JP Taxi green
- AVE-HJPDOTW-DG3
· Hercules JP Landing green - AVE-HJPDOLW-DG3
· Hercules JP Taxi red
- AVE-HJPDOTW-DR3
· Hercules JP Landing red
- AVE-HJPDOLW-DR3
· Hercules JP Taxi blue
- AVE-HJPDOTW-DU3
· Hercules JP Landing blue
- AVE-HJPDOLW-DU3
Black
Natural
Blue
Green
Red
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Installation Manual AVE-HJPDO-IM Issue 01
1.2 Operating Instructions
When installed on the aircraft, using the aircraft's power (14 or 28 volts), the light will be at its maximum intensity. Operating Voltage range is +9..+36VDC
1.3 Installation Schematic / Wiring Diagram
1.4 Control & Power Inputs
BLUE RED
Ground Power
1.5 Technical Specification
Light characteristics: Voltage range: Voltage protection:
LED quantity: Performance:
Chromaticity: Viewing Angle: Ambient temperature:
Landing Light or Taxi Light / PAR36
+9..+36 VDC
a. Transcient voltage:
2 seconds +80 VDC
b. Under-voltage lockout: +9 VDC, not more
c. Over-voltage lockout: +36 VDC, not less
18 pcs
a. Input current: 5.65 A @ 14 VDC
2.65 A @ 28 VDC
b. Input power:
79.1 W @ 14 VDC
74.3 W @ 28 VDC
Cool White
8° Landing
9° x 20° Taxi
-55°C...+85°C / -67°F...+185°F
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Installation Manual AVE-HJPDO-IM Issue 01
Overheat protection:
Wiring: Weight: Useful life:
Yes (temperature dependent decrement of intensity, see note below) N/A, Connector 2 poles 293 g / 10.33 oz not less than 30.000 aircraft flight hours.
Device RTCA/DO160 (G) qualified:
Environment Temperature / Altitude Temperature Variation Humidity Operational Shock and Crash Safety Vibration Explosive Atmosphere Waterproofness Fluids Susceptibility Sand and dust Fungus Salt Spray Magnetics Effects Power Input Voltage Spike Audio Freq. Conducted Susceptibility Induced Signal Susceptibility Radiated and Conducted Susceptibility Radiated and Conducted Emissions Icing
Section 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 24
Category F2 A C B
U, curves G H R F D F T Z Z A Z ZC TT H
A and C
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1.6 Technical Drawing
Installation Manual AVE-HJPDO-IM Issue 01
*dimensions in [inches] / mm
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Installation Manual AVE-HJPDO-IM Issue 01
1.7 Wiring Chart
Use diagram below defining the wiring size depending on the current and the wire length. Make sure you add up the current for all connected lights. If current is not given, then divide the power by the voltage.
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1.8 Optic Simulation
Taxi Version 51 000 cd
Installation Manual AVE-HJPDO-IM Issue 01
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Landing Version 100 000 cd
Installation Manual AVE-HJPDO-IM Issue 01
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Installation Manual AVE-HJPDO-IM Issue 01
1.9 Equipment Limitation
Hercules JP should only be powered by +9..+36 V DC
1.10 Care and Cleaning of Lights
Aveo Engineering Aviation Lights are factory polished and delivered as ready to install on the aircraft.
If the lights need a deeper cleaning, they should be polished with a quality lamb's wool sheet that is suitable also for deeper polishing. Under no circumstances should any petroleum based product be used to clean the lights.
1.11 Testing the Lights 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 Hercules JP light, and wish to test the function of the light prior to installation on your aircraft, please note the following:
1. Please review the written information that is enclosed in the packaging. Warranty information as well as a cautionary note about power supply removal is enclosed with each package.
2. Remove the light from the package. Note that there is connector with 2 colors:
Blue Ground Red Power
3. Testing of the function of the light can be done with a regular 14VDC or 28VDC power supply (not a battery charger).
Connect the ground wire to blue pole and then connect the power wire to the red pole. The Hercules JP light should start lighting. When installed on the aircraft, using the aircraft's power (14 or 28 VDC), the light will be at its 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..+36 V DC, or a 14 / 28 volt battery be used to test the light. Do not use: Battery chargers, battery back-up power devices, or other bench avionics testing methods to test the aviation light. The light is functional between 9-36 volts. Use of a battery
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Installation Manual AVE-HJPDO-IM Issue 01
charger or other power unit to test the light will void the warranty and may damage the light.
If you have any questions about the installation of the lights, please refer to our web site: www.aveoengineering.com
1.12 Continued Airworthiness Information
Circuit/Wiring Protection
Each Hercules JP light features a Negative Temperature Coefficient (NTC) circuit that limits internal temperatures by attenuating operating current (with a corresponding reduction of brightness) when internal temperatures reach a certain threshold. This proprietary circuitry serves to protect the light itself, and associated aircraft wiring, against a thermal runaway condition.
1.13 RoHS Compliance Statement
Scope
This statement clarifies Aveo Engineering's compliance with European Union Directive 2015/863/EU on the restriction of the use of certain hazardous substances in electrical and electronic equipment ("RoHS") that took effect on June 4, 2015. The RoHS Directive restricts the sale of electronic equipment containing certain hazardous substances in the European Union including:
Cadmium(Cd): 0.01% Mercury: 0.1% Lead(Pb): 0.1% Hexavalent chromium (Cr6+): 0.1% Polybrominated biphenyls (PBB): 0.1 %; Polybrominated diphenyl ethers (PBDE): 0.1 % Bis(2-Ethylhexyl) phthalate (DEHP): 0.1% (added in 2015); Benzyl butyl phthalate (BBP): 0.1% (added in 2015); Dibutyl phthalate (DBP): 0.1% (added in 2015); Diisobutyl phthalate (DIBP): 0.1% (added in 2015)
Compliance
Aveo Engineering certifies that all products sourced from manufacturing facilities comply with the environmental standards set forth by the Directive 2015/863/EU, recast amendment of RoHS Directive 2011/65/EU Article (4), and do not contain any of the above-mentioned, 10 hazardous substances above the specified limits. All products manufactured by Aveo Engineering are RoHS-compliant. With regards to RoHS-2 CE marking, product packaging is labeled attesting conformity if required.
References
Directive 2015/863/EU of the European Parliament and of the Council on the restriction of the use of certain hazardous substances in electrical and electronic equipment.
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Installation Manual AVE-HJPDO-IM Issue 01
1.14 EU REACH Regulation (EC) No. 1907/2006
Aveo Engineering declares that no chemicals are produced and that none of the chemicals used during the production process or needed for the product maintenance or service, is listed on the current European Chemicals Agency's Candidate list of Substances of Very High Concern for Authorization.
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