AVEO ENGINEERING AVE-HJPDO-IM Hercules JP LED Light Installation Guide
- June 4, 2024
- AVEO ENGINEERING
Table of Contents
AVEO ENGINEERING AVE-HJPDO-IM Hercules JP LED Light
© 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.
Document Administration
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: 27 Apr 2022
Petr Jaros
Engineer, Aveo Engineering Group, s.r.o.
Approved by: 27 Apr 2022
Georg Hartl
Head of DO, Aveo Engineering Group, s.r.o.
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. | Details | Date of issue | Effected Pages |
---|---|---|---|
01 | Initial Issue | 27 Apr 2022 | ALL |
Table 01: Record of Document Amendments
Effected Pages Procedure
ALL pages affected by ANY raise of issue of this manual will be listed in
Table
- 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
Installation data
Hercules JP™
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
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
Installation Schematic / Wiring Diagram
Control & Power Inputs
- BLUE Ground
- RED Power
Technical Specification
-
Light characteristics: Landing Light or Taxi Light / PAR36
-
Voltage range: +9..+36 VDC
-
Voltage protection: a. Transcient voltage: 2 seconds +80 VDC
b. Under-voltage lockout: +9 VDC, not more
c. Over-voltage lockout: +36 VDC, not less -
LED quantity: 18 pcs
-
Performance: 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 -
Chromaticity: Cool White
-
Viewing Angle: 8° Landing 9° x 20° Taxi
-
Ambient temperature: -55°C…+85°C / -67°F…+185°F
-
Overheat protection: Yes (temperature dependent decrement of intensity,see note below)
-
Wiring: N/A, Connector – 2 poles
-
Weight: 293 g / 10.33 oz
-
Useful life: not less than 30.000 aircraft flight hours.
Device RTCA/DO160 (G) qualified
Environment | Section | Category |
---|---|---|
Temperature / Altitude | 4 | F2 |
Temperature Variation | 5 | A |
Humidity | 6 | C |
Operational Shock and Crash Safety | 7 | B |
Vibration | 8 | U, curves G |
Explosive Atmosphere | 9 | H |
Waterproofness | 10 | R |
Fluids Susceptibility | 11 | F |
Sand and dust | 12 | D |
Fungus | 13 | F |
Salt Spray | 14 | T |
Magnetics Effects | 15 | Z |
Power Input | 16 | Z |
Voltage Spike | 17 | A |
Audio Freq. Conducted Susceptibility | 18 | Z |
Induced Signal Susceptibility | 19 | ZC |
Radiated and Conducted Susceptibility | 20 | TT |
Radiated and Conducted Emissions | 21 | H |
Icing | 24 | A and C |
Technical Drawing
dimensions in [inches] / mm
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.
Optic Simulation
Taxi Version
51 000 cd
Landing Version
100 000 cd
Equipment Limitation
Hercules JP should only be powered by +9..+36 V DC
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.
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:
-
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. -
Remove the light from the package.
Note that there is connector with 2 colors:
Blue – Ground
Red – Power -
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 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
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.
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.
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.
References
Read User Manual Online (PDF format)
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