AVEO ENGINEERING AVE-LG-IM Morpheus 115VAC Logo Light Instruction Manual
- June 6, 2024
- AVEO ENGINEERING
Table of Contents
- Part 0 Document Administration
- Part 1 Installation data
- 1.1 Product info
- 1.2 Operating Instructions
- 1.3 Installation Schematic / Wiring Diagram
- 1.4 Control & Power Input
- 1.5 Technical Specification
- 1.6 Technical Drawing
- 1.7 Wiring Chart
- 1.8 Optic Simulation
- 1.9 Equipment Limitation
- 1.10 Care and Cleaning of Lights
- 1.11 Testing of the light before installation
- 1.12 Notes on Installation
- 1.13 Continued Airworthiness Information
- 1.14 RoHS Compliance Statement
- 1.15 EU REACH Regulation (EC) No. 1907/2006
- References
- Read User Manual Online (PDF format)
- Download This Manual (PDF format)
INSTALLATION MANUAL
Morpheus 115VAC
Logo LED Light
Issue 02
AVE-LG-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.
Part 0 Document Administration
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 the following part numbers:
- Morpheus™ 115VAC
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 the Head of DO.
Issue No. | Details | Date of issue | Affected Pages |
---|---|---|---|
01 | Initial Issue | 17 May 2018 | ALL |
02 | Technical specification update |
D0160 table addition
Technical drawing update
Note addition into section Wiring chart Picture addition into section Optic
simulation| 26 Aug 2021| 5
6
7
8
8
| Adding section 1.13 Continued Airworthiness
Information
Adding section 1.14 RoHS Compliance
Statement
Adding section 1.15 EU REACH Regulation
(EC) No. 1907/2006| | 11
12
12
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 – Affected Pages Column.
The reason(s) for EACH raise of the issue and the description of the 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**
Part 1 Installation data
1.1 Product info
The Morpheus™ logo light is a high-powered LED light used 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.
- Morpheus™ 115VAC
PN : AVE-LGM1WCNUB-20C
1.2 Operating Instructions
When installed on the aircraft, using the aircraft’s power (115 V AC), the light will be at its maximum intensity. The operating voltage range is 96 – 129V AC, 360-440 Hz.
1.3 Installation Schematic / Wiring Diagram
| White AWG 20
Black AWG 20
Green/Yellow AWG 20 | – GND
– 115 V AC
– Case
---|---|---
1.4 Control & Power Input
BLACK | Power Input 115 V AC |
---|---|
WHITE | Power Return – Ground |
GREEN/YELLOW | Case |
1.5 Technical Specification
Operating voltage range: | 96 – 129 V AC, 360-440 Hz |
---|---|
Dimensions: | 3.098“ x 6.5“ (78,7 mm x 165,1 mm) |
Ambient temperature: | -55°C..+85°C / -67°F..+185°F |
Overheat protection: | +85°C / +185°F |
Input Current: | 0.49 A @ 115V |
Output Power: | 40 W max. |
Input Power: | 56.35 W @ 115V |
Waterproof |
Device RTCA/DO160 qualified:
Environment | Section | Category |
---|---|---|
Temperature / Altitude | 4 | C2 |
Temperature Variation | 5 | A |
Humidity | 6 | C |
Operational Shock and Crash Safety | 7 | B |
Vibration | 8 | R, Curve G |
Explosive Atmosphere | 9 | A |
Waterproofness | 10 | S |
Fluids Susceptibility | 11 | F |
Sand and Dust | 12 | D |
Fungus | 13 | F |
Salt Spray | 14 | 5 |
Magnetics Effects | 15 | – |
Power Input | 16 | A (CF) |
Voltage Spike | 17 | – |
Audio Freq. Conducted Susceptibility | 18 | R (CF) |
Induced Signal Susceptibility | 19 | AC |
Radiated and Conducted Susceptibility | 20 | TT |
Radiated and Conducted Emissions | 21 | H |
Icing | 24 | A |
Radiated and Conducted Emissions | 25 | H |
1.6 Technical Drawing
1.7 Wiring Chart
Use the 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 the current is not given, then divide the power by the voltage.
1.8 Optic Simulation
Polar Candela Distribution Plot
Rectangular Candela Distribution Plot
1.9 Equipment Limitation
Morpheus™ should only be powered by 96-129 V AC.
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 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 products are used to clean the lights.
1.11 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 burn-in time as well as other functional testing. No light is released for sale without undergoing this extensive operational testing.
When you receive the Morpheus™ 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 are three wires:
BLACK| 115 V AC
---|---
WHITE| Ground
GREEN/YELLOW| Case -
Testing of the function of the light can be done with a regular 96-129 V AC power supply (not a battery charger). Connect the white wire to the ground (negative) leads of a power supply, and then connect the black wire to the positive (+) leads on the power supply. The logo light should start lighting. When installed on the aircraft, using the aircraft’s power (115 V AC), 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 96-129 V AC @ 360-440 Hz be used to test the light. Do not use Battery chargers, battery backup power devices, or other bench avionics testing methods to test the aviation light. The light is functional between 96 and 129 Volts. The 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 website: www.aveoengineering.com
1.12 Notes on Installation
Spread the tightening forces evenly around the mounting hole. Stainless steel screw is recommended. The length depends upon the placement location of the aircraft.
1.13 Continued Airworthiness Information
Circuit/Wiring Protection
Each Morpheus series light features a Negative Temperature Coefficient (NTC) circuit that limits internal temperatures by attenuating the 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.
Periodic Inspection Procedure
The Morpheus light is maintenance-free. Periodical checks that the light is functioning are to be done as required by the aircraft documentation. The light only contains one LED so the light is either fully operative or not. The problem of loss in intensity by partially failing LED is therefore not applicable.
1.14 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.
1.15 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 product maintenance
or
service is listed on the current European Chemicals Agency’s Candidate List of
Substances of Very High Concern for Authorization.
AVE-LG-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.