AVEO AVE-CCPS-IM Crystal Conforma Instruction Manual
- June 15, 2024
- AVEO
Table of Contents
INSTALLATION MANUAL
Crystal Conforma
AVE-CCPS-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
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:
• Crystal Conforma (Red, Raised wingtip)
• Crystal Conforma (Green, Raised wingtip)
• Crystal Conforma (Red, Drooped wingtip)
• Crystal Conforma (Green, Drooped wingtip)| AVE-CCPSR-R01
AVE-CCPSG-R01
AVE-CCPSR-D01
AVE-CCPSG-D01
---|---
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 |
|---|---|---|---|
| 1 | Initial Issue | 3-Jul-17 | ALL |
| 2 | Wiring diagram update | ||
| Section 1.7 text addition | 26-Jun-23 | 6, 7, 10 |
9
Affected 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
Part 1 Installation data
1.1 Product Info
Crystal Conforma™ is the ultimate ALL-IN-ONE wingtip module for aircraft. This
light provides Position and Strobe Light per ETSO standards.
Crystal Conforma (Red, Raised wingtip)
Crystal Conforma (Green, Raised wingtip)
Crystal Conforma (Red, Drooped wingtip)
Crystal Conforma (Green, Drooped wingtip)| AVE-CCPSR-R01
AVE-CCPSG-R01
AVE-CCPSR-D01
AVE-CCPSG-D01
---|---
1.2 Operating Instructions
When installed on the aircraft, using the aircraft’s power (14 and 28 volts), the light will be at its maximum intensity. Operating voltage range is 9 to 36 V DC.
1.3 Installation Schematic / Wiring Diagram
Wire length: 30“ minimum (770 mm minimum)
1.4 Control & Power Inputs
| Red | +14 V DC or +28 V DC, Nav. Steady |
|---|---|
| Yellow | +14 V DC or +28 V DC, Anti-collision Strobe |
| Black | Common 14 V DC or 28 V DC, return VRTN |
| Blue | Synchronisation |
| Green/Yellow | Chassis (Bonding) |
1.5 Technical Specification
Dimensions:| 286.8 mm x 62,1 mm x 56,5 mm
11.29” x 2.44” x 2.22”
---|---
Weight:| max. 410 g / 0.90 lbs
Operating Voltage Range:| 9 to 36 V DC
Input power, not more than:
| – navigation – steady red | 4.5 W |
|---|---|
| – navigation – steady green | 7.1 W |
| – pulse strobe white | 36 W |
Input Current, not less than:
| – navigation steady red | 0.42A@14VDC |
|---|---|
| – navigation steady red | 0.21A@28VDC |
| – navigation steady green | 0.6A@14VDC |
| – navigation steady green | 0.3A@28VDC |
| – white strobe | 2.48A@14VDC |
| – white strobe | 1.15A @28VDC |
| Repetition Flash Rate of Strobe: | 50 cycles per minute |
| --- | --- |
| Warm up time: | not more than 40 s |
| Low temperature slope start: | not more than 60 s |
| Ambient temperature: | -55 °C … +80 °C |
| Overheat protection: | +85 °C |
Voltage protection:
a. Transient voltage:
b. Under-voltage lockout:
c. Over-voltage lockout:| 60 V, both polarities
9 V , not more
36 V, not less
---|---
1.6 Technical Drawing
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.
1.8 Equipment Limitation
Crystal Conforma should only be powered by 9-36 V DC.
1.9 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.
1.10 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 Crystal Conforma light, and wish to test the function of
the light prior to installation on your aircraft, please observe the following
procedure:
- Review the written information that is enclosed in the packaging. Warranty information as well as a cautionary note about power supply removal is enclosed in each package.
- Remove the light from the package. Note that there are two sets of wires:
Red| +14 V DC or +28 V DC, Nav. Steady
---|---
Yellow| +14 V DC or +28 V DC, Anti-collision Strobe
Black| Common 12 V DC or 28 V DC return VRTN
Blue| Synchro
Green/Yellow| Chassis - Testing the function of the light can be accomplished using a regular 14V/10A DC or 28V/5A DC power supply (not a battery charger).
Connect the black wire to the ground (negative) leads of a power supply, then
connect the yellow or red wire to the positive (+) leads on the power supply.
The light should start flashing (yellow wire = strobe light) or lighting (red
wire = green/red light). Connecting the blue wires from each Crystal Conforma
light together (and not to the ground or positive terminals on the battery)
should result in flashing all lights at once.
It indicates the synchronization feature is working properly.
When installed on the aircraft and using the aircraft’s power (28 volts), the
light will be at its maximum intensity.
If the tests are successfully completed, the lights can be installed on the
aircraft.
IMPORTANT NOTES:
Under no circumstances should any power supply other than a 9-36V DC, or a 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 and 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.
1.11 Notes on Installation
In order to meet all ETSO requirements, the Crystal Conforma light module
should be installed into an Aveo manufactured wingtip only. In case you intend
to mount any other than AVEO wingtip, contact kindly the manufacturer on the
website http://www.aveoengineering.com/contact-us/.
Stainless steel screws M4 (DIN912) or SHCS #8-32 or equivalent mounting screws
are recommended to be used for installation. Screw length depends on placement
of screws on aircraft.
Spread the tightening forces evenly around the mounting hole.
1.12 Continued Airworthiness Information
From the webpage http://www.aveoengineering.com/ the customer can
download the form F-AVE-001A which shall be used by operator for reporting any
occurrences to the Aveo Engineering as the ETSO holder. The form contains the
Aveo Engineering telephone number and the occurrence e-mail address
([email protected]).
The operator shall report immediately as the ETSO holder is obliged to report occurrences having potential to lead to an unsafe condition within 72 hours.
a. Circuit/Wiring Protection
Each Galactica series light features a Negative Temperature Coefficient
(NTC) circuit that limits internal temperatures by attenuating operating
current (with corresponding reduction of brightness) when internal
temperatures reach a certain threshold. This proprietary circuitry is intended
for protecting the light itself, and associated aircraft wiring, from a
thermal runaway condition. The operation of strobes without airflow is
recommended to be limited in order to avoid heat buildup. This NTC circuitry
feature
enables the life of LEDs and electronic components to be tripled and thereby
provide an even great margin of safety for continued airworthiness due to the
dramatic enhancement of electronics reliability.
b. Periodic Inspection Procedure
The Crystal Conforma lights should always be checked for proper operation
during preflight. This procedural information is already provided in all
general aviation aircraft flight manuals.
The lights should be visually examined for general condition, proper
operation, and correct installation at each inspection to be carried out
annually and/or after 100 hours of operation. Any debris or atmospheric
deposits accumulated on the surface of the lights should be removed using a UV
Wax such as Farecia Profile UV Wax to ensure ongoing optical clarity.
In addition, refer to section 1.10 of installation manual for detailed
cleaning instructions.
The following procedure shall be performed, firstly, in the steady mode and
secondly, in the strobe mode:
- Turn the lights on.
- Put on polarized sunglasses or welder goggles to prevent eye damage when looking into the lights.
- Examine the individual LEDs. If any of the LEDs fail, the light shall be removed and sent to Aveo Engineering for replacement under the Warranty Program.
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.
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.
References
- Aveo Engineering - Brilliantly Different - AveoEngineering
- Aveo Engineering - Brilliantly Different - AveoEngineering
- Contact Us - AveoEngineering