Aveo Engineering THOR 36 DROP-IN Bedienungsanleitung

INSTALLATION MANUAL

THOR 36 DROP-IN

AVE- THD36-IM

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.

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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 THOR™ 36 DROP-IN................................................................5

1.2 OPERATING INSTRUCTIONS ..........................................................5

1.3 INSTALLATION SCHEMATIC /WIRING DIAGRAM...................................5

1.4 CONTROL &POWER INPUTS..........................................................6

1.5 TECHNICAL SPECIFICATION ..........................................................6

1.6 TECHNICAL DRAWING.................................................................7

1.7 WIRING CHART ........................................................................7

1.8 OPTIC SIMULATION ...................................................................8

1.9 EQUIPMENT LIMITATION ............................................................ 10

1.10 CARE AND CLEANING OF LIGHTS .................................................. 10

1.11 TESTING THE LIGHTS BEFORE INSTALLATION .................................... 10

1.12 CONTINUED AIRWORTHINESS INFORMATION .................................... 11

1.13 ROHS COMPLIANCE STATEMENT .................................................. 11

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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 following part numbers:

•THOR 36 DROP-IN LANDING - AVE-THD36LW-TD1

•THOR 36 DROP-IN TAXI - AVE-THD36TW-TD1

Compiled by: 09 Dec 2020

Petr Jaros

Engineer, Aveo Engineering Group, s.r.o.

Approved by: 09 Dec 2020

Georg Hartl

Head of DO, Aveo Engineering Group, s.r.o.

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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.

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

Issue

No.

Details

Date of

issue

Effected

Pages

Initial Issue

27 Oct 2020

ALL

Lens and intensity update

09 Dec 2020

6, 8, 9

Table 01: Record of Document Amendments

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Part 1 Installation data

1.1 THOR™36 Drop-In

THOR 36 Drop-In 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.

•THOR 36 DROP-IN LANDING - AVE-THD36LW-TD1

•THOR 36 DROP-IN TAXI - AVE-THD36TW-TD1

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

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1.4 Control & Power Inputs

BLUE Ground

RED Power

1.5 Technical Specification

Light characteristics: Landing Light or Taxi Light / PAR36 replacement

Voltage range: +9..+36 VDC

Voltage protection: a. Transcient voltage: 2 second +40 VDC

b. Under-voltage lockout: +9 VDC, not more

c. Over-voltage lockout: +36 VDC, not less

LED quantity: 14 pcs

Performance: a. Output power: 55 W

b. Input current: 4.7 A @ 14 VDC

2.25 A @ 28 VDC

c. Input power: 65.8 W @ 14 VDC

63 W @ 28 VDC

Chromaticity: Cool White, Color shade 1D0

Viewing Angle: 9°

7.5° Landing

11x16.5 °

9x11° Taxi

Low temp. slope start: -55°C / -67°F

Ambient temperature: -55°C...+85°C / -67°F...+185°F

Overheat protection: Yes

Wiring: N/A, Terminal Block –2 contacts

Weight: 562 g / 19.82 oz

Useful life: not less than 30.000 aircraft flight hours.

Device RTCA/DO160 qualified:

•chapter 4, Temperature - Altitude, Category F2

•chapter 5, Temperature Variation, Category A

•chapter 6, Humidity, Category C

•chapter 7, Operational Shocks and Crash Safety, Category B

•chapter 8, Vibration, Category U, curves G

•chapter 9, Explosion proofness, Category H

•chapter 10, Waterproofness, Category R

•chapter 11, Fluids Susceptibility, Category F

•chapter 12, Sand and Dust, Category D

•chapter 13, Fungus resistance, Category F

•chapter 14, Salt spray, Category T

•chapter 15, Magnetic effects, Category Z

•chapter 16, Power Input, Category ZXX

•chapter 17, Voltage Spike, Category A

•chapter 18, Audio Frequency Conducted Susceptibility, Category Z

•chapter 19, Induced Signal Susceptibility, Category ZC

•chapter 20, Radio Frequency Susceptibility, Category T

•chapter 21, Emission of Radio Frequency Energy, Category H

•chapter 22, Lightning induced transient susceptibility test, Category A2E2X

•chapter 24, Icing, Category A

•chapter 25, Electrostatic Discharge (ESD), Category A

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1.6 Technical Drawing

1.7 Wiring Chart

*dimensions in [inches] / mm

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1.8 Optic Simulation

Taxi Version

73 900 cd

82 300 cd

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Landing Version

143 990 cd

211 800 cd

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1.9 Equipment Limitation

Thor 36 Drop-In 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 Thor 36 Drop-In 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:

Blule –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 Thor 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 voltbattery 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.

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