Midcontinent MD41-1817 Documento tecnico

INSTALLATION MANUAL AND

OPERATING INSTRUCTIONS

MD41-1817

Annunciation Control Unit

For Lithium Ion Battery Systems

MD41-1817 28vdc Horizontal Mount

Mid-Continent Instruments and Avionics Manual Number 9018252

9400 E. 34th Street N., Wichita, KS 67226 USA Rev. D January 27, 2020

Phone 316-630-0101  Fax 316-630-0723

Rev. D January 27, 2020 2 Manual Number 9018252

FOREWORD

This manual provides information intended for use by persons who, in accordance with current regulatory

requirements, are qualified to install this equipment. If further information is required, please contact:

Mid-Continent Instruments and Avionics

Attn: Customer Service Dept.

9400 E. 34th ST North

Wichita, KS 67226 USA

Phone 316-630-0101 Fax 316-630-0723

We welcome your comments concerning this manual. Although every effort has been made to keep it

free of errors, some may occur. When reporting a specific problem, please describe it briefly and include

the manual part number, the paragraph/figure/table number, and the page number. Send your

comments to:

Mid-Continent Instruments and Avionics

Attn: Technical Publications

9400 E. 34th ST North

Wichita, KS 67226 USA

Phone 316-630-0101, Fax 316-630-0723

[email protected]

www.mcico.com

Mid-Continent Instruments and Avionics

Rev. D January 27, 2020 3 Manual Number 9018252

REVISION DETAIL

Rev. Date Detail

A 09/29/14 Initial Release.

B 07/29/15 Added Environmental Qualification Form.

C 04/25/16 Revised graphics and text to change annunciation text from STANDBY to

CHARGING and FAIL to TEMP. Minor modifications to Sections 3 and 4.

Added DO-160 section 22 qualification test.

D 01/24/20 Added wiring diagrams for 6430017-2 battery connections.

Rev. D January 27, 2020 4 Manual Number 9018252

TABLE OF CONTENTS

SECTION 1 GENERAL DESCRIPTION 5

1.1 INTRODUCTION 5

1.2 TECHNICAL SPECIFICATIONS 5

1.2.1 MODELS 5

1.2.2 PHYSICAL ATTRIBUTES 5

1.2.3 PERFORMANCE 5

SECTION 2 INSTALLATION CONSIDERATIONS 6

2.1 COOLING 6

2.2 EQUIPMENT LOCATION 6

2.3 ROUTING OF CABLES 6

2.4 LIMITATIONS 6

2.5 TECHNICAL SPECIFICATIONS 6

SECTION 3 INSTALLATION PROCEDURE 7

3.1 GENERAL INFORMATION 7

3.2 UNPACKING AND INSPECTING 7

3.2.1 INCLUDED PARTS 7

3.2.2 AVAILABLE PARTS 7

3.3 CABLE HARNESS 7

3.3.1 LIGHTING CONTROLS 11

3.3.2 POWER AND SIGNALS 12

3.3.3 HARNESS VERIFICATION 12

3.4 MOUNTING 13

SECTION 4 OPERATION 14

4.1 FRONT PANEL CONTROLS AND ANNUNCIATIONS 14

4.1.1 CONTROLS 14

4.1.2 ANNUNCIATIONS 14

SECTION 5 CONFORMANCE 15

5.1 CONTINUED AIRWORTHINESS STATEMENT 15

APPENDIX 1 16

NUMBER LIST OF TABLES AND FIGURES

TABLE 1 MODELS 5

TABLE 2 PHYSICAL ATTRIBUTES 5

TABLE 3 PERFORMANCE 5

FIGURE 1 25 PIN D-SHELL REAR VIEW CONNECTOR PINOUT 7

TABLE 4 SCHEMATIC PINOUT 8

FIGURE 2 WIRING DIAGRAM – TWO TB17 (6430017-1) BATTERIES 8

FIGURE 3 WIRING DIAGRAM – ONE TB17 (6430017-1) BATTERY 9

FIGURE 4 WIRING DIAGRAM – TWO TB17 (6430017-2) BATTERIES 10

FIGURE 5 WIRING DIAGRAM – ONE TB17 (6430017-2) BATTERY 11

FIGURE 6 OUTLINE DRAWING 13

FITURE 7 FRONT PANEL 14

Rev. D January 27, 2020 5 Manual Number 9018252

SECTION 1 GENERAL DESCRIPTION

1.1 INTRODUCTION

The MD41-1817 products are compact, self-contained Annunciation and Control Units (ACUs). The fully

integrated control unit provides annunciation for Mid-Continent Instruments and Avionics TB17 battery

systems. It combines the necessary functions and annunciations required to interface with an approved

system.

Highlighted features include long-life LEDs used for all lighting, internally backlit selection switch, dead-

front inactive annunciations, and the installation option for manual or automatic dimming. An external

annunciation dimming adjustment is provided for balancing low-level light conditions.

1.2 TECHNICAL SPECIFICATIONS

1.2.1 MODEL

MD41-1817

Orientation Horizontal

Power Input 28VDC

Lighting Input 28VDC

TABLE 1

MODEL

1.2.2 PHYSICAL ATTRIBUTES

Characteristics:

Weight: 0.26 pounds

Dimensions:

(not including connector or mate)

3.2 inches long

2.75 inches wide

0.8 inches high

Mating Connector: Positronic RD25F10JVL0 or equivalent (MCI P/N 7014517)

Instrument Panel Mounting: Rear mount

TABLE 2

PHYSICAL ATTRIBUTES

1.2.3 PERFORMANCE

Specifications:

Power Requirement: 0.20 A max

TABLE 3

PERFORMANCE

Rev. D January 27, 2020 6 Manual Number 9018252

SECTION 2 PRE-INSTALLATION CONSIDERATIONS

2.1 COOLING

No direct cooling is required. As with any electronic equipment, overall reliability may be increased if the

unit is not located near a high heat source or crowded next to other equipment. Means of providing some

airflow is considered beneficial.

2.2 EQUIPMENT LOCATION

The MD41-1817 ACU must be mounted as close to the pilot’s field of view as possible. The unit depth,

with connector attached, must also be taken into consideration when selecting an appropriate location.

Allow at least 3 inches of space behind the unit for connector attachment and removal.

2.3 ROUTING OF CABLES

Care must be taken not to bundle the MD41 series ACU logic and low level signal lines with any high

energy sources. Examples of these sources include 400 Hz AC, Comm, DME, HF and transponder

transmitter coaxial cables. Always use shielded wire when shown on the installation print.

Avoid sharp bends in cabling and routing near aircraft control cables. Also avoid proximity and contact

with aircraft structures, avionics equipment, or other obstructions that could chafe wires during flight and

cause undesirable effects.

2.4 LIMITATIONS

Note that this product is part of an incomplete system. It is designed to be installed with other applicable

equipment to provide functionality for main battery systems.

2.5 TECHNICAL SPECIFICATIONS

The MD41-1817 complies with the manufacturers’ specifications and has been verified and approved for

use with the following systems:

Mid-Continent Instruments and Avionics

Model Number(s):

Designed for use with

Battery System:

MD41-1817

Manufacturer: Mid-Continent

Instruments and Avionics

Model(s): TB17

Rev. D January 27, 2020 7 Manual Number 9018252

SECTION 3 INSTALLATION PROCEDURES

3.1 GENERAL INFORMATION

This section contains interconnect diagrams, mounting dimensions and other information pertaining to

the installation of the MD41 series ACU. After installation of cabling and before installation of the

equipment, ensure that power is applied only to the pins specified in the interconnect diagram.

3.2 UNPACKING AND INSPECTING EQUIPMENT

When unpacking this equipment, make a visual inspection for evidence of any damage that may have

incurred during shipment.

3.2.1 INCLUDED PARTS

A. Main Battery ACU – MCIA P/N MD41-1817 series

B. Installation Manual – MCIA P/N 9018252

3.2.2 AVAILABLE PARTS

A. J1 Connector Kit (25 pin) – MCIA P/N 7014517

B. 7-pin Cylindrical TB17 Signal Connector – MCIA P/N 9017889-1

C. Annunciator Cutout Template – MCIA P/N 8014474

3.3 CABLE HARNESS

The MD41 cable harness should be made using 24 AWG wire or larger for all connections. Construct the

cable harness with regards to the instructions below and using the Connector Pinout of Figure 1,

Schematic Pinout of Table 4, and Wiring Diagram of Figures 2 and 3.

FIGURE 1

REAR VIEW OF 25-PIN D-SUB CONNECTOR (J1)

Rev. D January 27, 2020 8 Manual Number 9018252

Connector Pinout

Pin # Description Pin # Description

1 CHARGING, Battery 1 14 Reserved

2 HEATING, Battery 1 15 Pin 2 of RTD 1, Battery 2

3 FAIL/FAULT, Battery 1 16 Pin 1 of RTD 1, Battery 2

4 HEATING, Battery 2 17 Panel Lighting Input, 28VDC

5 CHARGING, Battery 2 18 Pin 1 of RTD2, Battery 2

6 FAIL/FAULT, Battery 2 19 Output to Pin 1 of RTD 1, Battery 2

7 Pin 2 of RTD 1, Battery 1 20 Input from Pin 1 of RTD 2, Battery 1

8 Pin 1 of RTD 1, Battery 1 21 Input from Pin 1 of RTD 2, Battery 2

9 Pin 1 of RTD 2, Battery 1 22 Pin 1 of Over Temperature Warning

10 Output to Pin 1 of RTD 1, Battery 1 23 Pin 2 of Over Temperature Warning

11 28 VDC, Battery 1 24 GROUND

12 28 VDC, Battery 2 25 GROUND

13 28 VDC, Aircraft Power

TABLE 4

SCHEMATIC PINOUT

CHARGING ANNUN, BATT 1

USE 2A CIRCUIT BREAKER

FROM LIGHTING BUS

HEATING ANNUN, BATT 2

OUTPUT TO RTD1/PIN1, BATT 2

RTD1/PIN1, BATT 2

CHARGING ANNUN, BATT 2

28 VDC AIRCRAFT PWR

OVER-TEMP WARN, PIN 1

OVER-TEMP WARN, PIN 2

BATTERY 2, 28 VDC

FAIL/FAULT ANNUN, BATT 2

HEATING ANNUN, BATT 1

RTD1/PIN1, BATT 1

OUTPUT TO RTD1/PIN1, BATT 1

FAIL/FAULT ANNUN, BATT 1

BATTERY 1, GROUND

BATTERY 1, 28 VDC 2A

28VDC

BATTERY 1

RESERVED

BATTERY 2, GROUND

NOTES:

1) ALL WIRING SHALL BE 24 AWG UNLESS OTHERWISE NOTED.

BATTERY 2

RTD1/PIN2, BATT 1

INPUT FROM RTD2/PIN1, BATT 1

RTD2/PIN1, BATT 1

RTD1/PIN2, BATT 2

INPUT FROM RTD2/PIN1, BATT 2

RTD2/PIN1, BATT 2

FIGURE 2

WIRING DIAGRAM - TWO TB17 (6430017-1) BATTERIES

Rev. D January 27, 2020 9 Manual Number 9018252

USE 2A CIRCUIT BREAKER

FROM LIGHTING BUS

28 VDC AIRCRAFT PWR

OVER-TEMP WARN, PIN 1

OVER-TEMP WARN, PIN 2

HEATING ANNUN, BATT 1

RTD1/PIN1, BATT 1

OUTPUT TO RTD1/PIN1, BATT 1

CHARGING ANNUN, BATT 1

FAIL/FAULT ANNUN, BATT 1

BATTERY 1, GROUND

BATTERY 1, 28 VDC 2A

28VDC

BATTERY 1

RESERVED

NOTES:

1) ALL WIRING SHALL BE 24 AWG UNLESS OTHERWISE NOTED.

RESERVED

RTD1/PIN2, BATT 1

INPUT FROM RTD2/PIN1, BATT 1

RTD2/PIN1, BATT 1

FIGURE 3

WIRING DIAGRAM - ONE TB17 (6430017-1) BATTERY

Rev. D January 27, 2020 10 Manual Number 9018252

USE 2A CIRCUIT BREAKER

FROM LIGHTING BUS

HEATING ANNUN, BATT 2

OUTPUT TO RTD1/PIN1, BATT 2

RTD1/PIN1, BATT 2

CHARGING ANNUN, BATT 2

28 VDC AIRCRAFT PWR

OVER-TEMP WARN, PIN 1

OVER-TEMP WARN, PIN 2

BATTERY 2, 28 VDC

FAIL/FAULT ANNUN, BATT 2

HEATING ANNUN, BATT 1

RTD1/PIN1, BATT 1

OUTPUT TO RTD1/PIN1, BATT 1

CHARGING ANNUN, BATT 1

FAIL/FAULT ANNUN, BATT 1

BATTERY 1, GROUND

BATTERY 1, 28 VDC 2A

28VDC

BATTERY 1

RESERVED

BATTERY 2, GROUND

NOTES:

1) ALL WIRING SHALL BE 24 AWG UNLESS OTHERWISE NOTED.

BATTERY 2

RTD1/PIN2, BATT 1

INPUT FROM RTD2/PIN1, BATT 1

RTD2/PIN1, BATT 1

RTD1/PIN2, BATT 2

INPUT FROM RTD2/PIN1, BATT 2

RTD2/PIN1, BATT 2

FIGURE 4

WIRING DIAGRAM - TWO TB17 (6430017-2) BATTERIES

105W, 1/4W

Indice

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