T
(F9111)
45, rue de Villiers
92526 Neuilly-sur-Seine Cedex - France
Tel : (33) 1 57 77 80 00
Fax : (33) 1 57 77 80 24
BATTERY CHARGE LIMITER
PART NUMBER
35-0L5-1003-06
35-0L5-1004-07
35-0L5-1005-08
35-0L5-1006-08
COMPONENT MAINTENANCE MANUAL
APPENDIX A
AUTOMATIC TEST REQUIREMENTS
Revision No. 13 24-38-34A
First issue : DEC 15/88 TP 1
COPYRIGHT THALES AVIONICS S.A. MAR 23/11
T
COMPONENT MAINTENANCE MANUAL
35-0L5
This document and any data included are the property of THALES. They cannot be reproduced, disclosed
or utilized without the company’s prior written approval. The recipient shall not use this document for any
purpose other than the installation or maintenance of relevant equipment and shall return it promptly to
THALES upon its request.
Users are kindly requested to notify THALES of any discrepancy, omission or error found in this manual.
Please send your comments to :
T
Documentation Department
18, Avenue du Maréchal Juin - B.P. 49
92362 Meudon-la-Forêt Cedex France
If you are calling from inside FRANCE :
Tel : 01 39 45 50 00
Fax : 01 39 45 58 71
If you are calling from abroad :
Tel : + 33 (0) 1 39 45 50 00
Fax : + 33 (0) 1 39 45 58 71
If you do not yet have access to our CMM website, you can apply through the following address :
http://www.thalesgroup.com
If you do not have internet access, you can ask for the file(s) to be sent to you from :
techpubs.frontoffice@fr.thalesgroup.com
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COMPONENT MAINTENANCE MANUAL
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RECORD OF REVISIONS
REV. REVISION INSERTION BY REV. REVISION INSERTION BY
No. DATE DATE No. DATE DATE
1 JUN 30/89
2 MAY 15/91
3 NOV 30/92
4 APR 30/94 APR 30/94 AS
5 MAY 15/96 MAY 15/96 AS
6 APR 04/06 APR 06 CC
7 OCT 20/06 NOV 06 CC
8 DEC 21/06 JAN 07 CC
9 JUN 26/07 JUL 07 CC
10 SEP 12/08 SEP 08 CC
11 NOV 28/08 DEC 08 CC
12 FEB 20/09 MAR 09 CC
13 MAR 23/11 APR 11 THAV
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COMPONENT MAINTENANCE MANUAL
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SERVICE BULLETIN LIST
EQUIPMENT
SERVICE BULLETIN PART NUMBER MANUAL
MODIFICATION REV
NO DATE SUBJECT STATE NO
35-0L5-24
-001 JUN 30/89 Evolution of unit to standard 35-0L5-1003-06 -
S6-00.
-002 MAY 15/91 Improved mechanical resistance 35-0L5-1003-0X -
of the boards in the unit.
-003 NOV 30/92 Evolution of unit 35-0L5-1003-07 -
(standard S7).
-004 Rev1 APR 30/94 Evolution of unit 35-0L5-1004-07 6
(standard S7). Amdt. A
-005 Rev1 APR 30/94 Evolution of unit 35-0L5-1003-06 6
(standard S6). Amdt. A and B
-006 APR 30/94 Evolution of unit to standard 35-0L5-1005-08 -
S8.
-007 MAY 15/96 Evolution of unit to standard 35-0L5-1005-08 -
S8. Amdt. A
-009 JUL/26/05 Discontinuation of the external 35-0L5-1005-08 6
painting. Amdt. B
-010 AUG 31/06 Inspection and replacement of None 7
capacitors on CPU and acquisi-
tion boards.
-011 Rev1 APR 27/07 Improvement of the robustness. 35-0L5-1003-06 9
35-0L5-1004-07
35-0L5-1005-08
Amdt. C
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COMPONENT MAINTENANCE MANUAL
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SERVICE BULLETIN LIST
For PNR 35-0L5-100x
EQUIPMENT
SERVICE BULLETIN PART NUMBER MANUAL
MODIFICATION REV
NO DATE SUBJECT STATE NO
35-0L5-24
-012 JUN 17/08 Introduction of a new type of 35-0L5-100x 10
Microprocessor. Amdt. D
-013 JUL 03/08 Inspection of the CPU board. None 10
-014 Rev1 MAY 18/10 Introduction of a new converter 35-0L5-100x 13
on the power supply board Amdt. E
-015 MAY 18/10 Improvement of the power up 35-0L5-100x 13
sequence management. Amdt. F
-016 MAR 17/11 Introduction of a new hardware 35-0L5-1006 13
standard due to obsolescence Amdt. F
of microprocessor (Mod. state
1006-08).
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COMPONENT MAINTENANCE MANUAL
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LIST OF EFFECTIVE PAGES
SUBJECT PAGE DATE SUBJECT PAGE DATE
Title Page 7 DEC 21/06
TP 1 MAR 23/11 * 8 MAR 23/11 *
TP 2 MAR 23/11 * 9 DEC 21/06
10 DEC 21/06
Record of 11 MAR 23/11 *
Revisions 12 MAR 23/11 *
ROR 1 MAR 23/11 *
ROR 2 Blank
Record of Temporary
Revisions
RTR 1 DEC 15/88
RTR 2 Blank
Service Bulletin
List
SBL 1 JUN 26/07
SBL 2 MAR 23/11 *
List of Effective
Pages
LEP 1 MAR 23/11 *
LEP 2 Blank
Table of Contents
TC 1 MAR 23/11 *
TC 2 Blank
Introduction
INTRO 1 NOV 30/92
INTRO 2 DEC 21/06
Automatic Test
Requirements
1 DEC 21/06
2 DEC 21/06
3 DEC 21/06
4 DEC 21/06
5 DEC 21/06
6 DEC 21/06
* indicates pages modified, deleted or inserted 24-38-34A
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COMPONENT MAINTENANCE MANUAL
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TABLE OF CONTENTS
PAGES
AUTOMATIC TEST REOUIREMENTS
1. Test conditions 1
2. Equipment required 1
3. Operating instructions 1
A. Brief description system 1
B. Principle 2
C. Operation 6
4. Test specification of the unit 8
A. General 8
B. Preliminary tests 8
C. Description ATLAS testing 8
D. Test specification architecture 9
E. Presentation of the ATLAS Test Specification 11
..............................................................................
LIST OF ILLUSTRATIONS
Figure 1 General view of the ATEC 3
Figure 2 ATEC System Architecture 5
Figure 3 Test Specification Architecture 10
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COMPONENT MAINTENANCE MANUAL
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The SMART system software controls the operation of the
instrumentation system for UUT testing. It includes :
- a man-machine interface,
- the interface between the TCC and the instrumentation system,
- the software environment to execute test programs,
- the functions necessary for the development and debugging of ATLAS
test programs,
- the functions necessary for the software configuration of the
instrumentation system.
The instrumentation system provides :
- source and sensor resources,
- ARINC 608A defined switching unit.
The Unit Under Test (UUT) and its Test Unit Adaptor (TUA) are
connected to the instrumentation system via the ARINC 608A standard
interface. A wide range of ATEC configurations is available, each
including a different set of test instruments.
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4. Test specification of the unit
A. General
This specification written in ATLAS language gives the general actions to
be carried out to test the Unit using an Automatic Test Equipment.
ATLAS (Abbreviated Test Language for All Systems) is a standard language
for describing test functions and programming test procedures in
accordance with ARINC 626 specification.
B. Preliminary tests
It is recommended to test insulation and electrical bonding of the unit
before starting test procedure written in ATLAS.
(1) Equipment required
- a megohmmeter.
- a milliohmmeter.
(2) Insulation test
- Short circuit all pins of rear connector (P1) except pin (P1-E).
- Connect the megohmmeter between interconnected pins and pin (P1-E),
under 45VDC voltage.
- Measure : R greater than 400 Mohms.
- Disconnect megohmmeter and interconnected pins.
(3) Bonding test
- Connect the milliohmmeter between pin (P1-E) and box structure,
under a 1A current.
- Measure : R lower than 20 Mohms.
- Disconnect milliohmmeter.
C. Description of ATLAS testing with ATEC series 6
(1) Preliminary Conditions, Test Equipment and Materials
(a) Test Conditions
1 The tests are done in these environmental conditions :
- Temperature : 15 to 30°C.
- Pressure : No specific environmental level other than the
ambient pressure level.
- Relative humidity : Refer to the Standard Practices Manual
Ref 20-00-02, Introduction page 2.§3.B Special instruction in
relation to SSD.
NOTE: Before the tests, let the equipment stay in these
conditions for two hours.
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COMPONENT MAINTENANCE MANUAL
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E. Presentation of the ATLAS Test Specification :
(1) ATLAS Test Specification for Part Numbers : 35-0L5-1003-06, 35-0L5-
1004-07, 35-0L5-1005-08 and 35-0L5-1006-08:
(a) The ATLAS Test Specification for the equipment is referenced by :
"SOURCE SPECIFICATION: DATED JAN 31/10" contained on related file
24-38-34A_ATS_6-E13E.pdf.
(b) The SOURCE Specification corresponds to the ATEC Program PN :
- 6-E13E release .. (on ATEC Series 6) Where :
.. = 01 to 99 : correction of test program independent of test
specification (example : typographical errors).
NOTE: Equivalent test programs and test benches can be used.
The illustration that follows shows the top of the "Main
Module"
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000010 BEGIN, ATLAS PROGRAM 'AS-BCL-MAIN' $
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****** ******
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****** A T L A S S O U R C E P R O G R A M F O R ******
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****** B A T T E R Y C H A R G E L I M I T E R (B.C.L) ******
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****** M A I N P R O G R A M ******
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****** SOURCE FILE NAME : E1ZZMA00.AS ******
****** ******
****** MANUFACTURER : THALES AVIONICS ******
****** ******
****** UUT PART-NUMBER : 35-0L5-1003-06 ******
****** 35-0L5-1004-07 ******
****** 35-0L5-1005-08 ******
****** 35-0L5-1006-08 ******
****** ******
****** SOURCE SPECIFICATION : DATED : JAN 31/10 ******
****** ******
****** ******
****** FOR MORE INFORMATIONS OR REFERENCES ******
****** SEE "IDENTIFY-PRODUCT" PROCEDURE IN THIS MODULE ******
****** ******
****** ******
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