This manual includes data for the equipment that follows:
Component
ELT/NAV Interface453-6501-B
Part No.Model No.
ACR ELECTRONICS, INC / ARTEX PRODUCTS
5757 Ravenswood Rd, Ft. Lauderdale, FL 33312
25-69-11
Cage Code: 60253
Page 1 of 58
JUL 28/11
570-6501 Rev. B
Initial Issue OCT 05/2000
ACR ELECTRONICS, INC / ARTEX PRODUCTS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
PROPRIETARY INFORMATION
This document contains proprietary information and such information may not be disclosed to others for any
purpose, nor used for manufacturing purposes without written permission from ACR Electronics.
Information in this manual is subject to change without notice. ACR Electronics makes no warranty, expressed
or implied, with regard to this manual, including but not limited to any implied warranties of merchantability,
fitness for a particular purpose, and non-infringement. In addition, ACR Electronics makes no warranty with
regard to the documentation or data contained herein. ACR Electronics is not liable in the event of incidentals,
special, consequential, or any other damages in connection with or arising from furnishing, performance, or
use of this manual.
Reproduction of this publication or any portion thereof by any means is prohibited. for further information contact Sales, ACR Electronics, 5757 Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (928) 708-1550
AIRWORTHINESS LIMITATIONS
The Airworthiness limitations section is FAA approved and specifies inspections and other maintenance
required under 14 CFR§ 43.16 and 91.403, unless an alternative program has been approved.
IMPORTANT NOTICE
ACR Electronics will be responsible for full distribution and revisions of ICA’s (Instructions for Continued
Airworthiness) For inquiries regarding the content and currency of this manual, contact ACR Electronics,
5757 Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (928) 708-1550
25-69-11
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ACR ELECTRONICS, INC / ARTEX PRODUCTS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
ACR Electronics will be responsible for full distribution and revisions of ICA’s (Instructions for Continued
Airworthiness) For inquiries regarding the content and currency of this manual, contact ACR Electronics,
5757 Ravenswood Rd, Fort Lauderdale, FL 33312. Telephone (928) 708-1550ACR Electronics will be
responsible for full distribution and revisions of ICA’s (Instructions for Continued Airworthiness) For
inquiries regarding the content and currency of this manual, contact ACR Electronics, 5757 Ravenswood Rd,
Fort Lauderdale, FL 33312. Telephone (928) 708-1550
REV NO.DCN NO.DCN DATEREV NO.DCN NO.DCN DATE
-RELEASEOct 05/2000
-DCN 1747Jul 19/2001
-DCN 2033Jun 18/2002
ADCA W9414Apr 06/2010
BECO 14756Jul 28/2011
RECORD OF REVISIONS
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
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ACR ELECTRONICS, INC / ARTEX PRODUCTS
ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
SERVICE BULLETIN LIST
SERVICE
BULLETIN NO
ISSUE
DATE
SUBJECT
MANUAL
REV NO
MANUAL
REV DATE
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
-B (453-6501)
LIST OF EFFECTIVE PAGES
SUBJECTPAGEDATESUBJECTPAGEDATE
Title Page1Jul 28/1130Jul 28/11
Notices2Jul 28/11Test and Fault Isolation31Jul 28/11
(1)This manual describes the operation, installation, and maintenance of the ELT/NAV Interface -
B. This information is provided to ensure initial and continued airworthiness. Information
presented in this manual is accurate at time of printing, but is subject to change. Refer to the
Artex products web site at www.acrelectronics.com for the latest information and any updates
to this manual.
(2)Web links provided in this manual were accurate at time of printing but may be subject to
change.
-B (453-6501)
INTRODUCTION
(3)Regulatory references contained herein are generally confined to United States and Canadian
requirements and, in any case, should not be considered all encompassing. Consult your
national aviation authority for applicable requirements.
SUBTASK 25-69-11-990-002
B.Application
(1)This manual constitutes supporting data/documentation for the ELT/NAV Interface -B,
including:
(a)Description and Operation
(b)Test and Fault Isolation (includes inspection criteria)
(c)Removal
(d)Installation
(e)Illustrated Parts List
(2)In the United States, the ELT/NAV Interface -B must be installed and maintained in
accordance with the requirements herein and 14 CFR, FAR Parts 43, and 91; and other
airworthiness requirements, as applicable.
(3)In Canada, the ELT/NAV Interface -B must be installed and maintained in accordance with the
requirements herein and Canadian Aviation Regulations (CAR), Part V and other CAR
airworthiness requirements, as applicable.
(4)ELT/NAV Interface -B installation and maintenance in all other countries must comply with the
requirements herein and applicable national airworthiness requirements.
(5)To ensure proper operation, only parts listed in the Illustrated Parts List of this manual or
those recommended by ACR Electronics may be used as replacement parts for the ELT/NAV
Interface -B.
25-69-11
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ABBREVIATED COMPONENT MAINTENANCE MANUAL
TASK 25-69-11-990-802
2.Model Description
SUBTASK 25-69-11-990-001
A.ELT/NAV Interface -B
(1)The ELT/NAV Interface -B provides the means to transmit position data received from the
aircraft navigation system to the ELT.
(2)The ELT/NAV Interface -B is available in two installation configurations:
(a)24-bit auto reprogramming and position data, or
(b)Position data only.
SUBTASK 25-69-11-990-002
B.Compatibility
-B (453-6501)
(1)The ELT/NAV Interface -B is designed for use with the Model B406-4 ELT (P/N 453-5004) on
Boeing aircraft.
TASK 25-69-11-990-803
3.Approvals
SUBTASK 25-69-11-990-001
A.Certification
(1)FAA TSO C126 System Component
NOTE
:Details of TSO certification for the ELT/NAV Interface -B are available in the “ELT/
NAV Interface -B System Qualification Report” (Document 572-0013).
(a)The conditions and tests required for TSO approval of this article are minimum
performance standards. It is the responsibility of those installing this article either on or
within a specific type or class of aircraft to determine that the aircraft installation
conditions are within TSO standards. TSO articles must have separate approval for
installation in an aircraft. The article may be installed only if performed under 14 CFR
Part 43 or the applicable airworthiness requirements.
(2)JTSO-2C126
SUBTASK 25-69-11-990-002
B.RTCA DO-160C and DO-160D Compliance
(1)Environmental Categories:
(a)DO-160C: C1-BA204204XRXXXXXZAZZ204BXXX (Table 1, on page 17)
(b)DO-160D: D1(A2)-BB[204(B)][204(C1)XRXXXXXZAZZ[204(T)]ZXXXX (Table 2, on page