User's Manual

ABBREVIATED COMPONENT MAINTENANCE MANUAL
1458-A-1101 / 1458-A-1300
B. Global Customer Care Center (Subtask 23-15-30-99F-008-A01)
(1) If you do not have access to the Honeywell Technical Publications Website, or if you need to
speak to personnel about non-Technical Publication matters, the Honeywell Aerospace Global
Customer Care Center gives 24/7 customer service to Air Transport & Regional, Business &
General Aviation, and Defense & Space customers around the globe.
• Telephone: [phone] (Toll Free U.S.A./Canada)
• Telephone: [phone] (International)
• Telephone: [phone] (EMEA Toll Free)
• Telephone: [phone] (EMEA Direct).
3. References (TASK 23-15-30-99F-803-A01)
A. Honeywell/Vendor Publications (Subtask 23-15-30-99F-009-A01)
(1) Not applicable.
B. Other Publications (Subtask 23-15-30-99F-010-A01)
(1) These publications are standard references:
• The United States GPO Style Manual 2000 (available at http://www.gpoaccess.gov
/stylemanual/browse.html)
• IEEE Std 260, Standard Letter Symbols for Units of Measurement (available from the
American National Standards Institute, New York, NY)
• ASME Y14.38, Abbreviations for Use on Drawings and in Text (available from the American
National Standards Institute, New York, NY)
• H4/H8 CAGE Codes (available at http://www.logisticsinformationservice.dla.mil)
• IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams (available
from the American National Standards Institute, New York, NY)
• TSO-C132 Geosynchronous Aeronautical Mobile Sat
ellite Services Earth Station Equipment
• ARINC 781 Mark 3 Aviation Satellite Communications System
• ARINC 758 Communications Management Unit Mark 2
• DO-160E Environmental Conditions and Test Procedures for Airborne Equipment
• DO-178B Software Considerations in Airborne Systems and Equipment Certification
• DO-254 Design Assurance Guidance for Airborne Electronic Hardware.
C. Certification and Approvals (Subtask 23-15-30-99F-011-A01)
(1) Installation of the A350 SDU and SCM system on an
aircraft typically requires the approval
of the appropriate government air/radio autho
rity (such as Transport Canada, the FAA, the
JAA, etc.). Honeywell highly recommends cont
acting the appropriate authorities early in the
system-planning phase to minimize approval/
certification issues that could delay release
of the aircraft.
(2) The conditions and tests for TSO approval of this article are minimum performance standards.
Those installing this article, on or within a specific type or class of aircraft, must determine
that the aircraft installation conditions are within the TSO standards. TSO articles must have
different approval for installation in an aircraft. The article can be installed only according to 14
CFR part 43, or the applicable airworthiness requirements.
(3) Contact Honeywell for more information on certification and approval issues.
EFFECTIVITY
ALL
23-15-30
Page 18 of 70
5 Oct 2012
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Interim DRAFT for FCC Approval Purposes
Do Not Use for Maintenance
10-Feb-2013