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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
WARNING: TO PREVENT DAMAGE TO THE UNIT, DO NOT INSERT THE
SCREWS MORE THAN 0.26 INCHES INSIDE THE CHASSIS OF
THE UNIT.
(4)
I nstallation Notes
2 9 B
1. All wire in accordance with MIL-W-22759/34, or equivalent, unless
otherwise specified.
2. All cable in accordance with MIL-C-27500 unless otherwise specified.
3. All coaxial cable in accordance with MIL-C-17 unless otherwise specified.
Coaxial cable must be manufacturer certified to meet FAR 25 Appendix F
Flammability Requirements.
4. Fabrication and installation of wiring harness in accordance with AC
43.13-1B, Chapter 11.
5. Grounding and bonding in accordance with AC 43.13-1B, Chapter 11,
Section 15 (bond J1 Pin B to airframe ground.)
6. Installation of CNX system in accordance with AC 43.13-1B, Chapter 4,
Section 4 and AC 43.13-2A, Chapter 2.
7. Refer to the aircraft structural repair manual and the aircraft maintenance
manual for instructions and information pertinent to this installation.
8. For all CNX variants, use circuit breaker part number MS3320-5 or
MS26574-5 or equivalent.
9. Connect power input to a load-sheddable bus.
10. The CNX system is qualified for installation in a pressurized, temperature
controlled location on an aircraft operated at cabin altitudes up to 15,000
feet.
11. After completing a first time installation of the unit, perform the
post-installation test procedure described in Post-Installation EMI Test
Procedure, CNX Network Module (TS-1110-50150) to ensure
non-interference with existing onboard systems.
Note: Installation of the CNX system according to this manual, STC, or other
airworthiness authority approved documentation does not authorize the use of
portable electronic devices onboard an aircraft. The permitted use of a portable
electronic device is the responsibility of operators in conjunction with their
regulatory authority.
For guidance, refer to FAA AC 91-21.1 (latest revision), Transport Canada
CARs 703.38(3), 704.33(5), and 705.40(4), or the EASA JAA TGL No. 29 -
Guidance Concerning the Use of Portable Electronic Devices Onboard Aircraft.
Honeywell Qualification Test Procedure, Aircraft Systems Susceptibility to
Transmitting Portable Electronic Devices (TS-1110-50373), or equivalent, may
be used to support applications for operational approval with the appropriate
regulatory authorities.
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Aspire-200
23-15-45
Page 4-5
28 Feb 2018
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