Users Manual Part 3
Table Of Contents
- 3. System Fails Post-Installation Checks
- 4. Incorrect Navigation Data
- 5. System Will Not Connect to the Network
- 6. Connectivity of Each Ethernet Port
- SECTION 7 – MAINTENANCE AND REPAIR
- 1. Maintenance Requirements
- 2. Continued Airworthiness, FAR 25.1529
- 3. Airworthiness Limitations
- 4. General Instructions for Inspection
- 5. Electrical and Mechanical Inspection and Check
- 6. Instructions for Continued Airworthiness
- 7. Visual Inspection and Check
- 8. Scheduled Maintenance and Inspections
- 9. Unscheduled Maintenance
- 10. Repair Requirements
- APPENDIX A – ENVIRONMENTAL CHARACTERISTICS
- APPENDIX B – INFORMATION SHEETS
- 1. Aircraft Information Sheet
- 2. JetWave™ MCS-8562 Terminal AES Subsystem Components
- A. JetWave™ MCS-8562 Terminal AES OAE - FMA Installation Information Sheet
- B. JetWave™ MCS-8562 Terminal AES KANDU Installation Information Sheet
- C. JetWave™ MCS-8562 Terminal AES BUC-HPA Installation Information Sheet
- D. JetWave™ MCS-8562 Terminal AES Modman Installation Information Sheet
- E. JetWave™ MCS-8562 Terminal AES APM Installation Information Sheet
- APPENDIX C – CHECKLISTS
- APPENDIX D – CUSTOMER PORTAL
- 1. Customer Portal
- 2. APM Request Form
- A. Requester Name
- B. Requester Email
- C. Honeywell Representative Name
- D. Hon Representative Email
- E. PO Number
- F. DP/VAR/Customer Name
- G. DP/VAR/Customer Name Contact Name
- H. DP/VAR/Customer Name Contact Email
- I. Channel Partner/Integrator/STC
- J. Estimated APM Due Date
- K. Aircraft Make / Aircraft Model
- L. Aircraft Model Variant
- M. Additional Notes/Comments
- 3. APM Parameter File
- 4. Request Assistance
Value√NAItemParameterSection
Minimum 1 inch (25.4 mm) from top
surface and 0.5 inch (12.7 mm) from all
other surfaces.
Clearance
ARINC 600 mating connector and pins,
refer to Table 3-2 ARINC 600
Connectors.
Electrical
connector
ARINC 600 polarized pins.
Bonding, refer to Modman.Electrical
bonding
Electrically wire and interconnect in
accordance with Figure 3-6 or Figure
3-7 and Figure 3-12.
Electrical
wiring
Equalizer in the TX path.Electrical RF
coaxial
TX path loss, refer to Table 3-4 Modman
Cable Loss Values.
Attenuator in the RX path.
RX path loss, refer to Table 3-4
Modman Cable Loss Values.
Examine for physical damage.PhysicalAPM
Environmental conditions, refer to Figure
3-8.
Can be installed in any orientation.
Refer to Figure 3-8.
Mounting
Use 0.164-32 UNC-2A corrosion
resistant mounting fasteners.
Do not exceed 25 in-lb (2.8 Nm) when
you torque the screws.
Electrically bond, refer to APM.Electrical
bonding
Electrically wire and interconnect in
accordance with Figure 3-12.
Electrical
wiring
APM to Modman interconnect cable
shall use ARINC 664 compliant 2
Shielded Twisted Pair 24 AWG (or
Aerospace Grade Shielded Cat 5/Cat
5E Minimum). Part No. ECS 922404 or
Equivalent, with a maximum length of
9.8 feet (3 m).
Examine for physical damage.PhysicalKANDU
Environmental conditions, refer to Figure
3-9.
Page C-2
23-15-84
EFFECTIVITY
ALL
11 Nov 2020
© Honeywell International Inc. Do not copy without express permission of Honeywell.
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
JetWave™ MCS-8562 Terminal