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
Electrically wire and interconnect in
accordance with Figure 3-9 and Figure
3-12.
Electrical
wiring
Install location of KANDU is airframe
specific.
The KANDU is installed inside a
pressurized location, the KANDU to
BUC-HPA and KANDU to FMA
interconnect are routed through a
Bulkhead Interface connectors.
Mounting
Refer to JetWave™ MCS-8562 Terminal
Internal LRU Installation, KANDU.
Electrical
Wiring
KANDU-FMA
Electrically bond, refer to KANDU.Electrical
bonding
KANDU bonding to the aircraft must be
achieved through the mounting structure
(fasteners) and KANDU A3J1-A.
The bulkhead interface connectors
should be electrically bonded to the
aircraft.
Examine for physical damage.PhysicalBUC-HPA
Environmental conditions, refer to Figure
3-10.
Install the thermal pad in accordance
with BUC-HPA .
The BUC-HPA is installed with the FMA,
Refer to FMA Installation Procedure.
The BUC-HPA feet are configured
differently depending on the part
number ordered. Make sure feet are in
the correct configuration for the aircraft
application.
Make sure the waveguide is connected
before powering the BUC-HPA.
Waveguide
Page C-3
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