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
(6) ARINC TX Mute Wiring
(a) Select option in column B to indicate if ARINCTXMUTE and/or FMAMUTE are
wired.
Removal of FMAMUTE requires a safety analysis to be performed to confirm this
is acceptable
ARINCTXMUTE if wired connects MP12E MODMAN to J1C on KANDU
(7) OAE Blockage
The Outside Antenna Equipment (OAE) Blockage Parameters are applicable to the FMA
antenna type.
Radiation from the antenna may be blocked by the airframe in certain directions, dependent
on the aircraft type and the location of the antenna. The antenna must mute the transmitter
when airframe scattering leads to non-compliant radiation.
The (OAE) Blockage Parameters are pre-populated using a look up table for the aircraft
Make Model and Variant (specified in the Generic Tab). If the default parameters are
changed, they are indicated in yellow highlight.
Table D-2. Boeing 737-700 Example
Blockage degrees
1.2A
-3b
57.7C
47d
2.7e
17f
-g
16.9h
5.3i
0.4k
3.6m
-4.1p
If the aircraft Make Model and Variant is not specified or FMA antenna is not located in
the standard ARINC791 position, please calculate the blockage angles a to p as described
in ARINC791 Attachment 3.
(8) Mapping of VLAN ID versus Modman port. The user VLAN ID to Modman port mapping
need to be indicated as follows:
Page D-10
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