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
- Use of external Modem.
- Ethernet port selections and addresses.
- Mapping of VLAN ID versus Modman port.
(1) A429 Bus Labels
ARINC429 labels are required for antenna pointing and should be provided by the aircraft
Inertial Reference System (IRS).
In some cases labels may required from an alternative bus connected to an Multi Mode
Receiver (MMR) or other equipment.
Reference NumberManufacturer
IRS
Multi Mode Receiver (MMR)
(if applicable)
(a) Enter the IRS reference number (refer to IRS).
The IRS must always use a high speed bus but the MMR or other device may use
high or low speed bus. This is selectable.
The manufacturer and part number of the IRS is mandatory, ideally the transmission
rate and nominal latency should be provided.
NOTE: If the ARINC 429 labels pass through a data concentrator (RDC, ...
etc) the latency of this unit must be included.
The following table provides a guide for compatible IRS Numbers for each aircraft
type. The selection is based on the Aircraft make and model.
(b) Complete section 1.2, enter the Min Transmission Rate (Hz) and Total Nominal
Latency [sensor reading to KANDU] (ms) for the following labels (as appropriate):
Table D-1. Primary Labels
UTC Time150
UTC Time Fine140
Date260
Present Position – Latitude254
Present Position – Longitude255
Altitude261
True Heading132
Pitch Angle324
Roll Angle325
Pitch rate326
Page D-8
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