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
Connection must be WR28 for TX and
coaxial cable for RX.
Waveguide -
BUC-HPA to
FMA
The TX interconnect path loss.
The RX interconnect path loss.
RX connection at the BUC-HPA requires
a WR42 to coax transition adapter at
the BUC-HPA J4.
Electrically wire and interconnect in
accordance with outline drawing Figure
3-10 and interconnect drawing Figure
3-12.
Electrical
wiring
Electrically bond, refer to BUC-HPA -
Thermal Conduction Path.
Electrical bonding
Examine the FMA AIM/LAIM for physical
damage.
PhysicalFMA Installation Proce-
dure
Examine the FMA assembly for physical
damage.
Examine the radome for physical
damage.
Environmental conditions, refer to Figure
3-11.
The aircraft fuselage mount OAE must
be mounted on the top of the fuselage.
Positioning
Refer to FMA Bonding .FMA AIM/
LAIM
Install and attach the radome skirt
fairing to fuselage.
Install radome
skirt fairing
Refer to FMA Installation Procedure .FMA Install
Attach the radome assembly onto the
AIM/LAIM/radome skirt fairing.
FMA radome
Electrically bond.FMA bonding
Automatic alignment, manual alignment,
or command, refer to FMA Alignment
and Inspection of Waveguide.
FMA alignment
Page C-4
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