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
Table 6-1. L1, L2 and L3 Codes (Cont)
Repair actionLog type
L3L2L1
DescriptionCode
Descrip-
tion
Code
Descrip-
tion
Code
Check A429 signal
from source
Critical FaultsSSM FW4
Body Pitch
Acceleration
50
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FW4
Body Roll
Acceleration
51
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Check A429 signal
from source
Critical FaultsSSM FW4
Body Yaw
Acceleration
52
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Status
Message
SSM NO
(Normal
Operation)
5
Pitch Angle
Label
1
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Status
Message
SSM NO
(Normal
Operation)
5
Roll Angle
Label
2
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Status
Message
SSM NO
(Normal
Operation)
5
Pitch Rate
Label
3
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Status
Message
SSM NO
(Normal
Operation)
5
Roll Rate
Label
4
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Status
Message
SSM NO
(Normal
Operation)
5
Yaw Rate
Label
5
IRU Input
Bus/
Aircraft
State Input
Bus
70/71
Page 6-67
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