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
APPENDIX A – ENVIRONMENTAL CHARACTERISTICS
1. RTCA/DO-160G Environmental Characteristics
A. Modman
The following characteristics are taken from the core equipment qualification program and do not
reflect any additional qualification conducted on a per installation basis.
CategoryConditionSection
A1(V)Temperature and altitude4
NOTE: Below 5˚F (-15˚C), user services are not offered. Altitude for all units extended to 55,000
feet (16,764 m) during the qualification test. Overpressure 28.9 PSI (199 kPa), Decompression
8,000 to 55,000 (75.25 to 9.12 kPa) in 15 seconds.
BTemperature variation5
BHumidity6
BOperational shocks and crash safety7
CAT S, CURVE B2Vibration8
X - not requiredExplosive atmosphere9
Y - not qualified for dripping
water
Waterproofness10
X - not requiredFluids specification11
X - not requiredSand and dust12
FFungus resistance13
X - not requiredSalt fog14
AMagnetic effect15
A (WF) HLPIPower input16
AVoltage spike17
KAudio frequency conducted susceptibility18
ZWInduced signal susceptibility19
RRRadio frequency susceptibility20
MEmissions of RF energy21
A2K2L3Lightning induced transient susceptibility22
X - not requiredLightning direct effects23
X - not requiredIcing24
AElectrostatic discharge25
C - covers 14 CFR 25.853Fire, flammability26
Page A-1
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