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
B. APM
CategoryConditionSection
A1(V)Temperature and altitude4
NOTE: Altitude test extended to 50,000 feet (15,240 m). Overpressure 28.9 PSI (199 kPa),
Decompression 6,000 to 55,000 (1828.8 to 16,764 m) in 2 seconds.
BTemperature variation5
BHumidity6
BOperational shocks and crash safety7
CAT S, CURVE B2Vibration8
X - not requiredExplosive atmosphere9
YWaterproofness10
X - not requiredFluid susceptibility11
X - not requiredSand and dust12
FFungus resistance13
X - not requiredSalt fog14
AMagnetic effect15
X - not requiredPower input16
X - not requiredVoltage spike17
X - not requiredAudio frequency conducted susceptibility18
ZCInduced signal susceptibility19
RRRadio frequency susceptibility20
MEmissions of RF energy21
A2K2L3Lightning induced transient susceptibility22
NOTE: Modified to extend single stroke to waveform 3 level 3 and multi-stroke to waveform 4
level 2.
X - not requiredLightning direct effects23
X - not requiredIcing24
AElectrostatic discharge25
C - covers 14 CFR 25Fire, flammability26
C. KANDU
CategoryConditionSection
D2Temperature and altitude4
NOTE: Altitude test extended to 51,000 feet (15,544.8 m). Overpressure 28.9 PSI (199 kPa),
Decompression 6,000 to 55,000 (1,828.8 to 16,764.0 m).
ATemperature variation5
Page A-2
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