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
CategoryConditionSection
BHumidity6
E and BOperational shocks and crash safety7
CAT R, CURVE E
CAT R, CURVE E1
Vibration8
NOTE: The sinusoidal sweep rate not to exceed 0.5 octaves/minute.
EExplosive atmosphere9
Y and RWaterproofness10
FFluid susceptibility11
NOTE: De-ice Ethylene Glycol, Hydraulic fluid phosphate ester AS1241 Type IV and V.
DSand and dust12
FFungus resistance13
SSalt fog14
ZMagnetic effect15
A (WF) HZPIPower input16
NOTE: Extended low frequency operation to 320 Hz.
NOTE: Power factor – leading greater than 0.98.
A (modified to 1,000 volts)Voltage spike17
KAudio frequency conducted susceptibility18
NOTE: RMS amplitude of the audio signal extended to not less than 10% of the maximum normal
AC input voltage and with a power source frequency of 320 Hz in addition to 360 Hz and 800
Hz.
CWInduced signal susceptibility19
NOTE: Extended low frequency operation to 320 Hz.
NOTE: With current and distance modified to 50 A at a distance of 0.4 inch (10 mm) for section
19.3.1.
RYRadio frequency susceptibility20
NOTE:
- 0.4 to 8 GHz: 150 V/m (Pulse repetition frequency of 1 kHz and a duty cycle of 1%, switched
on and off at a 1 Hz rate and 50% duty cycle). Pulse width is 10 µsec (1% of 1 kHz).
- 0.3 to 6 GHz: 20 V, (Pulse repetition frequency of 200 Hz and a duty cycle of 12.5%). Pulse
width is 625 µsec (12.5% of 200 Hz).
Page A-3
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