Users Manual Part 1

Table 1-6. FMA Leading Particulars (Cont)
SpecificationCharacteristic
No scheduled maintenance requiredMaintenance
P1 - Power from KANDU
P2 - Control interface from KANDU
P3 - IMU power and control from KANDU
J4 - RF RX to BUC-HPA
J5 - RF TX from BUC-HPA
Interfaces
2. Honeywell JetW
ave™ MCS-8562 Terminal Architecture
This section describes the AES system that Honeywell has implemented for the following classes of terminal:
- Class A aftermarket satellite terminal: For use on CAT types of aircraft. This uses a FMA assembly.
The terminal can also be used in the large aircraft segment of the BRS.
The JetWave™ MCS-8562 Terminal behaves in the same manner as the JW1.0 system in operation apart
from the responding to requests for different TX/RX polarization and/or frequency band switching as
commanded by the ACM based on the Inmarsat satellite topology.
The JetWave™ MCS-8562 Terminal wideband system also supports an optional external modem and is
capable of switching between the commercial bands and Non-Commercial bands of operation. The switch
between services is controlled by an external Modman discrete, GUI menu option and/or external SNMP
branch which will indicate to the terminal dynamically which mode of operation it should be in.
The external modem operates in a standalone mode of operation where modem parameters such as
satellite target longitude, beam polarity, frequency band etc are passed to the Modman by user entering
the parameters into the GUI.
Refer to Figure 1-2 for the JetWave™ MCS-8562 Terminal block diagram.
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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