User Manual Part 1

Page 1-10

16 Sep 2015

23-15-29

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

JetWave™ System

• It supplies the user interfaces to the aircraft and passengers as follows:

• The PODD interfaces provide service to the passengers through the use of Ethernet

(10/100/1000 Base T).

• The PIESD interfaces provide services to passenger entertainment devices installed on

the aircraft (in flight entertainment systems). This system uses Ethernet (10/100/1000

Base T).

• The AISD interfaces provide services to the aircraft/cockpit, such as the electronic flight

bag, data load, etc. This system uses Ethernet (10/100/1000 Base T) interfaces.

• The discrete I/O for aircraft status and for reporting system status.

• Has two LEDs to provide power and fault status on the front panel.

• Accepts 115 VAC from the aircraft.

• Manages the BIT for the complete AES.

• Contains the modem, which transmits and receives to/from the KRFU.

• Controls the KRFU and KANDU (and through it, the OAE) through the Ethernet interface and

RS-422 discretes.

E. APM

• The APM holds the configuration data for the system.

• Is powered by the Modman.

3. Honeywell Implementation

The Honeywell implementation varies from the ARINC 791 configuration as follows:

• No ARINC 629 support is provided (optional in ARINC 791).

• No EN1 Ethernet functionality between the KRFU and KANDU is provided (the provisioned

standard inter-wiring is not utilized).

• ARINC 429 TX mute between the Modman and the KANDU is not implemented (manufacturer

specific RS422 signaling is used instead).

• Manufacturer-specific circuits 1 to 6 carry a BUC Mute signal, a Filter Select signal, and an

KANDU Reset signal.

• The RSSI function is in the Modman.

• No EN2 Ethernet interface functionality between the KANDU and OAE on the TMA variant (the

provisioned standard inter-wiring is not utilized).

• There are LED indicators on the front panel of the Modman to show status.