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29 January, 2020 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 TRANSMITTAL INFORMATION TO HOLDERS OF ASPIRE-400 SDIM, ATA NO. 23-15-49 (PUB. NO. D201902000020), ISSUED FOR USE IN SUPPORT OF THE FOLLOWING: Table TI-1 shows the applicable components. Table TI-1. Applicable Components...
Scope This manual provides detailed information for avionics technicians about the wiring, installation, and setup of every component of the Aspire-400. The installer is responsible for the approval and certification of system components on the aircraft, and for the installation of wiring in the aircraft. This manual includes information for end users about how to operate the Aspire-400.
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Reporting System), Cockpit voice, Position Reporting and AIS Electronic Flight Bag services. A second channel for cabin voice and data services. The Aspire-400 contains three main components, the HPA, the SDU, and the SCM. The Aspire 400 system consists of three main components, the High Power Amplifier (HPA), the Satellite Data Unit (SDU) and the SDU Configuration Module (SCM).
SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ASPIRE-400 Electrical Installation (TASK 23-15-49) General The Electrical System for the Aspire-400 consists of three main components, the HPA, SCM and SDU, with the SDU acting as a central hub for the other two. HPA Installation Power Requirements The HPA system runs on 115 VAC with a maximum power consumption of 280 W and has a maximum power dissipation of 240 W.