飞行翻译_公务机_公务航空_Business Jet_Business Aviation

The antenna is steered by the antenna control unit to point a high gain beam in the direction of the desired satellite.
COMMUNICATION LINK SCHEMATIC
The following schematic depicts the interface between the various components as related to the Rockwell Collins SAT-6000, minus buyer furnished equipment. Example: PC data provision, FAX and analog phones.

Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2

The Cabin Communication System (CCS) provides a private automatic branch exchange switching network. This network routes voice and data communications to and from up to nine active devices (handsets/FAXs/modems/data link etc.) in the airplane and provides six air-to-ground channels. The systems includes connections of basic telephone/telecomputing equipment to UHF antenna and SATCOM links. In the event a data link device is installed on the airplane, the CCS has the capability to communicate with the data link device using an internal modem.
The digital radio components consist of: one UHF antenna, duplexer and one airborne radio telecommunication unit. The CCS plus all customer supplied handsets/FAXs/Modems is known as the Office-In-The-Sky (OITS). The system will interface with personal computers, cabin handsets and facsimile machines.

The digital handset is located in the flight compartment and has a backlit LCD display and telephone style keypad used to dial calls and select various options. A credit card reader (for optional billing) is built into the handset and a two-button increase/decrease volume control (side of handset) is also installed.
Refer to the Magnastar C-2000, G5000 ICG Aerocom A3000B and ICS-100 telephone system user guide for description/function and operation of the system.
Volume 2 Flight Crew Operating Manual Rev 12, Aug 14, 2006
The flight compartment printer is installed in the copilot’s side console. The printer has ARINC 429 and laser quality thermal printer/plotter that is capable of full format and graphic printing from CAIMS and DATALINK.

The printer can be used to print selected messages and weather data sent to it via the Airborne Data Link System (ADLS). The printer is also used by the Central Aircraft Information Maintenance System (CAIMS) to print out certain maintenance fault and status information. This is accomplished via the Portable Maintenance Access Terminal (PMAT).

PRINT MAINT REPORT Button . active fault reporting can be printed by pressing the button and a short report will be printed even if no faults are detected.
GF0610_071
The PMAT can be used to generate an active fault report to the printer by operating the “PRINT MAINT REPORT” button located on the left forward bulkhead in the flight compartment.
Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2 CSP 700.5000.6 06.10.39
The printer interfaces with a communication link to the Airborne Data Link System (ADLS) and a parallel interface from the PMAT.