Epstein Secrets

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or lat

f primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electronics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VOR/DME systems in accordance with manufacture's Installation and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or la

f primary system components. The heart of the system is the ST 3100 ASE Transceiver, which includes internal electronics to support operation in the Iridium satellite network. Other system components include the externally mounted antenna, a low loss coaxial cable, and various user interfaces including

ics Suite Air Data Computer: Dual Air Data Computers Attitude Heading Reference System: Dual Litef LCR-92s AHRS Automatic Direction Finder: Single Collins ADF-462 ADF Receiver Cockpit Voice Recorder: Universal CVR--I20 Communications: Dual Collins VHF-22a VHF Radios Distance Measuring Equipment: Dual

ning Detection System Weather Radar: Honeywell Primus Wu-880 Weather Radar XM Graphical Weather: Garin Gdl-69 XM Weather Receiver Communications - Iridium Phone System Passenger Addressing System Entertainment - XM Satellite Radio Additional Features Dual Retractable Steps Pulse Light System Led Rec