Epstein Secrets

3 Honeywell TR-865A & NC-860A Comm w/ 8.33khz Spacing - 2 Honeywell NV-875A VOR/ILS/Marker Beacon Receivers - 2 Honeywell DF-855 ADF Receivers - 2 Collins HF-9034 HF Transceivers - 2 Honeywell DM-855 Receivers - 3 Honeywell Lazeref V Inertial Reference Units - 3 Honeywell AZ-200 Digital Air Data Syst

oice Recorder - Honeywell SSFDR Flight Data Recorder - 2 Honeywell XS-875A Mode S XPDR w/ Flight ID - ACSS TCAS 2000 w/Change 7.1 - Honeywell DMU Data Transfer Unit - 2 Honeywell CMA-4024 Global Position Sensors - Honeywell EGPWS EGP-100 w/ Windshear Alert & Peaks - Honeywell HDU - Honeywell Satellite Communi

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

red to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The EMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight direct

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

red to the other FMS such that both systems have GPS 1 and GPS 2 data as inputs. The FMS's receive air data parameters from an Air Data Computer. A Data Transfer Unit (DTU100) is used to load periodic navigation data base updates via zip disks. The systems provide navigation and steering data to the flight direct