Epstein Secrets

SITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS- ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF" INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

airplane is modified by the installation of a single Eventide Avionics Argus 5000/CE Moving Map Display receiving navigation inputs from the No. 1 UNS-1D Flight Management System (FMS) in accordance with manufacture's Installation Manual No. sop Revision 03.07, dated July 10, 1995 or later approved revision and FAA Form 337,

OSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS-ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF' INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

r the FAA approval of the new flight manual supplement on N908JE under Banyan Air Servive, Avionics Division work order #68062. A. Removed existing UNS-1D Flight Management System (FMS) control display/computer units and routed to the manufacture for upgrade to UNS-1D+. Reinstalled UNS-1D+ FMS CDU computers. System ground che

ER AIRCRAFT EQUIPMENT. NO WIRING OR STRUCTURAL ALTERATIONS WERE ACCOMPLISHED. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER HONEYWELL MST67A MODE S TRANSPONDER SYSTEM MANUAL 006-00681-0006 WITH NO DISCREPANCIES. AN EMI TEST, REPORT NO.: G2B-20895-080 WAS CONDUCTED AND THE INSTALLE

SW« r..4./rtu,34..• Al 2EA de a4.- Gulfstream sik.d•e!: G1159 (GE) G1159B (GM) G1159A (GBI) Installation of a dual Universal Avionics Systems UNS-1D Flight Management System with Global Positioning System in accordsnr-P with Jet Aviation Associates' Master Drawing List, MDL98001, Rev A, dated March 11, 1999, or later FAA