Epstein Secrets

GATION AND COMPLIANCE • Auto-brake • CPDLC • ADS B version 2 13 EFTA00793175 :117,m? ti)k - AVIONICS EFIS (Electronic Flight instrument) Four Honeywell Large 14" adaptive LCD displays FMS (Flight management system) Triplex Honeywell NEXTGEN IRS (Inertial Reference system) Triple Honeywell LASEREF V

Triple Honeywell VHF Receivers 8,33 kHz spacing VDL mode A and mode 2 capabilities HF COM (High Freq. Com) Dual With SELCAL SATCOM (Satellite com) Single Honeywell MCS-7210 INMARSAT satellite communication system Aircell axxess II iridium satellite communication system RADAR Single RDR-4000 3-D Weather radar

nters EFTA00595504 2002 Gulfstream IV-SP Serial Number TBA page 2 AVIONICS • FMS Dual Honeywell NZ-2000 Flight Management Computer • EFIS Honeywell SPZ-8400 • EGPWS Allied Signal, Enhanced with RAAS • TCAS Single Honeywell TCAS 2000/7 • LRN Honeywell LASERTRAK • GPS Dual Honeywell HG-

IONICS • FMS Dual Honeywell NZ-2000 Flight Management Computer • EFIS Honeywell SPZ-8400 • EGPWS Allied Signal, Enhanced with RAAS • TCAS Single Honeywell TCAS 2000/7 • LRN Honeywell LASERTRAK • GPS Dual Honeywell HG-2021 • DME Dual Collins DME-422 • AFIS DMU w/Cockpit Printer • HF Comm D

e Bulletin 504 to Part Number 822-9210-308 (Enhanced Surveillance) Serial Numbers ICBM and 4J2W. Interfaced the TDR.940 to the Number 1 and Number 2 Honeywell HGT1075AE03 Inertial Reference Systems and made additional voting changes per CE Avionics, Inc. Drawing Number 5893B-t. Revision UR dated March 22,

88. Installed a third Honeywell Inertial Reference System (IRS), a third Honeywell Flight Management System, NZ910 Navigation Computers (3), and a Single Honeywell VLF/OMEGA Sensor in accordance with data approved by STC SA3774NM. Flight Manual supplements provided and Equipment List revised. Aircraft weight

acent to the TCAS control stating: 'TCAS INOP PENDING STC APPROVAL- has been removed. Gylfstream Aerospace Ground Test Plan/ReponittSC41 129602 for Honeywell (TCAS) Systems has been accomplished to verily the installation and operation of tee systems as installed in this aircraft; test results have been

ted September 7, 1989 regarding installation of a third Honeywell Flight Management System, a third Honeywell Inertial Reference System (IRS) and a Single Honeywell VLF/OMEGA Sensor as previously installed per Western Commander, Inc. (WCI) Supplemental Type Certificate SA3T74NM. Previous installations approved