Epstein Secrets

. Dry Weight: 885 lb PERFORMANCE RATINGS: T-O Power Rating: 16.46 kN (3,700 Ib) Bypass Ratio: 2.80

8.33 spacing Dual RNZ 850Nays Dual DF 850 ADF Dual DM 850 DME Dual KHF 950 HF Honeywell LSZ-850 Stormscope Honeywell SPZ 8000 Flight Director Dual Honeywell FMZ-2000 w 5.2 software and & dual GPS. Honeywell Primus 880 Dual Honeywell FZ-800 FGC Five tube EFIS Features: Exxon Mobil previous owner TCAS

in Rolls Royce Corporate Care Program Auxiliary Power Unit (APU) SIN P-I27: 5543 TT (Not enrolled in M

94D Mode S Transponder Mode Dual Collins RTU-4280 Radio Freq Mgt Dual Honeywell IC-800E Integrated Avionics Dual Honeywell HG-2021 12 Channel GPS Dual Honeywell NZ-2000 FMS B&D Instruments 91005-0031112 FDR Honeywell DL-950 Data Loader Additional Equipment: Allied Signal Mark V EGPWS with RAAS / TCAS II w

rash Compactor Removable Cabin Curtain Divider Power Accordion Shades hird Crew Member Seat Single 6

DME's Dual Collins TDR-94D Mode S Transponders Enhanced Flight ID (7 of 8 DAPS) Honeywell Primus 880 Weather Radar Honeywell DL-900 Data Loader Dual Honeywell IC800E FMS Dual Honeywell GPS HG2021 Sensor Dual Honeywell CD-810 FMS CDU's Triple Honeywell LaserRef III IRS Honeywell CG 1227 Mode Selector Uni

Cycles Since New Serial Number 16228 AUXILIARY POWER UNIT: Garrett (Honeywell) GTCP36-100G Honeywell

ning System • Honeywell TCAS-z000 Traffic Collision Avoidance System With Change 7 • Triple Honeywell Laseref II IRS Inertial Reference Units • Dual Honeywell FMZ-2000 FMS Flight Management Systems With Dual 12-Channel GPS Global Positioning System 6.oA Software And CD-82o Displays Dual Motion Industries

ctive Action Send Win Gallery. PS-855A Emergency Power supply battery. and Grimes emergency tght power s

NTATION SYSTEM: Honeywell ED-800 EFIS System EMERGENCY LOCATOR TRANSMITTER: Artex C406-N ELT with Nav Interface FLIGHT CONTROL SYSTEM / AUTOPILOT: Dual Honeywell FZ-706 Flight Control Computers FLIGHT MANAGEMENT SYSTEM: Universal UNS-IFw GLOBAL POSITIONING SYSTEM: Universal UNS-IFw WAAS/LPV MULTI-FUNCTION

el selector valves, (xi) current on the Sikorsky "Power Assurance Program" with respect to the three gea

ENTATION SYSTEM: Honeywell ED-800 EFIS System EMERGENCY LOCATOR TRANSMITTER: Artex G40644 ELT with Nav Interface FLIGHT CONTROL SYSTEM / AUTOPILOT: Dual Honeywell FZ-706 Flight Control Computers FLIGHT MANAGEMENT SYSTEM: Universal UNS-1 Fw GLOBAL POSITIONING SYSTEM: Universal UNS-1Fw WAAS/LPV MULTI-FUNCTION

K-C Aviation,Inc electrical drawings: Electrical Power Distribution (Galley Power), GIV-24-1085-100 (Sh

its previously installed per STC #SA3774NM. Flight Manual Supplement Numbers 08015014 and 08015015 "Original" Revisions dated 07/18/91 for FMS-3 and Dual Honeywell Global Positioning Sensor System were removed from the Airplane Flight Manual. Installed provisions for a third Honeywell NZ-2000 Flight Management