Epstein Secrets

RCENT CHANGE Change Last Quarter: -2.38% Change Last Year: -2.38% Change Since New: -45.91% Price When New: $37,900,000 BASE PRICE INCLUDES Honeywell SPZ-8500 avionics with six tube EFIS, Satcom, HUD, RVSM, TAWS A, TCAS II, CorporateCare, like new P&I. PERFORMANCE & SPECS Config Twn, fanjet Mx

ft 6in Length 96ft 5in Height 25ft 10in MARKET DATA & RECENT ADS Interior prices can impact values by more than $1m. Priced with CorporateCare. Rolls-Royce at 703-621- 2752 for hourly engine rates. ADs = 05-16-14 floor heat; 06-11-03 damper shafts; 06-18-08 tires; 06-18- 13 wiring; 07-12-25 water drain;

rmation. A general summary of this aircraft's next generation, Honeywell Primus Epic avionics suite is as follows • PlaneViewTM Avionics Suite • Honeywell Head Up Display / Visual Guidance System • Enhanced Vision System (EVS) Airborne Flight Information System (AFIS)with Satellite Communications Lin

Airframe: 5948 Hours 2134 Landings Engines: Rolls-Royce BR710 C4-11 Left and Right: 5948 Hours Left and Right: 2134 Cycles Engines enrolled on Rolls-Royce CorporateCare program APU: Honeywell RE220 Total Time: 5345 Hours APU enrolled on Honeywell MSP program Interior: Dual CD and DVD Players Airsh

ic with FM Immunity • Radio Altimeter: Dual Honeywell RT 300 • RMI BF Goodrich EBDI 4000 • SATCOM: Honeywell MCS 7000 7 Channel • Stormscope: Honeywell LZS 860 with tail antenna • TAWS: Dual Honeywell EGPWS • TCAS: Honeywell TCAS 2000 with change 7 • Transponder. Honeywell Primus II Epic Mode S

2009 Status March 2015 Airframe Total Time 1235:58 511 Engines BR710C4-11 LH 1235:58 511 BR710C4-11 RH 1235:58 511 Engines enrolled with Rolls-Royce CCA APU Honeywell RE-220 SN P560 TT 1586 APU enrolled with Honeywell MSP Plan - i - EFTA00605157 Brief Introduction for Key System Component

ic with FM Immunity • Radio Altimeter: Dual Honeywell RT 300 • RMI BF Goodrich EBDI 4000 • SATCOM: Honeywell MCS 7000 7 Channel • Stormscope: Honeywell LZS 860 with tail antenna • TAWS: Dual Honeywell EGPWS • TCAS: Honeywell TCAS 2000 with change 7 • Transponder: Honeywell Primus II Epic Mode S

y 2009 Status 28 Sep 2015 Airframe Total Time 1338.2 545 Engines BR710C4-11 LH 1338.2 545 BR710C4-11 RH 1338.2 545 Engines enrolled with Rolls-Royce CCA APU Honeywell RE-220 Tr 1760.0 APU enrolled with Honeywell MSP Plan - - EFTA_R1_00017425 EFTA01735335 Brief Introduction for Key System

's next generation, Honeywell Primus Epic avionics suite is as follows=u> EFTA_R1_01908066 EFTA02660449 • PlaneViewTM Avionics Suite</=> • Honeywell Head Up Display / Visual Gui=ance System • Enhanced Vision System (EVS) Airborne =light Information System (AFIS)with Satellite Communications Li

Airframe: 5948 Hours 2134 Landings Engines: Rolls-Royce =R710 C4-11 Left and Right: 5948 Hours Left and Right: 2134 Cycles =ngines enrolled on Rolls-Royce CorporateCare program APU: Honeywell RE220 Total Time: 5345 Hours =PU enrolled on Honeywell MSP program Interior: Dual CD and DVD Players Airsh

al summary of this aircraft's next generation, Honeywell Primus Epic avionics suite is as follows=u> • =nbsp; PlaneViewTM Avionics Suite • =nbsp; Honeywell Head Up Display / Visual Guidance =ystem • =nbsp; Enhanced Vision System (EVS) Airborne Flight=Information System (AFIS)with Satellite Communicati

Airframe: 5948 Hours 2134 Landings Engines: Rolls-Royc= BR710 C4-11 Left and Right: 5948 Hours Left and Right: 2134 Cycles =ngines enrolled on Rolls-Royce CorporateCare program APU: Honeywell RE220 Total Time: 5345 Hours =PU enrolled on Honeywell MSP program > Interior: Dual CD and DVD Players Ai

Sump Heater- EFF: APU SN#s APU I Replace before P-4 I 4 957863 SB RE220-49-7863 Replace APU I Electronic Control Unit EFF: Before SN# P- 421. Honeywell recommends that this bulletin be accomplished at first return for any cause. at a Honeywell authorized ovhltrepair facility. SB RE220-49-7890

sion 3 of this Non- Modification Service Bulletin has been issued to delete the requirement to return the removed fuel pump splined coupling to Rolls-Royce Deutschland. Service Enginesting.P/N BRR52639. See s/b for due time requirement. Cancelled See code 72 GAC LTN CAN CPN BMX000258 3029.7

09 C EASA AD 0.00 2006-0286 R1 AD 992704 AD 2007.07.12 Honeywell Nav Computer Airframe NOTE: Due with 14 days of &0711 Applicable to all Honeywell NZ-2000 Navigation Computers and all IC-800 Integrated Avionics Computers If Reference: Honeywell Technical Newsletter A23-6111.008. Revision

n // Within 4 months after the effective date of this AD accomplish touch- and-go and overshoot calculations per the instructions as defined by Rolls-Royce Deutschland Alert NMSB-BR700.72- A900504 Revision 'paragraph 3.B game tab MAN CM 1145.2 362 05 May 2010 C 0.00 AD 993053 EASA AD2010-007