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Embraer Legacy 650
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| | YEAR:............... | 2010 |
| | REGISTRATION: |
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| | AIRFRAME TOT | 145 |
| | ENGINE TIME(S) | 145 TSNEW |
| | | 145 TSNEW |
| | LOCATION: | Maryland, United States |
EXTERIOR:
New paint, never flown.
INTERIOR:
The cabin is configured for 13 passengers (LOPA A) in a three zone arrangement. The forward zone features four seats in club configuration with a central isle. The mid cabin zone includes a double club configuration opposite a credenza. The aft cabin includes a three seat, fully berthable divan, opposite a single club arrangement of two seats. The rear cabin is separated from the forward and mid cabin zones by a solid partition, with an optional acoustic curtain to separate the isle. For entertainment, dual CD/DVD players provide video through dual 17.5” HD monitors. The monitors are installed on the forward and aft bulkhead respectively. Audio is played through 6 cabin speakers, and 3 subwoofers. In addition to the single standard VIP cabin controller, a second controller is also included. Also installed is an Aircell Iridium ST-3100 satellite phone, with two handsets. Swift Broadband provides high-speed wireless internet throughout the cabin. A total of 14 A/C outlets are provided through out the galley, cabin, and lavatory. The galley consists of a microwave oven, as well as the additional convection oven, a refrigerator, and a “Nespresso” Brewer, and sink. Further Upgrades include a flight attendant seat, as well as a forward crew lavatory.
AVIONICS:
Honeywell Primus Elite Five 8X7” LCD Displays with EICAS
Electronic Flight Bag - CMC Electronics Pilot View Class II
FMS - Dual Honeywell 6.1
Auto Pilot - Honeywell IC-600
Data Loader - Honeywell DL-1000
Comms - Dual Honeywell RCZ-833
HF with Selcal - Dual Honeywell KHF-1050
Navs - Dual Honeywell RNZ-851
DME - Dual Honeywell RNZ-851
ADF - Dual Honeywell RNZ-851
ADC - Dual Honeywell AZ-950
Inertial Reference System - Dual Honeywell Laserref IV
ISIS - Thales
Radio Altimeter - Honeywell RT-300
EGPWS - Allied Signal MkV
TCAS II - TCAS 2000
Central Maintenance Computer - Vibrometer
Stall Protection System - Dual Goodrich sensor
Weather Radar - Honeywell WU-880 with turbulence
WAAS/LPV
Smart Runway / Smart Landing
XM Weather
SSFDR
SSCVR
EQUIPMENT:
Certified under FAA design criteria. The aircraft is also equipped with an Artex C-406-2 ELT, the FAA required 88 parameter FDR, two digital clocks, and two 115V power outlets located in the cockpit. Also located in the cockpit is the 3rd observer’s seat. The FMS is coupled with VNAV, and qualifies for RNP .3. The aircraft is approved for steep approaches, and operations into Cannes Airport. Also installed are Provisions for extended over-water operations. An optional 77 cubic foot Oxygen bottle is installed in addition to the standard 115 cubic foot bottle. An interphone system allows communication between the cockpit, galley, and cabin.
REMARKS:
Aircraft is scheduled to deliver in May of 2012.
PRICE: $
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