Embraer 135 BJ Legacy 600

Description

Currently Not Available 
Embraer 135 BJ (Business Jet) Legacy 600
Year 2006
Manufacturer EMBRAER
Model LEGACY 600
Condition Used
Total Time 4,280
Number of Seats 13
Location: United Arab Emirates

Airframe:
Total Hours: 4,280 Hours Since New
Total Landings: 1,580 Landings Since New (as of 2006)
Enrolled on JSSI Tip to Tail

Aircraft will be delivered FRESH Out of : 
LU6+12+24+48+48T96+48T192+72+144
NL/MLG O/H Scheduled maintenance inspection +A/C WEIGHING 

Engines
Rolls-Royce AE3007A1E/1P
Hours Since New:    4,186 Hrs 
Cycles Since New:   1,546 Cycle
Enrolled on Rolls-Royce Corporate Care

APU
Hamilton Sundstrand  APS500R/T-62T-40C14
4065Hrs	3902cycles

Airframe
4,185 Hours Since New / 1,546 Landings Since New (as of Aug, 2018)

Interior:
Forward right hand side galley, forward left hand side entertainment cabinet, forward left hand side crew Lavatory , and a rear Pax lavatory. Flat floor cabin , seating for 13 passengers (forward cabin zone: 2 single club seats; mid cabin zone: 2 double club seat on the left hand side and a credenza on the right hand side; aft cabin zone: one divan on the right hand side and Two single club seat on the left hand side and a mid cabin divider separating the divan zone.

Iridium ST-3100 and AEROCOM 1000 Interphone Systems with three (3) points of connection: one point of connection integrated with the crew headsets, one handset in the arm ledge of the RH forward facing seat of the forward cabin zone (FWD RH VIP seat) and one handset located in the arm ledge of the LH conference table.

Entertainment Equipment and Communications Systems consisting of: two (2) 15.1” wide screen monitors being one 15.1” wide screen LCD monitor at the forward left bulkhead and one 15.1” monitor at the aft right bulkhead; two (2) DVD’s; thirteen (13) headsets; stereo speaker system; ten (10) 115VAC power outlets including galley, cabin and lavatory; one SVGA port interfacing with the forward left hand side monitor.

High Speed Data System –Wireless technology (Wi-Fi) Consists of a Dual channel global high speed data solution using Swift 64 Immarsat aeronautical service with a global coverage reaching up to 128Kbps of data rate connecting the aircraft to internet plus a WLAN supported by an on board Hot Spot multi standard (a ,b &g)
Galley including: Microwave oven, coffee maker, 115VAC power outlet, sink with hot and cold water, storage boxes for drinks, work surface table, ice storage, thermos storage, galley control panel, trash container.

The aft lavatory incorporates a flush chemical toilet, sink with hot and cold water and one 110VAC power outlet, left hand side wardrobe and an access door to the baggage compartment.

Interior Options:

• High temperature oven
• Flight Attendant Seat with intercom handset integrated
• High Speed Data – HSD Additional 110V GFI outlet in the Credenza toe kick area
• Cockpit Seat with Sheepskin
• 2 Life rafts for EASA aircraft (JAR OPS-1 Compliance – 2 life rafts for 12 passengers)
• Mid Cabin Curtain Divider Separating the divan zone

Avionics:

• Five Tube 8” X 7: displays (2 PFD’s, 2 MFD’s, & 1 EICAS) w/ multi-reversionary e tube 8” x 7” displays (2 Primary Displays – PFD, 2 Multifunction Displays – MFD and 1 EICAS Display)
• Dual Integrated Computer encompassing the functions of display driving, dual Flight Director/single Autopilot and EICAS
• Dual Honeywell FMS + GPS System
• Dual RMU’s
• 1st & 2nd VHF Comms – 8.33 khz spacing (integrated VHF/Mode S Elementary & Enhanced Surveillance Transponder)
• Single Passenger Address & Cabin Interphone System
• Solid State CVR
• Solid State FDR
• Single Emergency Locater Transmitter
• EICAS
• Single Aural Warning Unit
• 33 / FM Immunity
• Dual Digital Clock
• Dual Air Data Computers RVSM compatible
• Integrated Stand-by Instrument System
• Dual IRS
• Single Radio Alt
• Dual VHF Navigation System (Integrated NAV / ADF / DME
• Single EGPWS / Wind Shear Detector and Escape Guidance
• Single Weather Radar w/ dual control panel and turbulence detection
• Single TCAS 2000
• CAT I & CAT II AP/FD
• Single Central Maintenance Computer (CMC)
• Dual Stall Protection System
• Single HF System
• Single SELCAL
• CMU w/ Third VHF (Honeywell)
• 2nd HF System
• The aircraft fulfills the following requirements:
• ACAS II (TCAS II with Change 7
• RVSM
• Mode S Enhanced Surveillance
• JAR-OPS 1
• IFR Car. I & II
• NAT-MNPS
• P-RNAV
• RNP-5
• RNP-10
• BRNAV
• FM Immunity & 8.33 KHz Spacing radio