Embraer Legacy 600 for sale

Embraer Legacy 600

For Sale

US$ 8,250,000

Year: 2007 | TTAF: 1620

Elegant 13 passengers cabin interior. Features forward 4 seats, mid cabin 4 place dining group seats and aft cabin 3 seats divan facing 2 opposite seats.

 

Specifications:

 

Airframe

  • Aircraft Manufacturer Embraer
  • Aircraft Type Legacy 600
  • Current Registration TBA
  • Serial Number 1450-TBA
  • Year of Manufacture 2007
  • Year of Delivery 2007
  • Airframe Total Hours* 1'620
  • Airframe Total Cycles* 681
  • Certification EASA
  • Navigation & Compliances RVSM CAT II

 

Engines

  • Manufacturer Rolls-Royce
  • Type AE3007A1E
  • Thrust Level (Lbf) 8'917
  • #1 Engine Total Hours 1'620
  • #2 Engine Total Hours 1'620
  • Engines Program RRCC(1)

APU

  • Manufacturer Hamilton Sundstrand
  • Type APS500R(2)
  • APU Total Hours 1'900
    • *as of November 2016
    • (1) Rolls-Royce Corporate Care
    • (2) With APU Silencer

 

Performance

  • Maximum Speed 455 Kts
  • Engines (x2) RRAE 3007A1E
  • Long Range Speed 424 Kts Thrust Level
  • Seats Full Range 3'091 Nm in Pound Force (each) 8'895 Lbf
  • Take-Off Runway Length 5'551 ft
  • Consumption  (Gallons per Hour) 363 (FAR135) 2'417 ft Passenger Configuration 13 Seats Steep Approach Capable Cabin Volume 1'656 Cu.ft (London City) Yes Luggage Volume 286 Cu.ft Maximum Operating Altitude 41’000 ft

Weights

LBS KG

  • Maximum Take-Off (MTOW) 22'500 49'604
  • Maximum Landing (MLW) 18'500 40'785
  • Maximum Zero Fuel (MZFW) 16'000 35'274
  • Maximum Payload 2'355 5'139
  • Payload - Full Fuel 684 1'507
  • Maximum Usable Fuel 8'242 18'170

 

AVIONICS

Simplicity and safety drive the Legacy 600 avionics system. The Traffic Collision and Avoidance System (TCAS) and Enhanced Ground Proximity Warning System (EGPWS) with wind-shear detector and escape guidance provide maximum safety against Controlled Flight Into Terrain (CFIT) and other air traffic threats.

VNAV is the functionality that provides to the aircraft the ability to fly a vertical navigation. VNAV computes guidance commands for the Autopilot or Flight Director follow the vertical guidance.

The flight profile reflects all speed and altitude restrictions specified in the flight plan while respecting airplane operating limits.

Required Navigation Performance (RNP 0.3) is a key component of next-generation performance-based navigation system. It utilizes global positioning and inertial reference system navigation, allowing aircraft to fly predetermined paths loaded in their flight management computers.

Note: Coupled VNAV, RNP 0.3 and Charts and Maps functionalities are follow-on certification items which may not be available at the delivery.

The reversion capability of the IC’s allows the all-glass, five Liquid Crystal Display (LCD) cockpit to be dispatched with one display inoperative.

AVIONICS

Type of Unit Qty Unit Description

  • Cockpit Equipment Single Honeywell Primus 1000
  • 8” X 7” displays Quintuple 2 PFD, 2MFD, and 1 EICAS
  • Communication System Dual Integrated VHF/ mode S diversity transponder with 8.33 kHz frequency spacing
  • Navigation Systems Dual NAV/ADF/DME
  • EGPWS Single Wind Shear Detector and Escape Guidance
  • Weather Radar Dual Control Panels and Turbulence Detection TCAS 2000
  • HF System Single With Second HF
  • CAT I and CAT II Single Autopilot/flight director
  • CMU Single With 3rd VHF
  • ELT Single Emergency Locator Transmitter
  • CVR Single Solid State Cockpit Voice Recorder
  • FDR Single Solid State Flight Data Recorder
  • ISIS Single Integrated Stand-by Instruments System
  • CMC Single Central Maintenance Computer
  • IRS Dual Inertial Reference System
  • RMU Dual Radio Management Units

 

CABIN

SUMMARY

  • 13 Seats Configuration
  • Length 49’8” ft/in
  • Height 6’0” ft/in
  • Width 6’9” ft/in
  • Volume 1'656 Cu. ft
  • Bagage volume 240 Cu. ft
  • Nb of standard baggages 47

 

DESCRIPTION

The interior arrangement provides accommodation for two pilots and one lf ight observerin the cockpit, and 13 passengers in the cabin.

A forward full service galley and crew lavatory are situated between the cockpit and the cabin.

The cabin is divided into forward, mid and aft compartments and at the rear of the aircraft is a vanity room / lavatory which also provides cabin access to the baggage compartment. (Source: Embraer)

 

CABIN

OVERVIEW

Cabin Description:

  • 􀁸 13 Passengers Configuration
  • 􀁸 Forward Lavatory
  • 􀁸 Flight Attendant Seat with Intercom System
  • 􀁸 Leg Rests
  • 􀁸 Provisions for Extended Over-Water Operations
  • 􀁸 Cockpit jumpseat
  • Entertainment:
  • 􀁸Two Bulkhead Mounted Monitors
  • Two CD/DVD Players
  • 􀁸 Moving Map - Airshow 4000
  • 􀁸 Newly installed WiFi system: internet speed - 432kbps, service: Swift Broadband
  • 􀁸 Water Heater
  • Utility:
  • 􀁸 Airshow 4000 Next-Generation w/multimedia inflight mapping
  • 􀁸 Dual 15-inch flat-screen monitor
  • s 􀁸 DVD/CD/MP3 multiregion
  • , 􀁸 Dual 18-inch flat LCD displays
  • Storage: 􀁸 In Flight Phone System – ST3100 Iridium
  • 􀁸 Mid-Cabin Partition Curtain
  • 􀁸 VIP Panel
  • 􀁸 Additional VIP Control
  • 􀁸 Life Raft
  • 􀁸 AC Power Outlets to all Cabin Zones including a 110 VAC Power Outlet in the Credenza Toe Kick Area
  • Galley:
  • 􀁸 Water Heater System (for Galley and Lav.)
  • 􀁸 Convection / Microwave Oven

 This specification is subject to changes without prior notification, specification subject to verification by purchaser.
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