2002 Embraer Legacy 600

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Aircraft Information

Make: Embraer
Country: United States
Model: Legacy 600
State/Province: Not provided
Year: 2002
City/Airport: Not provided

Serial No: 145637
Registration No: VP-CFB

Flight Time: 3890 hours
Engine Time: 3890 hours

Attached Files

Current Status Report

Description

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AIRFRAME:
Times Current as of 7/17/2014.
Total Hours: 3889.93
Total Landings: 1978
Gross Weight (Ramp): 49,758 lbs.
Max Takeoff Weight:49,604 lbs.
Fuel Capacity: 17,600 lbs

ENGINE 1
Total Hours: 3889.93
Total Cycles: 1978

ENGINE 2
Total Hours: 3889.93
Total Cycles: 1978

APU:
Hamilton Sundstrand APS 500R/T-62T-40C14
SN: SP-E0214403
Hours: 5079 (As of 11/10/2013)
Cycles: 3693 (As of 11/121/2013)



Avionics

·5 Cathode ray tube 8″ x 7″ displays (2 PFD, 2 MFD & 1 EICAS display) w/multi reversionary capabilities: Honeywell.
·Dual Integrated Avionics Computers encompassing functions such as displays, driving, dual Flight Director/ Single Autopilot, EICAS and EFIS: Honeywell IC 600.
·Dual RMU: Honeywell RMU-855B.
·First and Second VHF Communication System – both comprising integrated s Mode S Diversity Transponder – w/8.33 kHz or 25 kHz frequency spacing: Honeywell RCZ-833.
·Single Passenger Address and Cabin Interphone Systems: Avtech 5482.
·Airborne Audio System: Honeywell AV-850.
·Solid State Cockpit Voice Recorder – SSCVR: Allied Signal.
·Solid State Flight Data Recorder – SSFDR: Allied Signal.
·Single Emergency Locator Transmitter: Artex 110-4.
·Engine Indication and Crew Alerting System – EICAS: Honeywell Phase 8.
·Single Aural Warning Unite – AWU: Grimes.
·Dual Digital Clocks: Air Precision.
·Dual Air Data Computers RVSM Compatible – ADC: Honeywell AZ-850.
·Integrated Stand by Instruments System – ISIS: Thales (Sextant).
·Dual Inertial Reference System – IRS: Honeywell Laserref IV.
· Single Radio Altimeter – RA: Honeywell RT-300.
· Dual VHF Navigation System (Integrated NAV/ADF/DME): Honeywell RNZ-851.
· Single EGPWS/Wind shear Detector and escape guidance: Allied Signal Mark V.
·Weather Radar w/Dual Control Panel and Turbulence Detection: Honeywell WU-880.
·Single traffic Alert and Collision Avoidance System – TCAS 2000: Honeywell 2000 Change 7.

Interior

13 Passenger Configuration.
Three distinct seating areas: Forward 4-place club, mid-cabin 4-place conference group, aft 3-place berthable divan and dual single club seats, flight attendant seat, cockpit jumpseat. Forward galley with water heater, microwave oven, coffeemaker and one power unit. Mid-cabin credenza, dual aft side cabinets. Airshow 410, dual DVD players, forward LS bulkhead 15.1-inch LCD monitor and aft RS bulkhead 15.1-inch monitor, acoustic entry curtain, arm ledge with VIP panel, dual 110-volt CFI outlets, five cabin power outlets. Aft pass-through baggage compartment with cargo door light and restraint net. Aft lavatory with water heater and vanity.

Exterior Description

White with two-tone blue stripes & gold accents.

Additional Features

· Dual Flight Management System + Ground Positioning System Dual FMS + GPS: Honeywell NZ-2000.
· CAT II Autopilot/Flight Director: Honeywell.
· Single Central Maintenance Computer: Vibrometer.
· Dual Stall Protection System – SPS: Rosemount.
· Single HF: Honeywell KHF-950.
· Selcal: Trimble Jetcall.
· Satcom Single Channel.

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