2002 LEGACY 600   Serial Number: 145637 Registration: VP‐CFB

AIRFRAME:  
CURRENT STATUS REPORT
Times Current as of 1/14/2014.
Total Time: 3889.93 Hours 
Total Landings: 1978
Gross Weight (Ramp): 49,758 lbs. 
Max Takeoff Weight:49,604 lbs. 
Fuel Capacity: 17,600 lbs. 
ENGINES:
Left / Right 
Model: Rolls Royce AE3007-A1E
SN: CAE 312273 / CAE 312310
Hours: 3889.93  / 3889.93  
Cycles: 1978 / 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.
· 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.
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 w