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Embraer Legacy 600 14500944 | A6-NKL
Embraer Legacy 600
14500944 | A6-NKL
Specifications Subject to Verification Upon Inspection
Specifications Subject to Verification Upon Inspection
Specifications Subject to Verification Upon Inspection
Specifications Subject to Verification Upon Inspection
Specifications Subject to Verification Upon Inspection
Specifications Subject to Verification Upon Inspection
Embraer Legacy 600 S/N: 14500944 Reg: A6-NKL
Airframe / Engines / APU
Airframe: 4,250 Hours Since New / 1,556 Landings Since New (as of May 2, 2017)
Enrolled on JSSI Tip to Tail
Certification Date: 24 February 2006 / In-service Date: 10 March 2006
Engines: Left Right
Serial Number: CAE-312875 CAE-312872
Hours Since New: 4,157 4,157
Cycles Since New: 1,522 1,522
Engine Model: Rolls-Royce AE3007A1E
Engine Program: Enrolled on Rolls-Royce Corporate Care
APU: Hamilton Sundstrand T-62T-40C14 / s/n: SP-E0514812 / 3,986 Hours / JSSI Enrolled
Avionics
-Honeywell Primus II Avionics Suite -Five Tube 8” x 7” displays (2 PFD’s, 2 MFD’s, & 1 EICAS) -Dual Honeywell IC-600 integrated computers -Dual Honeywell NZ-2000 FMS + GPS System -Dual RMU -Dual Honeywell RCZ-833 VHF Comms – 8.33 kHz spacing -Honeywell CMU with Third VHF -Honeywell AV-850 audio panel -Honeywell radio management unit -Dual Honeywell VHF Navigation System (Integrated NAV/ ADF/DME) -Honeywell PC-4000 CAT I & CAT II Autopilot/Flight Director -Passenger Address & Cabin Interphone System -Honeywell Solid State CVR -Honeywell Solid State FDR -121.5/243/406 MHz Emergency Locator Transmitter -EICAS -Aural Warning Unit -Dual Digital Clock -Dual Honeywell Air Data Computers -Integrated Stand-by Instrument System
Specifications Subject to Verification Upon Inspection
-Dual Honeywell LASEREF IV IRS -Radio Altimeter -Honeywell EGPWS with Wind Shear Detection and Escape Guidance -Honeywell WU-880 Weather Radar w/ dual control panel and turbulence detection -TCAS with Change 7.1 -Central Maintenance Computer -Dual Stall Protection System -Dual Honeywell HF System w/ SELCAL
Optional Equipment
-Entrance Control Panel -FADEC -Vibro-meter Engine Vibration Monitoring -Honeywell Altitude Alerter -Honeywell GC-550 Guidance Controller -AEROCOM 1000 Interphone System -AirCell Iridium ST-3100 Flight Phone
Compliance Capabilities
-RVSM Capable -Mode S Enhanced Surveillance -NAT-MNPS -P-NAV -RNP-5
-RNP-10 -B-RNAV -FM Immunity -8.33 kHz Spacing
Interior
13 passenger configuration featuring a flat floor cabin. Forward cabin: four (4) seats in a dual
club configuration, mid cabin: four (4) place conference group opposite a credenza, and aft
cabin: three (3) place divan opposite two (2) seats in a club configuration with zone divider
separating the aft from mid cabin.
Entertainment equipment includes two (2) 15.1” located in the forward and aft bulkheads.
Stereo speaker system. Two (2) DVD players. Ten (10) 115VAC power outlets. One (1) SVGA port
interfacing with the monitor located in the forward bulkhead.
Forward right hand side galley featuring a microwave oven, coffee maker, 115VAC power
outlet, sink with hot and cold water, storage boxes for drink, work surface table, ice storage,
thermos storage, galley control panel, and trash container.
The aft lavatory incorporates a flushing toilet, sink with hot & cold water, and one (1) 110 VAC
power outlet. Left hand side wardrobe and an access door to the baggage compartment.
Specifications Subject to Verification Upon Inspection
Contact Information Empire Aviation LLC
14605 North Airport Drive, Suite 100
Scottsdale, Arizona 85260
Office: +1(480) 659-0808 | Fax: +1(480) 659-0363 | [email protected] | www.empire.aero
