2011 Embraer Legacy 650

14501141 | A6-ADL

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

Specifications Subject to Verification Upon Inspection

Specifications Subject to Verification Upon Inspection

Specifications Subject to Verification Upon Inspection

Specifications Subject to Verification Upon Inspection

2011 Embraer Legacy 650 S/N: 14501141 Reg: A6-ADL

Airframe / Engines / APU

Airframe: 1,521.15 Hours Since New / 486 Landings Since New (as of May 3, 2017)

Enrolled on Embraer Executive Care Enhanced

Engines: Left Right

Serial Numbers: CAE-313271 CAE-313272

Hours Since New: 1,521.15 1,521.15

Cycles Since New: 486 486

Engine Model: Rolls-Royce AE3007A2

Engine Program: Enrolled on Rolls-Royce Corporate Care

APU: Hamilton Sundstrand T-62T-40C14 / 1,366 Hours / Enrolled on EEC Enhanced

Avionics -Honeywell Primus Elite Avionics Suite -Five 8” x 7” Liquid Crystal Displays, 2 Primary Flights Displays, 2 Multifunction Displays, and 1 Engine Indication and Crew Altering System with Multi Reversionary Capabilities

-Dual Integrated Avionics Computers -Dual Honeywell VHF Navigation System (Integrated NAV, ADF and DME Functions)

-Cabin Interphone Systems -Honeywell AV-850 Airborne Audio Systems -L3 Solid State Cockpit Voice Recorder -L3 Solid State Flight Data Recorder -Engine Indication and Crew Alerting System -Aural Warning Unit -Dual Digital Clocks -Dual Honeywell AZ-850 RVSM Compatible Air Data Computers

-Integrated Standby Instruments System -Dual Inertial Reference System -Dual Honeywell Radio Management Units -Dual VHF Communication System with 8.33 KHz Frequency Spacing

-Dual Honeywell Mode S Transponder

-Honeywell RT-300 Radio Altimeter -Honeywell Mark V EGPWS with Windshear Detector and Escape Guidance

-Honeywell WX-880 Weather Radar with Dual Control Panel and Turbulence Detection

-Traffic Alert and Collision Avoidance System (TCAS 2000)

-Dual Honeywell NZ-2000 Flight Management Systems (FMS) + Honeywell Global Positioning System + Honeywell Laseref V IRS

-Data Loader DL-1000 -CAT II Honeywell Autopilot / Flight Director -Central Maintenance Computer -Dual Stall Protection System -HF Radio -SELCAL -Artex C406-2 Emergency Locator Transmitter -Honeywell AWU Altitude Alerter -Honeywell HD-710 SATCOM DADOS – HSD -Coupled VNAV -RNP 0.3 -Charts and Maps

Specifications Subject to Verification Upon Inspection

Optional Equipment -Smart Runway and Smart Landing RAAS System

-Communications Management United with 3rd VHF (8.33 KHz Frequency Spacing)

-2nd ADF

-Steep Approach Capability & London City Airport Operation + Operation in Cannes Airport

-Electronic Flight Bag and EDS Software

-Additional Convection Oven

-Flight Attendant Seat with Intercom Handset Integrated

-77 ft3 Oxygen Bottle in Addition to the Existing 115 ft3

-Forward Crew Lavatory Externally Serviceable Replacing Storage Closet

-220V Power Outlet (all cabin will have the same power supply)

-Coffee Brewer

-Two Standard Units / Food Container

-Additional VIP Control in the AFT Cabin Zone at the LH AFT Facing Seat

-Swiftbroadband High Speed Data System

-Cockpit Seat with Sheepskin

-Provisions for Extended Overwater Operation (storage space for 2 life rafts for 12 passengers + lifeline)

-Towbar

-Mid Cabin Curtain Divider Separating the Divan Zone

-Seat Belt Extension

Interior

Cabin Layout – 13 Passenger Configuration

The cabin features three distinct zones. The forward cabin offer a four place club with two executive

tables. The mid cabin offers a conference setting with four cabin chairs stationed around a conference

table and opposite a credenza. The aft cabin features two club chairs opposite a three place divan.

There is an aft lavatory, forward crew lavatory, and a forward galley.

*please note the interior configuration above does not depict the fwd. externally serviced crew lavatory

Specifications Subject to Verification Upon Inspection

Cross Section

Notes -Warranty Start Date 29 November 2011 -CPDLC is completed -FANS-1/A is completed

Contact Information

Empire Aviation LLC

14605 North Airport Drive, Suite 100

Scottsdale, Arizona 85260

Office: +1(480) 659-0808 | Fax: +1(480) 659-0363 | aircraftsales@empire.aero | www.empire.aero