Airframe:
AFTT: 515

Engine Specs:
PW617F

Left Engine
TBO: 3,500
TSN: 515
CSN: 519

Right Engine
TBO: 3,500
TSN: 515
CSN: 519

Avionics/Radios:
ADF: Yes
Avionics Package: CAT-I
Compass: Dual AHRS
EFIS: 3-tube 12-inch
FMS: FMS
LRN: Yes
Transponder: Dual Mode S w/diversity
Autopilot: 3-axis CAT-I
Communication Radios: Dual
DME: Dual
Flight Director: CAT-I
GPS: Dual GPS
TAWS: TAWS
Weather Radar: Yes

Additional Equipment:
Electronic Jeppesen Charts w/ChartView Sheepskin Cockpit Seats Cockpit Flood Lights Cockpit Sunshade & Sun Visor Crew Portable Breathing Equipment Smoke Goggles

Exterior:
Overall White with Blue Stripes

Interior:
Recessed aisle. Four passengers in single club seats, Aft lavatory with cabin partition. Life vests.

Inspection Status:
RVSM, located in the UK

This aircraft is being brokered by Flight Source International, Inc. Flight Source International, Inc. has not conducted a pre-purchase inspection of this aircraft to verify mechanical condition, airworthiness or accuracy of specifications. Prospective purchasers are encouraged to conduct their own independent prepurchase inspection as Flight Source International, Inc. makes no representations as to the airworthiness of the aircraft or the accuracy of the above information. Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale.

Contact:

For additional information, please contact us via the contact form on this page or through the information below:

Phone: (941) 355-9585
Fax: (941) 296-7442

Email: sales@flightsource.com

Airframe:
Total Time: 811
Total Landings: 501

Engine Specs:
Engines: AE3007A1E (Roll-Royce Corporate Care) TBO 6,000
LH Engine: 811 hours total time
RH Engine: 811 hours total time

APU: Sundstrand

Avionics/Radios:
5 Tube 8×7 displays (2 Primary Displays – PFD, 2 Multifunction Displays – MFD and 1 EICAS Display)
Dual Integrated Computer encompassing the functions of display driving
Dual Flight Director / single Autopilot and EICAS
Dual Flight Management System + Global Positioning System (FMS + GPS Honeywell)
Dual Radio Management Units (RMU)
1st and 2nd VHF Communications System – 8.33 KHz spacing (integrated VHF/Mode S Diversity Transponder) Passenger Address and Cabin Interphone
Solid Sate Cockpit Voice Recorder – SSCVR
Single Emergency Locator Transmitter Solid State Flight Data Recorder – SSFDR
Single Aural Warning Unit
EICAS
Dual Air Data Computers (ADC) RVSM
Dual Digital Clock
Integrated Stand-By Instrument System (ISIS)
Dual Inertial Reference System (IRS)
Single Radio Altimeter (RA)
Single TCAS 2000
Dual VHF Navigation System (Integrated NAV / ADF / DME)
CAT 1 and CAT 11 AP/FD
Single EGPWS / Wind Shear Detector and Escape Guidance
Dual Stall Protection Systems
Single Central Maintenance Computer (CMC)
Single HF System
Single Weather Radar with dual control panel and turbulence detection
Single SELCAL

Additional Equipment:
EGPWS w/ wind shear detection & escape, Air Cell ST-3100 SATCOM, dual integrated computers w/ EICAS, electronic flight bag w/software, dual radio management units, PA/cabin interphone system, ELT, aural warning unit; Integrated standby instrument system, central maintenance computer, dual stall protection systems, CMU w/third VHF, tire pressure gauges, dual air data computers, multi-function display, dual digital clocks, Long-range fuel system, baggage compartment w/in-flight access door, cargo door sill protection & door light, door locks, dual life rafts w/storage, Sundstrand APU w/reduced noise levels

Optional Equipment:
CMU with 3rd VHF (8.33 KHz frequency spacing)
2nd HF
Steep Approach Capability
Service Bulletin for Cannes Operation
Electronic Flight Bag with software
Long-Range Fuel System
Winglets
Access Door to Baggage Compartment
Sundstrand APS500R APU with reduced noise levels
Tire Pressure Gauges
Door Locks

Exterior:
White with Black and Grey Stripes

Interior:
Forward hand right side galley, forward left hand side entertainment cabinet, forward left hand side storage closet, and a rear lavatory. Seating for 13 passengers (forward cabin zone: 2 single club seats; mid cabin zone: one double club seat on the left hand side and a credenza on the right hand side; aft cabin zone: one divan on the right hand side and one single club seat on the left hand side and a mid cabin divider separating the divan zone. Iridium ST-3100 and AEROCOM 1000 Interphone Systems with three (3) points of connection: one point of connection integrated with the crew headsets, one handset in the arm ledge of the RH forward facing seat of the forward cabin zone (FWD RH VIP seat) and one handset located in the arm ledge of the LH conference table. Entertainment Equipment and Communications Systems consisting of: two (2) 17” wide screen monitors being one 17” wide screen monitor at the forward left bulkhead and one 17” wide screen monitor at the aft right bulkhead; two (2) DVD’s; thirteen (13) headsets; stereo speaker system; ten (10) 115VAC power outlets including galley, cabin and lavatory; one SVGA port interfacing with the forward left hand side monitor. Galley including: Microwave oven, coffee maker, 115VAC power outlet, sink with hot and cold water, storage boxes for drinks, work surface table, ice storage, thermos storage, galley control panel, trash container. The aft lavatory incorporates a flush chemical toilet, sink with hot and cold water and one 110VAC power outlet, left hand side wardrobe and an access door to the baggage compartment.

Interior Options:
Recessed Floor, High temperature oven, Flight Attendant Seat with intercom handset integrated, Additional VIP Control in the aft cabin zone, High Speed Data – HSD, Additional 110V GFI outlet in the Credenza toe kick area, Cockpit Seat with Sheepskin, Storage space for life rafts (2 life rafts for 12 passengers), 2 Life rafts for EASA aircraft (JAR OPS-1 Compliance – 2 life rafts for 12 passengers), Mid Cabin Curtain Divider Separating the divan zone

Inspection Status:
Maintenance: Maintained: JAR Ops 1 Inspection: RVSM & CAT I & CAT II. Steep Approach capable. Cannes Operation SB c/w as reported 12/05/08. Certifications: CAT II, RVSM.

This aircraft is being brokered by Flight Source International, Inc. Flight Source International, Inc. has not conducted a pre-purchase inspection of this aircraft to verify mechanical condition, airworthiness or accuracy of specifications. Prospective purchasers are encouraged to conduct their own independent prepurchase inspection as Flight Source International, Inc. makes no representations as to the airworthiness of the aircraft or the accuracy of the above information. Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale.

Contact:

For additional information, please contact us via the contact form on this page or through the information below:

Phone: (941) 355-9585
Fax: (941) 296-7442

Email: sales@flightsource.com

Airframe:
Landings: 1,483
Airframe Total Time: 2,064

Engine Specs:
Engines: RR AE-3007A1E – TBO: 6000

LH Engine: 2,109 hours total time

RH Engine: 2,109 hours total time

APU: Sundstrand APS500R

Avionics/Radios:
Avionics: Dual Honeywell Primus IFCS / Primus II
ADF: Dual Honeywell RNZ-851
Autopilot: Honeywell Primus IFCS CAT I & II
Comms Radios: Dual Honeywell RCZ-833E w/8.33 kHz spacing
CVR: Honeywell SSCVR
Compass: Honeywell AHS-3000 AHRS
EFIS: Honeywell Primus 1000 5-tube
DME: Dual Honeywell RNZ-851
Flight Phone: AEROCOM 1000
FDR: Honeywell SSFDR
IRS: Dual Honeywell LASEREF III
Flight Director: Dual Honeywell Primus IFCS CAT I & II
Radar Altimeter: Dual Honeywell RT-300
FMS: Dual Honeywell NZ-2000 w/dual Honeywell GR-550 GPS
TAWS: Honeywell Mark V EGPWS w/windshear
Hi Frequency: Dual Honeywell KTR-953 w/SELCAL
TCAS: Honeywell TCAS-2000 w/change 7
Navs: Dual Honeywell RNZ-851
Weather Radar: Honeywell WU-880
SATCOM: Universal TT-3000
Transponder: Dual Honeywell RCZ-833E Mode S diversity w/elementary surveillance

Additional Equipment:
RVSM
8.33 SPACING
HONEYWELL RT-300 RA
HONEYWELL AS-400
DUAL DIGITAL CLOCKS
GRIMES AURAL WARNING UNIT
SINGLE CMC-116
HONEYWELL CDU-850
HONEYWELL DL-900
8-110V/60 HZ OUTLETS
SEPTEMBER 2010,500/1000/2000/4000/8000HR
INSP C/W 9/10, WEIGHT & BALANCE C/W 9/10 B/P-RNAV/MNPS/RNP-10
FULL JAR OPS COMPLIANT
UNIVERSAL ACARS
DUAL HONEYWELL RM-855
DUAL HONEYWELL DA-800
THOMSON INT STDBY INSTRUMNTS
DUAL HONEYWELL AZ-840
HONEYWELL AHS-3000
HONEYWELL CD-810
6.5″PLUG-IN LCD PROVISION
6/12/24/48/96 MO INSP C/W

Year Painted:
2010

Exterior:
OVERALL WHITE W/LIGHT & DARK BLUE STRIPES, TOUCHED UP 2010.

Interior:
15 PLACE FIREBLOCKED INTERIOR W/FWD DBL CLUB, MID CONFERENCE GROUP OPPOSITE CREDENZA FOLLOWED BY SINGLE LH SEAT FACING AFT OPP SINGLE RH SEAT FACING FWD AND AFT 2-PLACE CLUB OPP 3-PLACE BERTHABLE DIVAN. BEIGE LEATHER SEATS & BEIGE CARPET. FWD GALLEY W/MICROWAVE & COFFEE MAKER. ENTERTAINMENT W/AIRSHOW 400, EACH SEAT W/6.5″
PLUG-IN LCD EXCEPT INBOARD CLUB SEATS, 15.1″ LCD ON LH FWD BULKHEAD, VCP, DVD & CD PLAYER. AFT LAV W/ELECTRIC FLUSHING POTTY.

Inspection Status:
MAINTAINED: JAR OPS 1, CAMP, CERTIFICATIONS: B-RNAV, P-RNAV, RNP-10, RVSM, INSPECTION: RVSM, B-RNAV, P-RNAV, MNPS & RNP-10. 6/12/24/58/96-MONTH INSPECTIONS C/W 09/10. 500/1000/2000/4000/8000-HOUR INSPECTIONS C/W 09/10. WEIGHT & BALANCE C/W 09/10. WEIGHTS (LBS.)MGTOW 49606, RAMP,50154, ZFW 35273, LANDING 40785,EMPTY 30793, FUEL 17844. FUEL CAPACITY:2664 U.S. GALLONS.

This aircraft is being brokered by Flight Source International, Inc. Flight Source International, Inc. has not conducted a pre-purchase inspection of this aircraft to verify mechanical condition, airworthiness or accuracy of specifications. Prospective purchasers are encouraged to conduct their own independent prepurchase inspection as Flight Source International, Inc. makes no representations as to the airworthiness of the aircraft or the accuracy of the above information. Specifications Subject To Verification Upon Inspection. Aircraft Subject To Prior Sale.

Contact:

For additional information, please contact us via the contact form on this page or through the information below:

Phone: (941) 355-9585
Fax: (941) 296-7442

Email: sales@flightsource.com