Category: News

Global Express MSN 9111

Global Express MSN 9111 AVAILABLE FOR SALE-MAKE OFFER

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DESCRIPTION
• New to market!!!
• 2003 vintage GLEX
• Single Fortune 500 owner
• Impeccable maintenance condition with Batch 3 Avionics
• Pristine exteriors and interiors
AIRFRAME

Total Time Since New 7557 Hours (as of 13 Sep 17)
Total Landings Since New 4440 Landings
Entry into service date 27-May-2003
Home Base Mumbai, INDIA
Maintenance Tracking ARMS
Program Coverage Smart Parts Program
Certification EASA, FAA, DGCA Certified

ENGINES

Left Engine Right Engine
Description Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20 Rolls Royce BR710-A2-20
Serial Number(s) 12334 12333
Total Hours Since New 6956 Hours 6774 Hours (As on 13 Sep 17)
Total Cycles Since New 4118 Cycles 3966 Cycles (As on 13 Sep 17)
Overhaul Due On Condition
Program Coverage Rolls Royce Corporate Care Program

APU

Description Honeywell RE220 (GX)
Serial Number P-221
APU Total Time Since New 7860 Hours (As on 8 Sep 17)
Program Coverage N/A

AVIONICS
This Global Express is equipped with a fully integrated Honeywell Primus 2000XP avionics suite.

Type of Unit Quantity Description
EFIS (Electronic Flight Instrument System) 6-Tube DU-875 Primus Elite LCD Displays
ESIS (Electronic Standby Instrument System) Single Thales IESI
FMS (Flight Management System) Triple Honeywell FMZ-2000
IRS (Inertial Reference System) Triple Honeywell
GPS (Global Positioning System) Dual Honeywell HG2021Sensor Unit
MADC (Micro Air Data Computer) Triple Honeywell
DME (Distance Measuring Equipment) Dual Honeywell RNZ-851
HUD (Head Up Display) Single Thales Head Up Display
ADF (Automatic Direction Finder) Dual Honeywell RNZ-851
AUTOPILOT Dual Honeywell IC-800
VHF COM (Very High Freq. Communication) Triple Honeywell Primus RCZ 833
SATCOM (Satellite Communications) Single Honeywell MCS 6000
VOR NAV / ILS / MARKER Dual Honeywell RNZ-851
RADAR Single Honeywell Primus 880, WU-880
RADIO ALT (Radio Altimeter) Dual Collins ALT- 4000
XPNDR (Transponder) Dual Honeywell RCZ-833, Mode S
EGPWS (Enhanced Ground Proximity Warning System) Single Honeywell Mark V w / Windshear
TCAS II (Traffic Collision Avoidance System) Single Honeywell TCAS 2000 w/ Change 7.1
CVR (Cockpit Voice Recorder Single Honeywell SSCVR
FDR (Flight Data Recorder) Single Honeywell SSFDR
Telelink Datalink ——- Teledyne TL-608

INTERIOR

Number of Passengers Sixteen (16)
Galley Location Forward
Fwd Cabin Configuration Four Place 9G Single Club Seats with foldout tables
Mid Cabin Configuration Six-Place 9G Single Seat conference group with conference table
Aft Cabin Configuration Six-place 16G Bed divan LH and RH (3 place each)
Lavatory Location(s) One Forward crew lavatory and One Aft fully enclosed lavatory with storage cabinet
Crew Area Forward
Jumpseat Yes

EXTERIOR

Base Paint Color(s) Overall White fuselage
Stripe Color(s) Golden and Blue accent stripe running from nose to tail and on the vertical stabilizer
Last Painted Date October 2013

ENTERTAINMENT

Type of Unit Description
Display/TV Monitor(s) Three (3) Bulkhead-mounted 18” LCD Monitor
Individual Monitors Two (2) Plug-in 10” touch screen LCD monitors
Airshow System Rockwell Collins Flight Information System (Moving Map)
CD/DVD Player(s) Multi-region CD/DVD Players combined unit

 
MAJOR INSPECTION STATUS

Inspection Last Performed Next Due
15 Mo. Check 15 Aug 2017 14 Nov 2017
30 Mo. Check 10 JUNE 2016 9 DEC 2018
60 Mo. Check 21 DEC 2013 20 DEC 2018
120 Mo. Check 21 DEC 2013 20 DEC 2023

OTHER / ADDITIONAL EQUIPMENT

Type of Unit Type of Unit
Provision for CVR Datalink Cockpit Printer
Airborne Data Link System (ADLS) Passenger Address (PA) System
Honeywell LSZ-860 Lightening Sensor System (LSS) ACARS Data Support
Global Office Operations at Airports with Maximum Weight Restrictions
Cockpit Refuel/Defuel Control Panel Towbar Assembly
Logo Light, Ext. Baggage Door Lock Override, EICAS “Small Serv Door” Annunciation, Aircraft ID Plate, APU Hour Meter Handrail Extension
Battery Access Multi-Purpose Ladder
Common Key Panels, Lockable Fuel Cap Aesthetic Side Covers on Main Entry Door
Aft Equipment Bay Storage Box Ground Service Cabin Power
Cabin Bus Disconnect 230V AC 50Hz GFI protected utility outlets
One (1) 3500 VA/230VAC/50Hz power converter Batch 3 Avionics Upgrade
ADSB Upgrade Package Magnastar C-2000 ARTU Cabin Communication System
CAIMS Information System CPDLC Support capability

NAVIGATION & COMPLIANCE

RVSM RNAV 10 (RNP 10)
MNPS RNAV 1 & 2
RNAV 5 FM Immunity

WEIGHTS

Gross Weight (Ramp) 96,250 lbs Max Fuel Capacity 43,538 lbs
Max Takeoff Weight 96,000 lbs Max Zero Fuel Weight 56,000 lbs
Max Landing Weight 78,600 lbs Basic Operating Weight 45,000 lbs

CONNECTIVITY

Type of Unit Description
High Speed Internet(Wi-Fi) Three (3) channels Aero H+ (2 voice and 1 Data). Data channel supports ACARS/maintenance functions
Wireless Ethernet LAN –
In Flight Phone Via Satcom Single-channel ICS-100 Iridium Telephone SystemThree (3) corded and One (1) Cordless Telephone Handsets
Cabin Cabin Printer/Fax Plain Paper
ACARS Data Support –

 

2003 CESSNA CITATION CJ2

2003 CESSNA CITATION CJ2 AVAILABLE FOR SALE-MAKE OFFER

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GENERAL INFORMATION

Well maintained jet with good paint and interior.

AIRFRAME

Total Time:            1675.15 Hours
Total Cycles:         1303
HIS Interval:          1750 Hours
Overhaul Interval:  3500 Hours

ENGINES

L/H Engine             : Turbo-fan (FJ44-2C)
Total Time              : 1675.15
Cycles                    : 1303 Cycles
R/H Engine             : Turbo-fan (FJ44-2C)
Total Time              : 1675.15
Cycles                    : 1303 Cycles

AVIONICS

  • PROLINE 21 SYSTEM
  • VHF/GPS/VOR/ILS – GNS 530/430
  • ADF RECEIVER – KR 87
  • HF TRANSCEIVER- KHF 950
  • DME TRANSCEIVER – KN 63
  • ATC TRANSPONDER – TDR-94D
  • WEATHER RADAR – RTA 800
  • EGPWS – MK VIII
  • TCAS II – TTR 4000
  • RADIO ALTIMETER – ALT 55B
  • ELT – ARTEX C406-2

AVIONICS OPTIONS

  • Universal UNS-1L FMS
  • Honeywell HF-950
  • Artex C406-2 Three Frequency ELT
  • Honeywell Mark VIII EGPWS
  • Honeywell RTA 800 Color Weather Radar
  • Honeywell TCAS 4000 (TCAS II)
  • L-3 Communications FA2100 CVR
  • FMS Performance Database

EXTERIOR

Overall Snow White with Sherwood Green Metallic, Platinum Metallic and Tibetan Gold Metallic stripes.

INTERIOR

2 Cockpit Seats, 3 Cabin Seats on LH Side, 3 Cabin Seats on RH Side, One Toilet Seat on LH Side, Safety Belts and Shoulder Harnesses for all crew and pax seats including toilet seat. One Foldable Table on LH side and RH side.

2002 EMBRAER LEGACY 600

2002 EMBRAER LEGACY 600 AVAILABLE FOR SALE-MAKE OFFER

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GENERAL INFORMATION

With a range of 3,450nm with 13 passengers, this super midsize jet handles high payload capacity and flexible takeoffs and landings

AIRFRAME

  • Total Time: 3745.2 hours
  • Total Cycles: 1900 (As of 14th Jan 2014)
  • Gross Weight (Ramp): 49,758 lbs
  • Max Takeoff Weight: 49,604 lbs
  • Fuel Capacity: 17,600 lbs

ENGINES
L/H Engine             : Rolls Royce AE3007-A1E
Total Time              : 3745.2 hours
Cycles                    : 1900
R/H Engine             : Rolls Royce AE3007-A1E
Total Time              : 3745.2 hours
Cycles                    : 1900
APU                       : Hamilton Sundstrand APS 500R/T-62T-40C14
Hours                     : 5079 (As of 11/10/2013)
Program Coverage: 3693 (As of 11/12/2013)

AVIONICS

  • 5 Cathode ray tube 8”x7” 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 Mode S Diversity Transponder – with 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 with 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

EXTERIOR

White with two – tone blue stripes & gold accents

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 jump seat. 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 and five cabin power outlets. Aft pass‐through baggage compartment with cargo door light and restraint net. Aft lavatory with water heater and vanity.

2007 CHALLENGER 605

2007 CHALLENGER 605 AVAILABLE FOR SALE-MAKE OFFER

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CL 604 Interior

GENERAL INFORMATION

Professionally overseen by one owner since new. Airframe & Engines enrolled on Smart Parts Plus, APU on MSP. Interior Partial Refurbishment December 2012. The stunning interior offers both an excellent working and dining environment.

AIRFRAME

Total Time: 3029.30 hours
Total Cycles: 1158 (As of 20th April 2014)
Enrolled on Smart Parts Plus

ENGINES

  • L/H Engine : GE CF34-3B
  • Total Time : 3029.30
  • Cycles : 1158 Cycles
  • TBO : On Condition Program
  • Coverage: Smart Parts Plus – Engines Supplemental

 

  • R/H Engine : GE CF34-3B
  • Total Time : 3029.30
  • Cycles : 1158 Cycles
  • TBO : On Condition Program
  • Coverage: Smart Parts Plus – Engines Supplemental

 

  • APU : GRT GTCP36-150 (CL)
  • Hours : 3302
  • Program Coverage: MSP

AVIONICS/RADIOS

  • ADF ANTENNA
  • AFT DME ANTENNA
  • AFT RADIO ALTIMETER ANTENNA
  • ALT-4000,TRANSCEIVER ALTIMETER ALT-4000 ROCKWELL COLLINS
  • ATS CONTROL PANELAUDIO CONTROL UNIT
  • AUTOPOWER COMPUTER
  • BAND PASS FILTER IRIDIUM FILTER
  • BLADE 406, ELT ANTENNA
  • CMU-4000,COMM.MANAGMENT UNIT
  • CSU-4100 UNIT
  • CSU-4100 UNIT
  • CVR – COCKPIT VOICE RECORDER L3 COMM
  • CVR ULB UNDERWATER LOCATOR BEACON
  • DATA BASE UNIT
  • DME-4000 TRANSCEIVER DME-4000 ROCKWELL COLLINS
  • DME-4001 TRANSCEIVER DME-4000 ROCKWELL COLLINS
  • ECU-3000,EXT.COMPENS UNIT
  • EFIS-THIRD VANE A0A TRANSMITTER TRANSDUCER
  • ELT – EMERGENCY LOCATOR TRANSMITTER
  • EMERGENCY LOCATOR TRANSMITTER (ELT) BATTERY
  • FDR – FLIGHT DATA RECORDER L3 COMM
  • FDR ULB UNDERWATER LOCATOR BEACON
  • FLIGHT CONTROL COMPUTER ROCKWELL COLLINS
  • FWD DME ANTENNA
  • FWD RADIO ALTIMETER ANTENNA
  • G/S – GLIDESLOPE ANTENNA
  • GLOBAL POSITION, GPS ANTENNA
  • GLOBAL POSITION, GPS RECEIVER GPS-4000A ROCKWELL COLLINS
  •  IAPS CONTROL UNIT
  • IAPS INTEG CARD CAGE CAGE 1CC-4007 ROCKWELL COLLINS
  • IRIDIUM ANTENNA IRIDIUM TRANSCEIVER (SATCOM) ICS-200 IRIDIUM
  • IRU – INERTIAL REFERENCE UNIT LASEREI V HONEYWELL
  • LH ADC-AIR DATA COMPUTER
  • ADC-850E ROCKWELL COLLINS
  • LH PITOT STATIC PROBE
  • LH VOR/LOC ANTENNA LIGHTNING PROTECTOR
  • LOWER ATC TRANSPONDER (XPNDR) ANTENNA
  • LOWER TCAS ANTENNA LOWER TCAS TRANSPONDER (XPNDR) ANTENNA
  • LOWER VHF ANTENNA
  • MARKER BEACON ANTENNA
  • MDC-3110, MAINT DIAG COMPUTER
  • NAV-4000,VHF NAVIGATION TRANSCEIVER NAV-4000 ROCKWELL COLLINS
  • NO. 1 FLIGHT MANAGEMENT (FMC) COMPUTER FMC-600 ROCKWELL COLLINS
  • NO. 2 DCU – DATA CONCENTRATOR UNIT DCU-4002 ROCKWELL COLLINS
  • NO. 2 FLIGHT MANAGEMENT (FMC) COMPUTER FMC-600 ROCKWELL COLLINS
  • NO.1 HF (HF-9031A) TRANSCEIVER HF-9031A ROCKWELL COLLINS
  • NO.1 HF ANTENNA COUPLER
  • NO.1 SERVO SWITCHING SSM-4000 SENSOR
  • NO.1 TDR-94D TRANSPONDER TDR-94D ROCKWELL COLLINS
  • NO.1 VHF-4000,COMM TRANSCEIVER VHF-4000 ROCKWELL COLLINS
  • NO.2 HF (HF-9031A) TRANSCEIVER HF-9031A ROCKWELL COLLINS
  • NO.2 HF ANTENNA COUPLER
  • NO.2 SERVO SWITCHING, SSM-4000 SENSOR
  • NO.2 TDR-94D TRANSPONDER TDR-94D ROCKWELL COLLINS
  • NO.2 VHF-4000,COMM TRANSCEIVER VHF-4000 ROCKWELL COLLINS
  • NO.3 VHF-4000,COMM (OPTIONAL) TRANSCEIVER VHF-4000 ROCKWELL COLLINS
  • RADAR, WEATHER RTA-854 ANTENNA RTA-854 ROCKWELL COLLINS
  • RH ADC-AIR DATA COMPUTER ADC-850E ROCKWELL COLLINS
  • RH PITOT STATIC PROBE
  • RH VOR/LOC ANTENNA
  • SELCAL DECODER
  • STANDBY PITOT PROBE
  • TAT – AIR TEMP SENSOR
  • TAWS-TERRAIN-AVOIDANCE WARNING SYSTEM (GPWS EGPWS) MARK V EGPWS HONEYWELL
  • TTR-4000,TCAS II. UNIT TTR-4000 ROCKWELL COLLINS
  • UMT-12,RAD.ALT. MOUNT
  • UPPER ATC TRANSPONDER (XPNDR) ANTENNA
  • UPPER TCAS (OPTIONAL) ANTENNA
  • UPPER TCAS TRANSPONDER (XPNDR) ANTENNA
  • UPPER VHF ANTENNA
  • VHF ANTENNA
  • WX-1000, LDS, LIGHTNING DETECTION ANTENNA
  • WX-1000E – LDS CONTROL STORME SCOPE SERIE 11 L3 COMM

EXTERIOR

2007 overall matterhorn white base with gloss gold metallic and gloss blue parallel stripes painted across fuselage with single gloss gold stripe extending to engine and winglets

INTERIOR

12 seats (11 certified for take-off & landing) Partial refurbishment December 2012 by TAG Aviation – major cabin items removal, refinished (strip & lacquer) and refitted. Other minor cabin defects rectification
MAINTENANCE

  • 1000 hour check complied with 24th January 2013
  • 400 hour check complied with 23rd May 2012
  • 800 hour check complied with 22nd July 2011
  • 1600 hour check complied with 31st March 2010
  • APU 500 & 1,000 hours checks complied with 07th February 2013

 

2006 Hawker 400XP

2006 HAWKER 400XP AVAILABLE FOR SALE-MAKE OFFER

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Citation

GENERAL INFORMATION

Well maintained Jet with good paint and interior.

AIRFRAME

  • Total Time:1301
  • Landings: 1090

ENGINES

  • Pratt & Whitney JT15D-5

Engine No.1

  • Total Hours: 1301
  • No. Of Cycles: 1090

Engine No.2

  • Total Hours: 1302
  • No. Of Cycles: 1090

AVIONICS

 

Manufacturer Type/Model Quantity
Automatic Pilot Radio Coupled Collins APS-4000 2
VHF Communication Collins VHF-422C 2
ADF Collins Collins 1
DME Collins DME-422 2
ATC Transponder Collins TDR-94D 2
Weather Radar Collins RTA-854 1
Radio Altimeter Collins ALT-1000 2
TCAS/ACAS Collins TTR-4000 1
GPS Collins GPS4000A 1
ELT Artex C406-2 1
Flight Data Recorder(FDR) Fairchild F1000 1
Cockpit Voice Recorder(CVR) Fairchild DK100 1
Other Equipments FMS Collins, EGPWS APS-5000, Mark V 2

EXTERIOR

Overall White with Red and Gold Stripping

INTERIOR

Eight (8) Passenger configuration w/ approved belted toilet seat. Seven individual beige leather seats (4) forward facing and (3) Aft. Lt Beige textured fabric interior with polished wood trim and fold out tables. Full enclosed Aft Lav with Vanity and Mirror. Forward Galley/Baggage Cabinet.

2011 EMBRAER LEGACY 650

2011 EMBRAER LEGACY 650 AVAILABLE FOR SALE-MAKE OFFER

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Legacy 650 Interior 2

GENERAL INFORMATION

Almost brand new aircraft with stunning Interiors. USD 800,000 worth of options.

 This low-flight time Embraer Legacy 650 is equipped with an integrated Honeywell Primus Elite TM Avionics and 13-passenger seat Configuration.

AIRFRAME

  • Total Time: 286.8 Hours
  • Landings: 94 cycles

ENGINES

L Engine s/n CAE 313243
Flight Hours: 286.8 Hours
Cycles: 94
R Engine s/n CAE 313245
Flight Hours: 286.8 Hours
Cycles: 94

AVIONICS

  • Five 8″ x 7″ Liquid Crystal Display (LCD), 2 Primary Flight Displays (PFD), 2
  • Multifunction Displays (MFD) and 1 Engine Indication and Crew Alerting System
  • (EICAS) with multi reversionary capabilities
  • Dual Integrated Avionics Computers (IAC) encompassing functions such as displays driving, dual Flight Director / Single Autopilot, Engine Indication and Crew Alerting System (EICAS) and Electronic Flight Instrument System (EFIS)
  • Dual Radio Management Units (RMU)
  • Dual VHF Communication System with 8.33 KHz frequency spacing comprising
  • Mode S Diversity Transponder
  • Dual VHF Navigation System (Integrated NAV, ADF and DME functions)
  • Cabin Interphone Systems
  • Airborne Audio System
  • Solid State Cockpit Voice Recorder (SSCVR)
  • Solid State Flight Data Recorder (SSFDR)
  • Engine Indication and Crew Alerting System (EICAS)
  • Aural Warning Unit (AWU)
  • Dual Digital Clocks
  • Coupled VNAV
  • RNP 0.3 capability
  • Dual RVSM compatible Air Data Computers (ADC)
  • Integrated Standby Instruments System (ISIS)
  • Dual Inertial Reference System (IRS)
  • Radio Altimeter (RA)
  • EGPWS with windshear detector and escape guidance
  • Weather Radar with Dual Control Panel and Turbulence Detection
  • Traffic Alert and Collision Avoidance System (TCAS 2000)
  • Dual Flight Management Systems (FMS) + Global Positioning Systems (GPS)
  • Data Loader DL-1000
  • CAT II Autopilot/Flight Director (FD)
  • Central Maintenance Computer (CMC)
  • Dual Stall Protection System (SPS)
  • HF Radio
  • SELCAL
  • Emergency Locator Transmitter (ELT)

EXTERIOR

Customized Paint Scheme

INTERIOR

Galley and Entrance Area

  • Flight Attendant Seat with intercom handset integrated
  • Forward Crew Lavatory external serviceable replacing storage closet
  • Additional Convection Oven
  • Four standard units/food container
  • Coffee Brewer

Entertainment

  • Fwd 17″ LCD Widescreen Monitor at the FWD partition on the on the RHS replacing the Std monitor on the LHS

General

  • Cockpit Seat with Sheepskin
  • Mid Cabin Curtain Divider Separating the divan zone

Layout Configuration

  • Second divan in the rear cabin section replacing the standard single club seat

2006 CESSNA CITATION XLS

2006 Cessna Citation XLS AVAILABLE FOR SALE-MAKE OFFER

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 Citation

AIRFRAME

  • Total Time: 2690 Hours
  • Landings: 1843 cycles

ENGINES

  • Pratt & Whitney PW545B
  • Left Engine: 2549 Hours / 1724 Cycles
  • Right Engine: 2529 Hours / 1749 Cycles
  • EASA and EU-OPS compliant
  • Currently enrolled on Cessna Pro Parts Program, Pro Advantage+ Program, Aux Parts Program
  • APU: Honeywell RE 100(XL)
  • APU Total Time: 2196 Hours / 2285 Cycles

AVIONICS

  • Honeywell P-1000 Integrated Flight Director & Autopilot System, 3-Tube 8×10” EFIS
  • Honeywell RCZ-833k Radios with Dual Comm, Dual Nav, ADF, Dual DME, Dual RMI
  • Dual Mode S Diversity Transponders with Enhanced Surveillance
  • Dual Universal UNS-1ESP FMS
  • JAA Flight Data Recorder
  • Honeywell HF-1050
  • Pulselite Sys interfaced to TCAS
  • Aircell ST-3100 Phone
  • Coltech CSD-714 Selcal
  • Honeywell AFIS (Provisions only)
  • L3 Communications TCAS 2000
  • Fairchild FA2100 CVR
  • Artex C406N ELT

EXTERIOR

Dual Tone Paint Scheme in Whisper Gray and Starlight Silver Metallic with a Black Metallic Stripe

INTERIOR

Overall Elegant Crème and Matte Black Color Scheme
Carpet is Flannel Colored Cut Pile
Window Reveals are Vanilla-Colored Cloth Material and the Lower Sidewalls are Black Suede Leather
Reblocked Passenger Seats are Matte Black Townsend Leather
Overall Cabinetry is High Gloss Zebrawood Veneer with Polished Gold Plating

2010 CESSNA CITATION XLS+

2010 Cessna Citation XLS+ AVAILABLE FOR SALE-MAKE OFFER

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OLYMPUS DIGITAL CAMERA

GENERAL INFORMATION

Cockpit Flood Lights, Cockpit Seats with Sheepskin Covers, Sunshade and Sun Visors, Life Vests, Smoke Goggles, Premium Pax Door, Enhanced Take-Off Power Package

AIRFRAME

  • Total Time: 1225 Hours
  • Landings: 880 cycles

ENGINES

  • Pratt & Whitney PW545C
  • Engine Total Time: 1225 Hours
  • Engine Cycles: 880 Cycles
  • Enrolled on Power Advantage Plus and Pro Parts
  • APU: Honeywell RE 100(XL)
  • APU Total Time: 750 Hours
  • Enrolled on Aux Advantage

AVIONICS

  • Mexico Certification
  • Collins Pro Line 21 Avionics Suite
  • Nav-4000 ADF Collins
  • Collins IFIS-5000 File Server System
  • Second FMS-3000
  • FA2100 Flight Data Recorder
  • Mobil Jet II
  • HF Provisions
  • Dual Collins AHC-3000
  • Dual Collins ADC-3000
  • Collins CCP-3310 Cursor Control Panels
  • Collins GPS-4000S
  • Collins DME-4000
  • Collins ALT-4000 Radio Altimeter
  • Collins TCAS-4000
  • Collins TWR-850 Doppler Weather Radar

EXTERIOR

White Base with Royal Blue and Manhattan Grey Striping

INTERIOR

  • Overall Beige Color Scheme with Complemented High Gloss Wood Veneer
  • Cabinetry and Satin Silver Accents
  • Standard Center Club Seating
  • RH Forward Two Place Side Facing Couch
  • RH Forward Closet with Rosen Flight View Moving Map System
  • LH Forward Refreshment Center
  • Two Executive and Two Slimline Tables with Leather Inserts
  • Removable LH Aft Side-Facing Seat
  • Aft Cabin Dividers with Mirror/Veneer Sliding Privacy Doors
  • Removable Belted LH Aft Side Facing Seat with Restraint System and Fold Down Seat Back Cushion for Storage with Cargo Net and Overwater Life Vest Stored in Seat Base
  • RH Non-Belted Externally Serviceable Flushing Toilet
  • 110 Volt AC Outlets
  • Headrest Slipcover Pillows and Indirect Lighting

2005 GLOBAL EXPRESS 5000

2005 GLOBAL EXPRESS 5000 AVAILABLE FOR SALE-MAKE OFFER

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Global 5000

GENERAL INFORMATION

One Owner Since New, Batch-3, TV/EVS/HUD, Impeccable Condition Inside & Out

AIRFRAME

  • Total Time: 2917 Hours
  • Landings  :  970
  • Rockwell Collins CASP Program
  • Honeywell APU MSP Program
  • Goodrich EEC Program

ENGINES

  • Rolls-Royce: BR710A2-20
  • 2917 Hours Since New

AVIONICS

  • Honeywell 2000 XP Integrated Avionics System
  • Six Tube 8″ x 7″ DU-870 Color Electronic Flight Instrument System (EFIS) Displays/ 2 PFD /2 EICAS/ 2MFD
  • Triple NZ-2000 Integrated Flight Management System w/ Dual 12 Channel GPS
  • Dual Full Regime Auto Throttle System
  • Triple IC-800 Integrated Avionics Computers (IAC) with Batch-2 upgrade
  • Triple AZ-840 Micro Air Data Computers (MADC)
  • Triple LASEREF IV Inertial Reference Systems
  • Quad Ameteck DA-810 Data Acquisition Units (DAU)
  • Primus WC-880 Color Weather Radar w/ Dual Controls
  • Dual Primus II RM-855 Integrated NAV/COM/Ident Radios w/ VOR/ILS/MKR/ADF/DME/
  • VHF Comm/Mode “S” Diversity
  • Central Aircraft Information Maintenance System (CAIMS)
  • TCAS II Traffic Alert and Collision Avoidance System (Change 7 Incorporated)
  • Dual ALT-4000 Radio Altimeters
  • Coltech CSD-714 SELCAL
  • Allied Signal SSCVR Cockpit Voice Recorder
  • Allied Signal SSFDR Flight Data Recorder
  • Artex 406 MHz Emergency Location Transmitter (ELT) with NAV interface
  • MCS-6100 6 – Channel SATCOM
  • Dual Collins HF-9000 HF Communication System
  • Enhanced Ground Proximity Warning System (GPWS) w/ Windshear Detection System
  • 8.33 kHz Channel Spacing/FM Immunity Compliant
  • Full Authority Digital Engine Control System (FADEC)
  • Engine Indication/Crew Alerting System (EICAS)
  • Flight ID/Enhanced Surveillance
  • Teledyne ACARS Datalink
  • Triple FMS 810 CDU’s

EXTERIOR

Tasteful two-tone paint scheme with Matterhorn White over Royal Blue Metallic with Gold Accent Striping

INTERIOR

  • The tastefully appointed cabin features eleven (11) individual passenger seats complete in exotic Suntan and Greenwood leathers
  • Forward cabin features four (4) executive club chairs with foldout tables
  • Center cabin features a two (2) place conference group with fold out tables opposite a large credenza
  • Aft cabin features two (2) executive club chairs with foldout tables opposite a three (3) place 16G berthable divan
  • The large aft passenger lavatory is appointed with wardrobe and vanity
  • The carpeting is a loop Moresque with Medallions
  • Cabinetry is a luxurious Pommele Sapele complimented by polished Champagne gold colored plating
  • Dado panels are 100% Bengaline Champagne silk, sidewalls are Fabric white gold and the headliner is an Ultra leather almond in color
  • The aircraft is equipped with the Global Office in the Sky system including high speed data capability with onboard wireless Ethernet local area network (LAN) and an all-in-one fax/printer/copier
  • The Entertainment center is located in the center cabin credenza and features the Tailwind 500 Direct TV System, Airshow Network and dual multi-region DVD players and multi-disc CD Player
  • Passengers enjoy cabin entertainment on eight (8) 10.4” individual armrest

2005 GLOBAL 5000

2005 GLOBAL 5000 AVAILABLE FOR SALE-MAKE OFFER

Download PDF Specs

 Global 5000 1

GENERAL INFORMATION

13 seater impeccably well maintained Global 5000 with good interiors.

AIRFRAME

  • Total Time: 4089:30 Hours
  • Cycles: 1534 (As of 2nd January 2014)
  • Airframe Enrolled on Smart Parts
  • EU OPS1 Certified
  • Commercially operated under Swiss AOC

ENGINES

  • Rolls-Royce: BR700-710A2-20
  • Engine Total Time: 4089:30 Hours
  • Engine Cycles: 1822
  • APU: Allied Signal RE-220 (GX)
  • APU Total Time: 3975 Hours

AVIONICS

  • Honeywell Primus 2000 6- Tube EFIS Integrated Avionics System
  • Dual IC-800 Integrated Avionics Computers (IAC) with EFIS
  • Dual Integrated Flight Management System
  • Quad Ametek DA-810 Data Acquisition Units (DAU)
  • Triple HG-2001GD03 Laseref IV Inertial Reference System
  • Dual Honeywell RM-855 Radio Management Units
  • Dual Honeywell RCZ-833K Integrated COM/Ident Radios w/Enhanced Mode S Transponders
  • 3rd VHF Comm. Installation (RCZ-833)
  • 8.33kHz channel spacing and FM Immunity compliant
  • Head-up Flight Display System (HUD)
  • Dual Collins HF-9031 HF Communication System
  • Single Avtech CSD-714 SELCAL Decoder
  • Dual Collins ALT-4000 Radio Altimeters
  • Dual Honeywell RNZ-851 Integrated NAV Radios with VOR/ILS/MKR/ADF/DME
  • Primus WU-880 Color Weather Radar
  • Honeywell DL-950 Data Loader
  • Honeywell TCAS 2000 Traffic Alert and Collision Avoidance with change 7
  • Honeywell Mark V EGPWS
  • Honeywell SSFDR Flight Data Recorder
  • Honeywell SSCVR Cockpit Voice Recorder
  • Tri Audio Control Panel AV-850A

EXTERIOR

Overall Matterhorn White with Grey and Yellow stripes. Global Gold tail (except horizontal stabilizer) and winglets.

INTERIOR

  • Fireblocked Thirteen (13) passenger configuration
  • Fwd cabin features four (4) executive club seats with foldout tables.  Mid-left cabin features a 4-place dinning group opposite a credenza cabinet
  • Aft cabin features two executive seats opposite a 3 place divan
  • Fwd galley is equipped with a high-temp oven, microwave, galley touchscreen and washbasin with water faucet
  • Fwd crew lavatory and aft full lavatory.