2003 CESSNA CITATION CJ2

2003 CESSNA CITATION CJ2 AVAILABLE FOR SALE-MAKE OFFER

Download PDF specs

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

Download PDF Specs

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

Download PDF Specs
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

Download PDF Specs
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.