aircraft specification -...

BOMBARDIER CHALLENGER 604Serial Number: 5318

Date: January 2013 A/C Type: Challenger 604 Year: 1996 Location: Johannesburg, South Africa Total Time: 7,632 Hrs Cycles: 3,273 Status Date: 30 November 2012 Price: USD 7,900,000 Green C of A Date: August 1996 Date Entered Service: September 1998

Aircraft Management CharterFBOSimplyFlySales & AcquisitionsMaintenanceCompletions Consulting

A F R I C A A S I A A U S T R A L A S I A E U R O P E L A T I N A M E R I C A M I D D L E E A S T

AIRCRAFT SPECIFICATIONPRE-OWNED AIRCRAFT

AIRCRAFT Maintenance Program & Warranty• Engines are enrolled on JSSI at $183.00 /hour per engine.• Airframe is enrolled on CAMP• Engines and APU On-Condition

ENGINES General Electric CF-34 3B

#1: TSN: 7,632 Hrs Cycles: 3,273 SN: 872053

#2: TSN: 7,632 Hrs Cycles: 3,273 SN: 872054

APU Honeywell GTCP 36-100E

TSN: 7,156 Hrs Starts: 4,284 SN: P-505

AIRFRAME/ENGINES/APU

AVIONICS

PRE-OWNED AIRCRAFT Aircraft offered subject to prior sale or withdrawal from market. Specifications subject to verification by Purchaser. /8


• Dual Collins AVSAT FMS-6000 Flight Management Systems• Dual Collins FCC-4006 Digital Flight Control Computers• Dual Collins ADC-850E Digital Air Data Computers• Dual Collins DCU-4000 series Data Concentrator Units• Single Dual Channel Collins Integrated Avionics Processing

Systems (IAPS)• Six Collins EFD-4077EFIS display tubes with EICAS• Single Collins MDC-4000 Maintenance Diagnostic Computer• Collins TWR-850 Weather Radar (RT A 854)• Dual Collins WXP 4220 Weather Radar Control Panels• Dual Collins Radio Altimeter (ALT 55B)

• Triple Litton LT N-101 Inertial Reference Unit• Dual Collins GPS-4000 Global Position Sensor• Dual Collins VIR-432 Nav Receivers (FM Immunity)• Dual Collins DME-442 Distance Measuring Equipment• Dual Collins ADF-462 Automatic Direction Finders • Dual Collins TDR -94D Mode S Transponders (-007)• Dual Collins RTU -4000 Radio Tuning units• Dual Collins VHF-422D Comm Transceivers (8.33 kHz

Spacing)• Dual Collins HF-9000 HF Communications System• Coltech CSD-714 Selcal Decoder System

MAINTENANCE

• 400hr check complied with 30-11-2012• 800/1600hr checks complied with 22-02-2011• 12/24/36 month checks complied with 22-02-2011• 400 APU check complied with 19-09-2012• 800 APU check complied with 21-02-2011• 48 month inspection completed on 30-11-2012• 96 month inspection completed on 30-11-2012• 12 month inspection completed on 30-11-2012• Main and nose gear overhaul completed on 30-11-2012• Exterior paint touch ups completed on 30-11-2012• Interior repair work and touch ups completed on 30-11-2012

Collins ProLine 4 (6 Tube EFIS):


Additional Avionics Equipment:• Collins TCAS-94 Traffic Alert and Collision Avoidance System• L3/Fairchild A100S Cockpit Voice Recorder• L3/Fairchild F1000 Flight Data Recorder• Honeywell MkV Enhanced Ground Proximity Warning System• Artex C406-1 ELT (121.5/243/406 MHz)• L3/BFGoodrich WX–1000E Lightning Detection Sensor System

Communication, Cabin entertaining- and Optional systems:• MagnaStar C-750 Telecommunications management system• Iridium flight phone• Collins/Airshow GENESYS cabin information system (Airshow)• Baggage compartment Smoke Detector• Pulse lighting unit• Entertainment System (DVD, CD players)• Fwd and Aft Monitors• 110 Volt Outlets

The following installation or modifications are incorporated:• SB 604-34-001 – Traffic Alert and Collision Avoidance System• SB 604-34-004 – Third Inertial Reference System• SB 604-34-005 – Second Radio Altimeter• SB 604-34-008 – Lightning Detection System• SB 604-34-020 – Enhanced Ground Proximity Warning System• SB 604-34-031 – Basic Mid Life Avionics Upgrade Rockwell-Collins Precision Plus• SB 604-34-035 – FMS; New V-Speed Data Bases• SB 604-34-037 – Elementary Mode S Surveillance/ACAS II

The aircraft fulfil the following requirements:• ACAS II (TCAS II with change 7)• RVSM• Mode S Elementary Surveillance• JAR-OPS1 Subpart K & L• IFR Cat. I & II, NAT-MNPS, RNP-10, RNP-5 and BRNAV

INTERIOR

The aircraft features a nine (9) passenger interior; forward there is a galley with wood trim and gold finishes moving aft there are four (4) executive seats arranged in a double club setting with fold out tables. Aft features a RH three (3) place berthable divan opposite two (2) executive chairs. The extended cabin then leads into a lavatory with sink and walk in baggage storage area. There was an interior refurbishment undertaken in May 08 with new head and side liners installed, new carpet as well as seat leather replacement and the woodwork was also refurbished.


AVIONICS


ADDITIONAL FEATURES

• BCCI Completion (Montreal/Innotech)• Certified for 10 Passengers (plus 1 belted Toilet seat)• Individual Jump Seat• Additional Rear Cabin Window• Fwd. Viewing Clare shield Camera System• Additional Cabin Oxygen Outlet• JAR OPS certified

WEIGHTS

CONTACT

Madie WernerGroup Sales Support ManagerTel: +41 44 876 [email protected] / [email protected]

• Max Ramp Weight 48,300 Lbs• Take Off Weight 48,200 Lbs• Landing Weight 38,000 Lbs• Max Zero Fuel Weight 32,000 Lbs• Basic Operating Weight 26,686 Lbs• Max Fuel Weight 19,850 Lbs• Aircraft Empty Weight 28,205 Lbs

FLOORPLAN

The exterior features an overall Matterhorn White finish with Light Grey and Blue accent striping completed in February 05.

EXTERIOR


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