Bombardier Challenger 605 - Southern Cross … · • Definition List E934000 updated to Revision CQ and Modification data ... • Aft Equipment Bay access ... Bombardier Challenger

Bombardier Challenger 605Serial Number: 5805 In Service: 2010

Registration: LV-CCW Certification: 2009

Airframe:

Total Time: 1740 Hours Total Landings: 720 Landings

On Smart Parts Plus at $397 / hour

Engines Information:

Left Engine CF- 34- 3B

Serial Number: 950829

ETSN: 1740 Hours

ECSN: 720 Landings

Overhaul Due: On Condition

On GE OnPoint at $161 / hour

APU: Honeywell 36- 150

Serial Number: P-259

TSN: 1194 Hours

On MSP

Capabilities:

• Datalink 2000+ CPDLC, ADS-B Out, RVSM, MNPS, RNAV/PRNAV 1 and 2, RNAV/BRNAV 5, RNP-10 and

VNAV Qualified

• 8.33 kHz Channel Spacing for COMM’s

• FM Immunity for NAV’s

• EU-OPS 1 Qualified

Weights:

Gross Weight (Ramp): 48.300 lbs.

Max Take Off Weight: 48.200 lbs.

Max Landing Weight: 38.000 lbs.

Max Zero Fuel Weight: 32.000 lbs.

True Empty Weight: 26.353.6 lbs.

Avionics:

• 4 LCD 10 x 12 inch display units

• Enhanced authothrottle

• Dual-channel flight director, autopilot and yaw damper system

• Third Honeywell Laseref V IRS

• Third FMS-6000 with coupled lateral and vertical navigation, performance calculations

• Dual GPS-4000A

• Dual NAV-4000 VOR/LOC, Glide slope, ADF and Marker Beacon Receiver

• Dual HF-9031A

• Third VHF-4000 Comm, 8.33/25 kHz

• Single ALT-4000 radio altimeter

• Two hour solid state CVR

Right Engine CF- 34- 3B

Serial Number: 950830

ETSN: 1740 Hours

ECSN: 720 Landings

Overhaul Due: On Condition

On GE OnPoint at $161 / hour



Avionics (Cont.):

• Dual TDR-94D mode S transponder with Enhanced Surveillance capability and ADB-S Out capability

• Honeywell Enhanced GPWS

• Artex 406 satellite ELT with nav interface

• Digital Clock with GPS updating

• EICAS, system synoptics

• Integrated Electronic Standby Instrument

• Dual RVSM ADC-850E

• Dual three-channel DME-4000

• Single two-channel Coltech HF SELCAL

• Avtech intercom and audio system

• TWR-850 Turbulence Weather Radar System

• JAROPS 1, Part 135 (9 pax) FDR

• TTR-4000 TCAS II Change 7.1

• Single data loader

• Access door annunciator

• Standby magnetic compass

• CAT II capable

• MDC-3110 maintenance diagnostic computer

Additional Avionics and SB´S:

• Installation of Honeywell Runway Awareness and Advisory System (RAAS)

• Replacement of a Collins TCAS II Bottom Omni Directional Antenna (Super Systems) with a Collins TCAS II

Bottom Directional Antenna in accordance with STC No. SA8133NM-D.

• Modification· Datalink System· Upgrade Datalink System to meet the Eurocontrol’s requirements

Link 2000+ Requirement (C23·440) by Bombardier

• SB 605-23-007, with VHF-4000 modified by Collins SB VHF-4000()-23-11

• SB 605-23-001, Rev 01 VHF System lnst. of third VHF (3RD VHF) .

• SB 605-23-002, Rev 01 Basic, Data Transmission Datalink System

• SB 605-31-003, Rev NC Upgrade the Adaptive Flight Displays (AFD) to " -204" and Incorporation of Rockwell

Collins Service Bulletins for Reliability Improvements

• SB 605-31-004, Rev NC Installation of Insulation Blankets to Control Condensation

• SB 605-34-001, Rev 01 Flight Management System -Installation of the Third Flight Management System

(FMS)

• SB 605-34-002, Rev NC Flight Management system (3DMAP-LRC) 3D MAP and Long Range Cruise

• SB 605-34-004, Rev 02 Inertial Reference System -Installation of the Third Inertial Reference (IRS 3)

• SB 605-34-006, Rev 01 Lightning Detec. System lnst. of LOS

• Installation of the Universal Graphical Weather on the Multi-Function Display (MFD)

• SB 605-34-013 Rev 02, ATC Transponder System – Incorporation of ATC Transponder Part N 622-9210-409

with Automatic Dependent Surveillance – Broadcast (ADS-B) Out capability



Additional Equipment:

• Complete Custom Aircraft Interior in accordance with Aero Consulting Services Ud. Configuration

• Definition List E934000 updated to Revision CQ and Modification data summary G294000 Revision NC

• FAA Approval is ST02355NY.

• SB 605-25-001, Rev 02 lnstl, of the Entry Headliner Strucl., the Cabin Primary Insulation Blanket and the top

cover.

• Installation of Emergency Vision Assurance System (EVAS) in accordance with Vision Safe MOL 176

• Rev. E, F-AA approval is ST01012WI.

• Pulsating landing lights

• SB 605-36-001 , Rev NC 10th Stage Bleed-Air Pressure Transducers Relocation

• SB 605-46-002, Rev 01

• Sixteen 115 VAC /60Hz Electrical Outlets

• Cockpit Refuel/Defuel Panel Option

• Aft Equipment Bay access ladder

• Aft Equipment Bay storage box

• Catwalk Battery Access

• Keyed Locking Fuel Caps

• Common Key Panels in external doors

• LED Cabin Lighting

• Aerolux Nesspreso Coffee Maker

• TIA Microwave Oven & TIA Convection Oven

• Maintenance Database CAMP Enrolled

• Rockwell Collins FMS Nav and E-Maps Database Enrolled

Interior:

• Configuration for 9 Passengers

• One Fwd Pull-Out In-Flight Seat (Jumpseat)

• Four Single wide executive seats with recliner style footrests, berthable/recline, and swivel capability

• Two Single wide executive seats with recliner style footrests, berthable/recline, and swivel capability

• One 3-place berthable 16G divan

Entertainment:

• Two dual multi-region CD/DVD players combined unit

• Two bulkhead-mounted 21.3-inch LCD video monitors in passenger cabin

• Airshow ASXi interactive In-Flight information system (moving map) incl. Audi Briefings (English & Spanish)





















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Bombardier Challenger 605 - Southern Cross … · • Definition List E934000 updated to Revision CQ and Modification data ... • Aft Equipment Bay access ... Bombardier Challenger