Specs
More Information
Year:2006
Make:BOMBARDIER
TTAF:650 Hrs.
Number of landings:228
Engine(s) Manufacturer:Rolls-Royce Deutschland BR710A2-20 turbofans
Engine 1: Time since new:550 Hrs.
Engine 2: Time since new:550 Hrs.
Auxiliary Power Unit: 395 Hours (RE 220GX and 522 cycles)
Maintenance Information: Rolls Royce Corporate Care
Smart Plus
Manufacturer`s Warranties (started on December 1st. 2006)
20 years or 20,000 hours aircraft Primary Metal Structured
5 years or 5,000 hours airframe and systems (excluding completion work)
5 years or 5,000 hours green avionics
6 years or 3,000 hours APU Parts
5 Yeas or 5,000 Hours APU Labor
2 Years or 2,000 hours Paint and Completion work
Engine Maintenance Plan:on Rolls Royce Corporate Care
Airframe Maintenance Plan:on Smart Plus
:: Propeller Info ::
:: Avionics :: Details:
Avionics/Electrical Systems:
- Satellite Communication System and High Speed Link (SAT-6100) IMT44304001
- Thales/Sextant Head-up Flight Display System (HFDS) CAT II operations (Factory/Completion installed)
- Central Aircraft – Information Maintenance System (CAIMS) – Installation of the CAIMS “ Report – to – printer “ switch
- Teledyne Datalink System (ACARS)IMT23234001
- Honeywell RCZ-833 Third VHF Communication System IMT23114001
- Honeywell LSZ-860 Lightning Sensor System (LSS)IMT34474001
- 3rd Honeywell Single Global Positioning (GPS)system
Other Avionics/Electrical System
- Satellite Communication System (SATCOM)
Three (3) channel Aero H+ (INMARSAT) System (2 voice channels and I data channel). Data channel supports ACARS/ maintenance functions.
One (1) single-channel Iridium based airborne telephone system
PBX (Aerocom 3000B) integrates two systems allowing common access from handset
Four (4) passenger cabin hansets (one is cordless). One handset in cockpit
Single channel high speed data system (HST- 2100) offers data transfer of up to 64 KBPS
- Cabin power bus disconnect
- Ground service cabin power
- One (1) power converter (3500VA/115V/60Hz) IMT24264001
- Additional TRU
- EICAS: “Door open” annunciation
- 115VAC GFI electrical outlets located as follows:
A dual outlet in each lavatory and at RH galley, LH galley annex, credenza, and LH entrance enclosure
A single outlet at each single chair and each outboard double chair
:: Special Features :: Details:
Equipment and Systems:
Soundproofing
- Bombardier vibro-acoustic soundproofing package tailored to the layout, and finishing trims
- Enhanced acoustic package.
Oxygen System:
- Factory-installed EROS MF-10 full-face masks are retained for the pilot and co-pilot
- Puritan Bennett “Sweep-On” 2000 half masks for pilot and co-pilot
- Eros MC-20 half mask and MXG goggles at flight observer seat.
- Oxygen drop boxes as required in main cabin as well as galley, lavatories and at jumpseat
- Two (2) therapeutic oxygen outlets in passenger cabin.
Environmental Control System (ECS):
- Passenger control of two cabin temperature zones (+/- 2 deg. C) around master control setting
- Entry area heater
Potable Water System (PWS):
- Re-circulating water system with dual pumps (for redundancy) and UV filter system
- 24.7 Gallon water tank
Cabin Electronic Systems (CES):
10/100 Base T Ethernet LAN with connections for lap tops and portable devices
Plain paper: NT compatible FAX/Printer/Scanner
RJ-45 LAN interface at each single, outboard double seat and in the cockpit
Wireless LAN
- Cabin Utilities/Control and Display
One (1) 10.4 inch galley touch screen control monitor
One (1) Cockpit Touch Screen Equipment (co-pilot side).
Passenger control switch panels, entertainment switch panel and local switch panels
Two (2) IR remote controls
- Power Distribution of aircraft AC and DC power
- Entertainment
Two (2) multi-region DVD players
One (1) multi-disk CD player
Two (2) bulkhead-mounted 21.3-inch LCD video monitors
High Quality Cabin Speaker/Subwoofer Arragement (10 speakers & 4 suwoofers)
Eight (8) receptacles for plug in monitors (4 plug in monitors are included)
Passenger headphone distribution
Airshow moving map
Cabin Services
Cabin/Lavatory Call System
Passenger Address System
Telephone system (PBX)
Passenger briefing system
ICG ICS-200 Iridium Telephone system
- Maintenance and Diagnostics
Central maintenance function for applicable integrated cabin systems
Diagnostic report viewing on the galley touch screen monitor
Lighting:
- LED interior lighting
- Exterior ground service lights (pylon lights)
- Wing tip taxi lights IMT33424001
- Pulse landing light system
- Wheel-well maintenance lights(factory installed)
- Logo lights
- Services lights timer override
- Exterior service panel lighting
Miscellaneous Installations and Equipment:
- Aircraft miscellaneous installations
Additional refuel-defuel panel IMT28234001
Forward handrail extension
Common keyed panel locks
Aft equipment bay storage box (30lb. maximum)
Crew plaque
Semi recessed Jeppesen manual storage box at cockpit entrance
Towbar and assembly storage (towbar is loose equipment)
Cockpit miscellaneous equipment
Two (2) engraved Maglite rechargeable flaslights
Two (2) roller screens
Two (2) writing pad holders
Thale Integrated Standby Instrument (ISIS)
- Galley miscellaneous equipment
10-cup, manual fill coffeemaker (TIA Model 1603)
Aerolux Nespresso manual fill coffee maker (AL –EX15-200E-17)
Chiller-cooled cold food storage
One divided ice drawer with overboard drain
High temp oven with digital controller (TIA Model) 1545-3
0.7 cu ft. microwave oven (TIA)
- Passenger cabin miscellaneous equipment
Electrically operated accordion style window shades
Eight (8) ledge storage boxes one at each single and double seat location
Additional Aft cabin window (S/B 700-56 -001 FS 788 RHS)
Emergency Equipment:
- Smoke detector in each lavatory, in aft wardrobe and in baggage (factory-installed)
- Life rafts, life vests, PBEs, fire extinguishers, and first aid kit as required
- Engraved Maglite flashlight (in addition to (2) cockpit flashlights)
Production-Installed Avionics:
Honeywell Primus 2000XP Integrated Avionics System
Production-Installed Avionics
Six 8x7 inch color CRT Display Units (DU-870) - 2 Primary Flight Display PFD, 2 Multifunction Display MFD, 1 EICAS and I System Synoptic Display
Three IC-800 Integrated Avionics Computers (IAC), each responsible for the following functions: I/O processor, ASCB controller, Electronic Display System EDS, Flight Management Computer, Autothrottle Control, Flight Guidance Computer FGC
Triple long-range navigation sources:
Triple integrated NZ-2000 Flight Management System with CD-820 CDUs
One DL - 800 data loader
One Lasertrack Navigation Data Unit (NDU)
Triple LASERREF IV Inertial Reference System (IRS)
Dual Primus II Nav/Com system with 25 KHz or 8.33 KHz channel spacing
Triple AZ-840 Micro Air Data Computers (MADC)
Dual Automatic Flight Control System (AFCS)
Primus 880 weather radar with dual Weather Radar Controllers
Dual full flight regime autothrottle
TCAS II TCZ-910 Traffic Alert and Collision Avoidance System with change 7 software upgrade
Triple Global Positioning System (GPS)
Central Aircraft Information and Maintenance System (CAIMS)
• Other Honeywell Systems (formally Allied Signal):
Enhance Ground Proximity Warning System (EGPWS)
Flight Data Recorder (FDR - 57 parameters part 91 only)
Solid State Cockpit Voice Recorder (SSCVR) – 4 channel recording with 2 hour duration
Collins Systems:
Dual ALT-4000 radio altimeter systems
Dual HF-9000 High Frequency (HF) communications system
• Coltech System:
Coltech CSD-714 Selective Calling System (SELCAL)
• Other
Artex ELT with NAV interface unit
External service panel lighting
:: Exterior ::
:: Interior :: Details:
Entrance Area:
- RH forward lavatory: vacuum toilet, vanity and sink
- LH entrance enclosure: cockpit flight observer seat (jumpseat), coat rod, storage areas and crew oxygen mask.
- RH galley: refer to list below for specifics of equipment
- LH galley annex with:10.4” Touch screen control panel, refer to list below for specifics of equipment
- Forward cabin bulkheads with LH sliding pocket door (separates entrance area from cabin)
Forward Cabin:
- RH side (zone 1A): One (1) pull – out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
- LH side (zone 1B): One (1) pull-out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
- Two (2) magazine racks-one (1) on each RHS & LHS fwd bulkheads
Mid Cabin:
- RH Side (zone 2A): Credenza cabinet including entertainment and FAX/printer. Low cabinet under emergency exit including miscellaneous storage
- LH side (zone 2B): One (1) manually-operated hi-low conference table and two (2) sets of low back, double seats that feature: integral headrest, recline, track & swivel ( swivel on inboard chairs only), and electric inflatable lumbar
- Mid cabin bulkhead on LHS, LHS pocket door and RHS removable bulkhead.
Aft Cabin:
- RH side (Zone 3A): 3-place 16G divan (forward seat position can be occupied when RH mid cabin bulkhead is removed) that also features: berthing and storage. Two (2) end cabinets, each features: (2) drink holders, storage, and CME interface
- LH side (Zone 3B): One (1) pull-out table and two (2) wide, low back, single executive seats that feature: integral headrest, recliner footrest, berthing/recline, track & swivel, and electric inflatable lumbar
Aft Lavatory Zone:
- Aft cabin bulkheads and hinged door
- Vacuum toilet
- Vanity cabinet with miscellaneous storage
- Wardrobe and storage cabinet featuring adjustable and fixed shelving
Baggage Compartment Area
- Approximately 145 cu. Ft.
- Two (2) fold-down shelves
- Two (2) hang-up bars (one swings down to stow)
:: Weights :: MTOGW89,700 (40,687 kg) lbs
RAMP89,900 (40,778 kg) lbs
ZFW56,000 (25,401 kg) lbs
LANDING78,600 (35,652 kg) lbs
BOW50,830 (23,054 kg) lbs
FUEL WT36,000 (16,329 kg) lbs
