Extremely Long Range
Large Comfortable Cabin
Latest in Technology
6,500 Nautical Mile Range
One U.S. Owner Since New Engines on Rolls Royce Corp Care APU on MSP
2020 Heads-Up Display Honeywell HS 700 High Speed Data Dual FMS with Triple CD 820s EGPWS w/ Windshear and RAAS Enhanced Flight ID Forward Galley Forward & Aft Lavs Excellent Pedigree
On CAMP maintenance tracking program
On MSG 3 aircraft maintenance program
1A Inspection c/w 1/6/2010 @ 5,752 AF hrs, next due 6252 AF hrs.
2A Inspection c/w 9/9/08 @ 5,081 AF hrs, next due 6,081 AF hrs
4A Inspection c/w 1/6/10 @ 5,752 AF hrs, next due 7,750 AF hrs
5A Inspection c/w 3/13/08 @ 4,812 AF hrs, next due 7,312 AF hrs
8A Inspection c/w 4/6/06 @ 3,750 AF hrs, next due 7,750 AF hrs
10A Inspection c/w 3/13/08 @ 4,812 AF hrs, next due 9,812 AF hrs
1C Inspection c/w 4/1/10 @ 5,852 AF hours next due 4/30/11
2C Inspection c/w 4/1/10 @ 5,852 AF hours, next due 4/30/12
3C Inspection c/w 3/27/09 @ 5,319 AF hrs, next due 3/31/12
4C Inspection c/w 4/1/10 @ 5,852 AF hours next due 4/30/14
12C Inspection due 9/30/10
Weight
& Balance:
Empty:
47,267 lbs
Max Takeoff:
90,500 lbs
Max Landing:
75,300 lbs
Avionics:
COM:
Triple Collins VHF 422D with 8.33 Spacing
NAV:
Dual Collins VIR 432
FDS:
Honeywell SPZ 8500
A/P:
Honeywell SPZ 8500
XPNDR:
Dual Collins TDR 94D Mode S with Enhanced
Flight ID
ADF:
Dual Collins ADF 462
DME:
Dual Collins DME 442
ADC:
Triple Honeywell AZ 850 MADC
FMS:
Dual Honeywell IAC FMS systems and single NZ 2000 with 5.2 software and triple CD 820s
GPS:
Dual Honeywell
AFIS:
VHF / Satellite with dedicated cockpit AFIS printer
STCOM:
MCS 7000+ with HS 700 2 channel HSD system
HFCOM:
Dual Collins HF9000 with SELCAL
FFONE:
Magnastar 2000
EFIS:
Honeywell SPZ 8500 6 Tube
RADAR:
Honeywell Primus 880 with LSZ 860 lightning detection sensor
RADALT:
Dual Honeywell RT 300
TCAS
II:
Honeywell TPU 67A TCAS II with Change 7
EGPWS:
Honeywell Mark V with Windshear and RAAS
LRNAV:
Triple Honeywell Laseref IV and single Lasertrak Nav Display Unit
FDR:
B&D Instruments
CVR:
Teledyne Controls
HUD:
Honeywell/GEC Marconi HUD 2020
Flight
Bags:
Single Flight Deck Resources Flight Bag
Additional
Equipment and Features:
RVSM Capable
MNPS / NAT Capable
CAT II Certified
P-RNAV/B-RNAV
RNP 10
FM Immunity Compliant
8.33 Spacing Compliant
TAWS Compliant
Dual Collins RTU 4280 Radio Tuning Units
WSI 300 Satellite Weather System
Genesis Airshow System
Precise Flight Pulse Light System
Meggitt Secondary Flight and NAV Display
Honeywell DL950 Data Loader
Honeywell HS 700 High Speed Data (2 channel)
Foxtronics Battery Temperature Indicating System
All CD 820s are capable of displaying Airshow on the FMS displays
ASC 25 Remote Oiler System
ASC 39 Single DAU for dispatch
ASC 64A Max landing gross weight 75,000 lbs
ASC 81 Max zero fuel gross weight 53,500 lbs
ASC 145A Horizontal Stabilizer Actuator Replacement
ASC 149 Digital Flight Data Recorder Download Port Installation
ASC 152 Cockpit Canopy Vortex Generator Installation
ASC 167 FADEC Modification to G10.2
ASC 159 Vortex Generator Installation and Rib Enforcement
ASC 160 Enhanced Baggage Door Seal System
ASC 168 Rudder Actuator Forward Fitting Replacement
ASC 169 Auxiliary Hydraulic Boost Pump Circuit Protection
ASC 176 Nose Landing Gear Actuator Modification
ASC 178 Rear Spar Fatigue Enhancement
ASC 180 Nose Landing Gear Up lock Hook Spring Replacement
ASC 181 Dual Brake Metering Valve Replacement
ASC 189 Wing Rear Beam Modification Flight Spoiler Actuator Attachment Point
Interior:
This aircraft has a thirteen passenger, fireblocked interior and one certified jump seat. The forward cabin features a RH two place club with a folding work table opposing a four place berthing Divan. The mid cabin includes a LH two place club with a folding work table opposing a single club seat with desk/workstation and storage cabinet. The aft cabin has a LH four place conference group with berthing table and an opposing credenza.
Hard bulkheads and pockets doors separate the galley and the forward cabin and also the forward and mid cabin seating areas. A removable bulkhead and curtain are carried in the aircraft to be installed in flight to separate the mid-cabin and aft cabin creating a private space.
There are phone handsets at each of the following locations: cockpit pedestal, 3rd crew seat, galley, forward Divan area, RH #2 seat, RH #3 VIP seat, LH forward facing seat, and conference table. The cabin also includes electric window shades.
Forward galley equipped with a microwave, convection oven, single coffee maker, sink with hot and cold water, china, crystal and flatware storage and ice storage.
Forward & aft lavs, both flushing, vacuum system, externally serviced and include sink facilities with hot and cold water.
The entertainment system features: Airshow Genesis with a cordless mouse, mid cabin VIP workstation includes a Rosen 20” pop-up monitor, cabin business media center, high speed data router, fax / printer, bulkhead mounted monitor on LH forward cabin bulkhead, aft cabin side panel mounted monitor over credenza, dual swing out individual monitors with close out door at each club seating location, Bose speaker, amplifier and equalizer system, 2 CD changers, one XR 900 AM/FM cassette, 2 VCP 012-401 VCRs and 1 DVD player.
Interior Coverings:
Single Seats covered in Classic Cow Ivory Leather
Four place divan and four place conference group covered in tan fabric
Medium wood
Carpet in tan and blue
Headliner in ivory
Silver burnished fixtures and latches
Partial refurbishment by Duncan Aviation in Battlecreek, MI on 3/14/08 @ 4,813 AF hours. Cabin single seats refoamed/recovered.
Exterior
Colors:
Overall Matterhorn White, Phantom Gray lower fuselage with light Blue, IBM Blue and Royal Blue stripes.
Additional
Information:
For more
information about our services please call us at:
Phone: +1 303-444-6766 Fax: +1 303-444-6866
3025 47th Street, Suite D2
Boulder, Colorado 80301 USA
Or E-mail sales@jetsales.com
Specifications
as of 7/14/10. Specifications are subject to verification upon
inspection
and should not provide a basis for reliance or create any other
binding obligation. Information has been provided by Seller and
has not been independently verified by JMCJSI. Presenting these
aircraft specifications does not constitute the registration of a
client by JMCJSI.