|
|
Airframe: |
| TTAF: |
2,206 hrs |
| Landings: |
1,012 |
|
|
Engines: |
|
Type: |
Rolls Royce BR700-710C4-11 |
|
|
#1 (Left) |
#2 (Right) |
|
S/N: |
15173 |
15172 |
|
TSN: |
2,206 hrs |
2,206 hrs |
|
Cycles: |
1,012 |
1,012 |
|
Midlife Due: |
3,750 |
3,750 |
|
O/H Due: |
7,750 |
7,750 |
|
|
APU: |
| Type: |
Honeywell RE 220 |
| S/N: |
P-346 |
|
TSN: |
1,343 |
|
O/H Frequency: |
On condition |
|
|
Maintenance / Inspections: |
|
12/24/48 month inspections c/w at Gulfstream, September 2008 at 1,912 AF hours.
|
|
|
Avionics: |
| COM: |
Honeywell Primus II Epic Dual MRC 855 with Primus II 3rd Com |
| NAV: |
Honeywell Primus II Epic Dual MRC 855 |
| FDS: |
Honeywell Primus Epic GP 500 Flight Guidance Panel |
| A/P: |
Honeywell Primus Epic GP 500 Flight Guidance Panel |
| XPNDR: |
Honeywell Primus II Epic Dual Mode S Diversity Enhanced Flight ID |
| ADF: |
Honeywell Primus II Epic Dual MRC 855A - DF 855 |
| DME: |
Honeywell Primus II Epic Dual MRC 855A - DM 855 |
| ADC: |
Triple Honeywell AZ 200 |
| FMS: |
Honeywell Primus Epic Triple Flight Management Systems |
| GPS: |
Dual Honeywell GPS 24 Channel |
| AFIS: |
Satellite AFIS with Cockpit Printer |
| STCOM: |
Honeywell MCS 7000 7 Channel with Magnastar Interface |
| HFCOM: |
Honeywell Dual |
| FFONE: |
Magnastar with 1 cockpit handsets and 5 cabin handsets |
| EFIS: |
Honeywell Four DU 1310 Flat Panel Displays with Triple MC 850s |
| RADAR: |
Honeywell WU 880 with Dual WC-884 Controllers |
| RADALT: |
Honeywell Dual RT 300 |
| TCAS
II: |
Honeywell RT 951 TCAS 2000 with Change 7 |
| EGPWS: |
Dual Honeywell Enhanced |
| LRNAV: |
Honeywell Triple IR 500 Laseref V Micro Inertial Units |
| FDR: |
L3 |
| CVR: |
L3 |
| ELT: |
Artex 406 MGHZ C-406-2 with NAV interface |
| Audio
Panels : |
Honeywell Triple AV-900 |
|
|
Additional Equipment
and Features: |
Gulfstream Certification "E" Synthetic Vision System
Certification "D" (software upgrade) complied with
RVSM Capable
MNPS Capable
FM Immunity Compliant
RNP 5 & 10 Compliant
8.33 Spacing Compliant
TAWS Compliant
Thrust Reversers
Honeywell Visual Guidance System (HUD, EVS)
Goodrich Magnetometer
Goodrich GH 3100 Standby Attitude/Airspeed/Altitude Indicator
Goodrich EBDI 4000 RMI
Dual Mason Cursor Control Devices
Miltope Cockpit Printer
Honeywell Triple MAU Modular Avionics Units
Additional Equipment & Features continued:
Honeywell MT-860 Third Navigation Communication Cabinet
Dual Davtron Clocks
Airshow 4000 Cabin Network with RF/IR Touch Screen Remote
Interlink Remote Point RF Mouse System for Airshow Network
Securaplane External Camera System
Dynamo Aviation Cold Storage Unit
Auxiliary Avionics Cooling
LED Wing NAV Lights (ASC 46)
Logo Lights
Wing Tip Taxi Lights
Wheel Well Lights
ATG Power Tech Electric Window Shades
Therapeutic O2 Outlet |
|
|
Interior: |
|
This aircraft has an elegant sixteen passenger, fireblocked interior, a forward crew rest station with one chair, forward crew galley and one certified cockpit jump seat. The forward cabin features a forward four-place club, the mid cabin features a four- place conference with table opposite a credenza and the aft cabin features (2) four-place divans with curtain separating the cabin. All windows include Electric shades.
Aft Galley equipped with dual coffee makers, warming oven, microwave and dynamo aviation cold storage unit.
Forward Crew Galley with ice drawer.
Forward Crew Lavatory and an Aft Lavatory.
The Entertainment System features: Dual DVD systems, VHS, Monitors on FWD and AFT bulkheads, Monitor located over credenza facing conference grouping, Airshow 4000 network, fax interface, provisions for LAN system, touch screen remote controls, RF mouse controls and Securaplane external camera system.
Interior Coverings:
All Club Seats covered in tan Leather
Both Divans covered in Gray fabric
Carpet in Brown with Blue accents
Headliner in Off white
Medium shade burl wood |
|
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Exterior: |
|
Overall Sherwin Williams Snow White with Sherwin Williams light blue, dark blue, chateau margaux and medium gray stripes.
Owner wishes to retain the registration number.
Specifications
as of 10/30/09. 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.
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