2008 HAWKER 750 - AD #: AC52
This is a Brand New Hawker 750 just purchased in Dec 2008. Still under warranty . Also available for Charter. Please bring all offers!
Specifications
| Ad #: | AC52 |
| Manufacturer: | HAWKER |
| Model: | 750 |
| Year: | 2008 |
| Type: | Business Jet |
| Quick Details: | The new Hawker 750 is designed to satisfy the market’s unmet need for a high-performance, ultra-comfortable light-midsize business jet. A derivative of the famed Hawker 800-series airframe, the Hawker 750 refines its predecessor’s capabilities even fur |
| City: | Orlando |
| State/Province: | FL |
| Postal Code: | 32801 |
| Country: | US |
| Engine Hours: | 300 |
| Asking Price | $9,900,000.00 |
| Willing to trade for: | This is a Brand New Hawker 750 just purchased in Dec 2008. Still under warranty . Also available for Charter. Please bring all offers! |
1.
2008 Hawker 750 Specifications
AirCell ST3100 iridium phone w/cordless cockpit
Electronic Charts
United States Weather
Single Collins HF-9000 HF Comm System with SELCAL
2nd Collins FMS-6000 FMS / GPS-4000A
2nd Graphical AFD-3010E Display and Cursor Control
Airshow 410 w/Flight Deck Controller
2nd 15” LCD Monitor
Power Outlet and Auxiliary A/V Package – 110
Cabin audio/video entertainment system
XM radio – 2 Channel System
Enhanced Refreshment Center Package
Precise Flight Pulselite system w/TCAS interface
Dual panel cockpit doors
Pyramid style cabinet
Wood Veneer Cabinetry (incl side edges)
Additional stowage drawers under each club chair
Drop down inboard armrests (all individual seats)
Belted lavatory seat
Two Honeywell Aerospace Engines Model #TFE731-5BR-1H
COLLINS PRO LINE 21 AVIONICS
Comm 1 - Collins VHF-4000 digital CNS radio transceiver (118.000
to 136.975 MHz in 8.33 KHz spacing increments), tuning
through either CDU-6200 or through CTL-23C
Comm 2 - Collins VHF-4000 digital CNS radio transceiver (118.000
to 136.975 MHz in 8.33 KHz spacing increments), tuning
through either CDU-6200
Nav 1 - Collins NAV-4000 VOR/LOC/GLS/ ADF/marker beacon
receiver, tuning through either CDU-6200 or through the CTL-
23C
Nav 2 - Collins NAV-4500 VOR/LOC/GLS /marker beacon receiver,
tuning through either CDU-6200
IFIS - Collins Integrated Flight Information System with single FSU-
5010 File Server Unit
GPS - single Collins GPS-4000A 12 channel GPS receiver
Full Performance FMS Database (performance and V speeds)
Transponders - dual TDR-94D, enhanced surveillance with Flight
ID, diversity transponders with dual antennas, tuning through
either CDU-6200
DME - dual Collins DME-4000 with DME information being
displayed on AFD’s
AHRS - dual Collins AHC-3000 attitude heading reference system
includes: dual FDU-3000 flux detector units, slaved and DG
heading modes
ADC - dual Collins ADC-3000 air data computers - RVSM capable
altimetry system
FMS - single Collins FMS-6000 flight management system with
navigational inputs from GPS receiver, Nav’s, and DME’s
CDU - dual Collins CDU-6200 control display units for FMS and
radio control
Flight display system - Pro Line 21 system with three AFD-3010
adaptive flight displays (pilot’s PFD and MFD and copilot’s PFD)
and one graphical AFD-3010E adaptive flight display (copilot’s
MFD); pilot’s MFD incorporates an engine indicating (EI) system
Checklist display - normal and emergency checklists displayed on
copilot’s MFD - operator checklist edit software provided
Maintenance diagnostics computer - Collins MDC-3110
maintenance diagnostics computer, displays maintenance
information on MFD and downloads through the DBU-4100
(shared with the FMS)
Automatic flight guidance system - dual Collins FGC-3000 flight
guidance computers, single autopilot system, yaw damper, FGP-
3000 flight guidance panel, and mach trim (integral to autopilot
system) - system has Category II approach capability
Audio system - dual dB systems digital control audio panels
Cockpit voice recorder - Universal CVR-120 with 2 hour recording
capability
Weather radar - Collins TWR-850 turbulence weather radar (RTA-
858 receiver/transmitter/ antenna) with display capability on any
AFD
Radio altimeter - single Collins ALT-4000 radio altimeter, measures
altitude up to 2,500 feet AGL, displayed on PFD’s
TCAS II - Collins TCAS-4000 traffic alert collision avoidance system
Secondary flight display system - Meggitt Mark II secondary flight
display system with independent air data unit - displays attitude,
altitude, airspeed, heading, Nav course deviation, and glideslope
Standby radio tuner - Collins CTL-23C
ELT - Artex C406-N (SAR type) with integral latitude/ longitude
information
Angle-of-attack system with remote mechanical AOA indicator
adjacent to pilot’s PFD (with selected V
ref
setting being indexed
by marker on the airspeed tape)
EGPWS - Honeywell Mark V enhanced ground proximity warning
system (EGPWS) with wind shear detection (satisfies FAA Class A
& B TAWS requirements)
Cockpit speaker inhibit switch
Collins FMS database update service-1
st
year only
Enhanced Map Overlays with one year subscription
2. ENGINES
Two Honeywell TFE 731-5BR engines (rated 4,660 lb thrust each)
Thrust reversers
DEEC - digital electronic engine controller with engine condition trend
monitoring (ECTM), download of ECTM data provided through
connectors located in area adjacent to refuel panel in forward
baggage header
Engine fire detection system
Engine fire extinguishing system
Engine synchronizer
3. FLIGHT CONTROL SYSTEM
Mechanical primary flight controls
Manual roll and rudder trim
Electric and manual pitch trim
Hydraulic flaps/lift dump
Hydraulic spoilers/speed brakes
Dual stall warning system
Asymmetric flap detection system
Angle of attack system
4. HYDRAULIC
Two engine driven pumps (3000 PSI)
2.4 gallon pressurized system
Ground service connections
Emergency hydraulic system
HAWKER 750 STANDARD EQUIPMENT LIST
(HB-6 THRU HB-33)
Aircraft Offered Subject To Prior Sale: Standard Equipment And Price Subject To Change Without Notice
2
HAWKER BEECHCRAFT CORPORATIONHAWKER BEECHCRAFT CORPORATION
HAWKER BEECHCRAFT CORPORATION
|2008_750_custver_stdequip_6-33_rev3_hbc.doc 5/29/08
5. LANDING GEAR AND BRAKES
Hydraulic extension and retraction system
Dual nose gear wheels and tire
Dual main gear wheels and tires
Emergency gear extension system
Hydraulic nose wheel steering
Anti-skid system (Maxaret
©
)
Parking brake
6. ELECTRICAL
Two starter/generators, 400 Ampere 28.5V D.C.
Dual 24V maintenance free lead acid batteries
External power receptacle
Over-voltage protection
Reverse current protection
Feeder fault protection
Honeywell 36-150[W] APU (approved for in-flight operation up to
30,000 feet)
7. INTERNAL LIGHTS
Internally-lit instruments
Electroluminescent switch panels and control placards
Standby instrument lights
Cockpit ceiling lights
Two overhead map lights with rheostats
Emteq LED lighting throughout the cabin including:
Emergency exit lights
Upwash lights
Reading lights above each passenger seat
Flood light above each console table
Aisle lights in the aisle side panels
Exit light over the main entry door
Lights in the closet/baggage area
8. EXTERNAL LIGHTS
HID (High Intensity Discharge) taxi/recognition lights and landing lights
Wing tips (incandescent) and tail (LED) navigation lights
Wing tips and tail strobe lights
Wing ice inspection lights
Beacon
Vertical tail illumination lights (logo)
Maintenance lighting in wheel bays
9. FUEL SYSTEMS
8,500 lb fuel capacity
Low fuel quantity warning system
Fuel temperature indicator
Cross-feed and fuel transfer capability
Two engine-driven fuel pumps
Two ejector jet pumps
Two fuel boost pumps (electric)
10. ENVIRONMENTAL
Three wheel air cycle machine
Bleed air pressurization system (8.55 max PSI)
Automatic/manual mode selector
Dual zone cabin and cockpit temperature system
11. PRESSURIZATION
Automatic pressurization controller
Manual depressurization control valve
Quick dump valve
Low cabin pressure annunciator
Two outflow valves
Cabin altitude limiters
Emergency pressurization
12.OXYGEN
2 x 750 liter oxygen bottles
Two diluter - demand regulated crew masks with microphones (EROS)
7.2 cu. ft. portable walkaround O
2
cylinder on cabin floor
Supplemental O
2
in cabin
13. DE-ICE/ANTI-ICE AND RAIN
Engine inlet anti-ice (bleed air)
Wing leading edge de-ice/anti-ice (TKS fluid with 10 gallon capacity)
Windshield anti-ice (electric heat)
Horizontal stabilizer de-ice/anti-ice (fluid)
Pitot-static system anti-ice (electric heat)
Angle of attack (AOA) transmitter anti-ice (electric heat)
14. CONTROLS AND INSTRUMENTATION: PILOT’S PANEL
Two AFD-3010 adaptive flight displays (AFD)- PFD and MFD
Angle of attack (AOA) indicator
Audio control panel
Master warning light
Display control panel (DCP)
CVR control panel
Writing surface with pencil holder
Instrument lighting controls
15. CONTROLS AND INSTRUMENTATION: COPILOT’S PANEL
One AFD-3010 adaptive flight display (AFD)- PFD
One graphical AFD-3010E adaptive flight display (AFD)- MFD
Oxygen pressure indicator
Cabin altitude/differential pressure indicator
HAWKER 750 STANDARD EQUIPMENT LIST
(HB-6 THRU HB-33)
Aircraft Offered Subject To Prior Sale: Standard Equipment And Price Subject To Change Without Notice
HAWKER BEECHCRAFT CORPORATION
| 2008_750_custver_stdequip_6-33_rev3_hbc.doc 5/29/08
3
Pressurization control panel
Audio control panel
Master warning light
Display control panel (DCP)
CTL-23C standby radio tuner
Cursor control panel (CCP)
Writing surface with pencil holder
Instrument lighting controls
16. CONTROLS AND INSTRUMENTATION:
CENTER PANEL/PEDESTAL/OVERHEAD PANEL
Dual control display units (CDU’s)
Flight guidance panel
Rudder trim control and indicator
Aileron trim control and indicator
Pitch trim control and indicator
Fuel temperature indicator
Thrust reverser control panel
Hydraulic pressure/brake pressure indicator
Landing gear control lever with position indicator lights
Warning and caution annunciator panel
Electronic standby instrument system (ESIS)
Secondary flight display system
Standby magnetic compass
Audible overspeed warning
Audible take-off out of trim warning
Audible landing gear warning
Stall annunciator’s and aural stall warning
Engine fire warning lights
Engine thrust/thrust reverser levers
Flap selector/flap position indicator
Air brake handle
Battery master switch
D.C. volt meter with select switch
Two boost pump switches
Two generator reset switches
Two engine fire extinguisher discharge switches
Environmental control panel
Fuel cross-feed transfer controls
17. EXTERNAL BAGGAGE
Externally accessed baggage; approximately 32 cu ft, 500 lbs
capacity
Heated, unpressurized
Smoke detector with fire extinguishing system
18. INTERIOR MATERIAL SELECTIONS
Standard carpet colors
Standard leather color palette
Standard fabric selection
Standard countertop material selection
Standard metal plating palette
19. CABIN
Collins Airshow 21 Cabin Management System
50” closet/baggage compartment
Smoke detector in the closet/baggage compartment
One BCF Halon fire extinguisher provided and mounted on the cabin
floor, aft of the forward left hand cabin bulkhead
Refuel control panel located in the upper section of the forward
stowage compartment
General stowage in the upper section of the center stowage
compartment
General stowage in the upper section of the rear stowage
compartment
2 coat rods - one full length (fore/aft orientation) in R/H forward
baggage compartment and one in aft closet
TKS access door with funnel - aft face of the vestibule/crew cabinet
Access for TKS filter under forward left hand refreshment center
Two each coat hooks on aft face of the crew cabinet
Main entrance door fold over hand rail
Main entrance door boarding lights - first and third steps
Main entrance door second step - ground equipment stowage
compartment
High gloss finish wood laminate with hardwood molding cabinetry and
leather wrapped bulkheads
Galley, 24” wide, forward left hand includes: two hot prepcos,
miniature liquor storage, ice/cold stowage drawer with heated
overboard drain, and large waste bin
Fold down acoustic main entry door curtain
Plug in style jump seat
Leather wrapped side ledge in main cabin
Dual drink holders at each seat
Lower side panel with single fabric finish
One conditioned air duct on each side of cabin at floor level
Flood duct
Five ERDA chairs with Hawker 750 styling/design that have adjustable
recline with separate control, 360° concentric swivel, side motion,
five inch base with telescoping integral headrest. Metal to metal
type seat belts, full berthing capability, magazine pocket in the seat
back. A lever is installed to control forward and aft movement on
the seat tracks, which are exposed
HAWKER 750 STANDARD EQUIPMENT LIST
(HB-6 THRU HB-33)
Aircraft Offered Subject To Prior Sale: Standard Equipment And Price Subject To Change Without Notice
4
HAWKER BEECHCRAFT CORPORATIONHAWKER BEECHCRAFT CORPORATION
HAWKER BEECHCRAFT CORPORATION
|2008_750_custver_stdequip_6-33_rev3_hbc.doc 5/29/08
Three place divan includes: break over forward arm rest, metal to
metal seat belts and shoulder restraints, drink holder is mounted in
each end armrest, stowage in forward and aft arms, stowage
underneath forward and middle seat cushions in Kydex tubs with
access through two piano hinged doors on aisle side of divan, and
two comfort throw pillows
Cockpit call switches located within the VIP touch screen panel and in
the lavatory
First aid kit stowed in the rear lavatory toilet seat back
Cabin paging and speaker system - cockpit to cabin paging and
speaker system with four cabin speakers
Soundproofing in the cabin, forward entrance area and lavatory
Console tables
“No Smoking - Fasten Seat Belts” signs with audible chime
One color 3.8” LCD touch screen VIP control panel located adjacent to
right hand forward facing chair contains cabin temperature, cabin
lighting on/off, bright/dim/off control functions
Six color 3.8” LCD touch screen passenger control panels control
reading light on/off, table flood light on/off
Cabin/lavatory door hinged on right side
Rear closet 21” wide forward of the rear right hand cabin bulkhead
includes luggage restraint net, coat rod, closet curtain,
miscellaneous stowage compartment above the coat hanging space,
and a light
Lavatory with a flushing toilet, external servicing, metal wash basin
plated same as latches and mounted in Corian, and smoke detector
Threshold rug
Entry rug
Three throw rugs between the seats
Vinyl maintenance runner extends from aft face of crew cabinet to the
rear of toilet compartment
Cabin chair maintenance covers (5 total)
Divan maintenance cover
Access panel for electrical components outboard of lavatory seatback
Passenger briefer cards (12 each) will be provided
Sealth Aero Marine (SAM) latches installed in all cabin furnishings
20. COCKPIT
Two IPECO crew seats upholstered with sheepskin to match cockpit
interior
Microphone boot on each yoke
Two cup holders
Headset/interphone stowage for 3
rd
crew member
Rosen sun visor system
Seat belts and harnesses
Jepps manual stowage with removable dividers
Two Scott EROS full face oxygen/smoke masks
Connectors for Collins CPAS-3000 portable access software system
located in lower crew cabinet
Spring style penholder
21. EXTERIOR PAINT SCHEMES
Standard exterior layout with standard paint colors to be maximum
two color stripe design
22. PUBLICATIONS
Airplane flight manual
Pilot’s operating manual
Abbreviated checklist
Log books (aircraft, engine, main batteries, emergency batteries, APU)
Major assembly record
Maintenance manual with maintenance requirement data and tool
equipment manual
Operator manuals for avionics equipment
Illustrated parts catalog
Wiring parts catalog
Maintenance schedule
Overhaul manual
Structural repair manual
Non destructive test manual
Engine maintenance manual
Engine parts catalog
Wiring diagram manuals
APU maintenance manual and illustrated parts catalog
23. LOOSE EQUIPMENT*
*Note: additional loose equipment and technical publications not specified here may also
be supplied
Aircraft model
MFD checklist edit software
Collins CPAS-3000 portable access software
First aid kit
Two flashlights (cockpit sidewall)
Two Halon fire extinguishers**, cockpit and cabin
**Warning - contains Halon substance which harms public health and environment
by destroying ozone in the upper atmosphere
Engine intake/thrust reverser covers
Pitot covers
Emergency escape hatch ground locking pin and flag
Door maintenance cable
Medeco keys for exterior panels and doors (all keyed alike)
Static and stall vent covers
Life vests (12 each)
Telex headsets (3 each)
Tool bag and miscellaneous hand tools
Fuel sampling tool
Fire ax
Landing gear locking pins
HAWKER 750 STANDARD EQUIPMENT LIST
(HB-6 THRU HB-33)
Aircraft Offered Subject To Prior Sale: Standard Equipment And Price Subject To Change Without Notice
HAWKER BEECHCRAFT CORPORATION
| 2008_750_custver_stdequip_6-33_rev3_hbc.doc 5/29/08
5
Jack pads
Dorsal intake plug
24. TRAINING*
Pilot Training: Two (2) pilots to type rating – Initial course
Minimum pilot qualification prerequisites: valid U.S. FAA Private Pilot Certificate
with multi-engine airplane instrument rating or a valid foreign equivalent, and
1000 hours total airplane pilot time.
Preferred pilot qualifications: valid U.S. FAA Commercial Pilot Certificate with
multi-engine airplane instrument rating or a valid foreign equivalent, 1500
hours total airplane pilot time with 250 hours multi-engine time, and previous
completion of turbine and high altitude training.
Maintenance Training: Two (2) maintenance personnel – Initial
course
Minimum maintenance personnel qualification prerequisites: valid U.S. FAA
Maintenance Technician Certificate or a valid foreign equivalent.
*Notes: All training expires one (1) year after aircraft retail delivery. Optional
training packages may be available. See Aircraft Specification & Description and
consult HBC Sales for further information.
25. GENERAL STANDARD WARRANTY*
Structure (Fuselage, Empennage, Wing and Control Surfaces) – 5
years
Non HBC & HBC manufactured parts - 5 years (3,000 hours),
whichever occurs first.
Collins avionics - 5 years
Honeywell engines - 5 years or 1,800 hours (whichever occurs first,
balance of remaining engine hours at time of delivery)
APU- 5 years or 2,500 hours (whichever occurs first)
Exterior paint and interior finish items - 2 years (600 hours limit),
whichever occurs first
CAMP service - Computerized Aircraft Maintenance Program System -
1
st
year provided at no charge
*Standard warranty coverage is for ‘conventional’ use only. Usage not considered
‘conventional’ includes, but is not limited to, shared ownership fleets,
government/military or special mission operations, flight/pilot training operations
26. REDUCED VERTICAL SEPARATION MINIMUM (RVSM)
SERVICE
Buyer has the option to receive an RVSM service that will provide
the owner/operator with the required material to achieve RVSM
operational approval and Aircraft-specific Minimum Equipment
List (“MEL”) approval from an RVSM service provider
(“Provider”).
Included in the RVSM service, Buyer will receive:
• An Aircraft-specific MEL
• Domestic RVSM Procedures Manual and/or International Operations Manual
• One year of Revision Support Services for the above documents
• Height Monitoring RVSM Validation Flight for collecting data to ensure
autopilot performance
Buyer is responsible for conducting the Height Monitoring RVSM
validation flight within six (6) months from obtaining Operational
RVSM Approval, however HBC customarily arranges for and
conducts a Height Monitoring RVSM validation flight on or
before the acceptance flight at delivery. The Provider will make
every reasonable attempt to provide Buyer with the
documentation required to obtain Operator’s RVSM Operational
Approvals at the time of Aircraft delivery.
However, it is important to understand that the length of time
required for the approval process is controlled by several factors
that are beyond the control of the Provider (i.e. Buyer’s local
regulatory authority). Therefore, Operational Approval, at the
time of Aircraft delivery, is not implied or guaranteed
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