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HAWKER 4000

STANDART EQUIPPED PRICE 20.000.000 USD

SATILDI - SOLD

BENZERİNİ BULABİLİRİZ

    celaluzar@yahoo.com                admin@tayyareci.com  

Standard Equipped  $20,000,000

Introduction

The Hawker 4000 is the newest, most technologically advanced super-midsize business aircraft. Flying faster and farther than its Hawker predecessors, the Hawker 4000 can cruise at speeds up to Mach .84 and has a maximum range up to 3,260 nm. Its advanced swept-wing design, composite fuselage and cutting edge avionics establish a whole new super-midsize category.

We produce the fuselage and empennage, Honeywell integrates and supplies the avionics and electronic systems, Pratt & Whitney Canada furnishes the total propulsion system, and Fuji Heavy Industries builds the totally integrated wing.

The perfect combination of technology, performance, and comfort, the Hawker 4000 represents the future in business aviation.

Hawker 4000 Features and Benefits

The following list captures a few of the major features offered in the Hawker 4000 that make it the best overall value for the jet airplane buyer.  The following pages will outline these and many more advantages you can expect from the Hawker 4000.

	Feature	Benefit
Cabin	Uninterrupted stand-up headroom	Cabin comfort
	Cabin layout flexibility	Variety of interior layouts available
	Internal baggage compartment	Heated, pressurized, accessible in flight
	Fully equipped galley	Passenger appeal
	Low cabin noise levels	Quietest cabin in its class
Paint	High solids urethane paint	Durability – hi gloss
	Custom paint schemes	Styling
	Polyamide corrosion proofing	Long term durability
Cockpit	Advanced Honeywell Epic™ Avionics	Integrated avionics
	Five Hi res. 8” x 10” LCD screens	Greater operational safety
	Dual FMS, EGPWS and TCAS II standard	Safety
	IPECO crew seats as standard	Comfort
Systems	PW308A turbofan engines	Quiet, durable, dependable
	Full Authority Digital Engine Control (FADEC)	Engine protection, eases pilot workload
	Auto-throttle as standard	Ease of operation – reduced workload
	Standard Auxiliary Power Unit (APU)	Convenience
	No wing leading edge devices	Improved dispatch and low maintenance
	Dual Air Cycle Refrigeration Packs	Over water redundancy
	Hydraulic Motor Driven Backup Generator	Over water redundancy
Ops	Seven passenger – full fuel capability	Operational flexibility
	Transcontinental range up to 3,260 nm	Non-stop coast to coast
	High landing gross weight	Multi-stop mission capability

Hawker Design Features

Composite Fuselage

The Hawker 4000 features an all-composite fuselage, built of carbon fiber/epoxy honeycomb which provides unprecedented structural strength, efficiency in design, excellent aerodynamic properties and relative immunity to fatigue and corrosion.

The fuselage has a diameter of 84 inches. Coupled with advanced interior materials and components, the resultant interior cabin offers a width of 6 feet 5½ inches and a flat floor stand-up height of 6 feet.

The baggage compartment is both internally and externally accessible and offers 89 cubic feet of storage capacity.

The aft fuselage section contains an equipment bay which is accessible through an under fuselage door. This bay houses key aircraft components and sub-systems. The in-flight capable Auxiliary Power Unit (APU) is mounted in the aft-most section of the fuselage. The APU is accessible through clamshell-like doors, which provide superior maintainability and accessibility.

Design Features (continued)

New Wing Design

The Hawker 4000 incorporates an all-new wing design. The moderate sweep, supercritical, aft-loaded airfoil offers excellent high speed characteristics for superior cruise and range performance. In addition, the outstanding low speed performance results in exceptional field performance and docile, pilot-friendly handling qualities.

New Empennage

The empennage is an all-new design incorporating a T-tail configuration. The horizontal stabilizer is fully trimmable utilizing a dual-wound electric motor for trim redundancy. The large, powered rudder allows for low pedal forces and excellent engine-out handling qualities.

Pratt & Whitney PW308A Turbofan Engines

The Hawker 4000 is powered by two Pratt & Whitney Canada PW308A high bypass turbofan engines each producing 6,900 lb thrust. The engines are flat rated to ISA+22°C thus assuring exceptional high/hot performance.

Building on the proven technology of the P&WC 300 series of engines, the PW308A features full FADEC (Full Authority Digital Engine Control) which results in exceptional fuel specifics and outstanding operating costs.

The engine is designed to have a 3,000 hour hot section interval and a 6,000 hour TBO. Pratt & Whitney is testing its engines during development so they will debut with mature maintenance intervals, thus saving downtime and operating costs.

Design Features (continued)

Honeywell Primus Epic Avionics

The Integrated Flight Control System and Avionics are provided by Honeywell. The Honeywell Primus Epic™ system features a five panel display format utilizing 10 x 8 inch LCD displays that provide crisp display quality under all light conditions. In addition to the two Primary Flight Displays and the two Multifunction Displays, the Epic system features an EICAS display (Engine Indicating and Crew Alerting System) with Synoptics.

The Honeywell Primus Epic™ system is an avionics suite built on the advanced avionics of the Boeing 777. The avionics system includes an integrated performance computer in the FMS coupled to a full-authority auto-throttle system.

Standard Auto-throttle

The Hawker 4000 has an auto throttle system through the flight management system. The auto throttle automatically positions the throttle levers to control the aircrafts thrust throughout the flight regime. The auto throttle is fully integrated with the aircraft’s Automatic Flight Control System.

Standard LASEREF V Micro Inertial Reference System

The duel Honeywell LASEREF V Micro IRS provides attitude, heading and position parameters with unmatched precision which makes the Hawker 4000 completely independent from ground based navigation aids.

Standard APU

An in-flight capable Auxiliary Power Unit (APU) fitted as standard, to provide electrical power and air-conditioning while the aircraft is on the ground (without the need to start the aircraft’s main engines) or for system back-up in the air.

Large Baggage Capacity

An 89 cubic feet / 990 lb. baggage compartment is located behind the full-service lavatory and is accessible both on the ground and during flight. Baggage can be loaded from outside through a large external baggage door. The sill height of the baggage bay opening makes loading easy particularly large loads or cumbersome items like skis or golf clubs.

Low Operating Costs

From the early stages of design, the Integrated Product Teams working on the Hawker 4000 Program have focused on Reliability, Maintainability, Safety and Operating Costs. The use of CATIA (Computer Assisted Three-dimensional Interactive Application) combined with experienced Logistics and Product Support teams ensure optimum component placement resulting in low maintenance and parts costs.

10 Year Airframe Warranty

The Hawker 4000 comes with a full 10 year/10,000 hour airframe warranty. The Pratt & Whitney PW308A engine, nacelle and reverser have a 5 years/3,000 hour warranty with a 5-year warranty for the Honeywell Epic Avionics Suite. Parts not manufactured by the company are warranted for 5 years / 5,000 hours with warranty for 2 years/800 hours for exterior paint and interior items.

Hawker Cabin Comfort

The Hawker 4000 features a functionally designed cabin, which provides passengers an environment conducive to both long-range and short-distance missions. The passenger cabin is divided into three sections; the vestibule area, housing the galley and storage, the cabin section and the aft lavatory section.

The passenger cabin features a flat floor throughout the entire length and extending into the baggage compartment.

A standard eight-place interior configuration is provided with the Hawker 4000 although the ability to customize your interior is available. The standard layout consists of the following:

Eight Fully Articulating Executive Seats

Each seat features full recline and 360° swivel. Positioned together, the seats can be reclined and berthed for comfortable sleeping on long distance flights.

Excellent Cabin Amenities

The Hawker 4000 features excellent cabin amenities including 24 inch wide tables between each Club Four arrangement. Standard cabin features include DVD video player and cabin climate control. A wide variety of materials and cabin finishes can be selected.

Fully Equipped Galley

The Hawker 4000 features a full service galley including hot/cold water, coffee maker and microwave oven.

Lavatory Compartment

A fully functioning, externally serviceable lavatory including flushing toilet and complete vanity is included as standard.

Hawker 4000 Cabin Dimensions

Hawker 4000 ‘Standard’ Eight Place Arrangement

Payload vs. Range

The Hawker 4000 design weights allow a maximum payload capability of 2,300 lb., which can be carried 2,855 nm.

With a typical payload of 6 passengers and baggage (1,200 lb.) the Hawker 4000 can fly 2,970 nm at Mach 0.82 and with a slightly reduced speed to Mach 0.78 can achieve a maximum range of over 3,150 nm.

Time to Climb

At 39,500 lb. the Hawker 4000 can climb directly to FL410 in just 19 minutes.

Cruising Speeds

The Hawker 4000 typically cruises at speeds up to M0.84 (the MMo is M0.84). High Speed Cruise is M0.82, Intermediate ( Normal ) Speed Cruise is M0.80.  A Long Range Cruise speed of M0.78 provides optimum range / time combination.

Hawker 4000 Cruise Speeds

Take-off Field Length vs. Range

Flight Profile Analysis Assumptions

A standard aircraft basic operating weight is assumed.  Each profile assumes cruise climb to altitude, cruise at ISA and descent to the destination airport.  The profiles are based on performance data from the Pilot’s Operating Handbooks.  The profiles were prepared using the following criteria:

Support PLUS+

The Support PLUS+ program is a managed maintenance service plan covering parts, or parts and labor on your new or “in-service” aircraft. Support PLUS+ provides aircraft owners with long-term maintenance cost predictability, and virtually eliminates high-cost surprises. Support PLUS+ is a transferable 60-month agreement with minimum annual flight hours, depending on the aircraft model. Support PLUS+ is available worldwide to all eligible aircraft at the same guaranteed hourly rates, regardless of location.

Aircraft owners have several coverage options:

·         Parts for scheduled and unscheduled inspections, maintenance and component removals

·         Labor for scheduled inspections, maintenance and component removals

·         Service bulletin coverage

The coverage provided under Support PLUS+Parts or Support PLUS+Parts & Labor can be customized to include engines, APU’s, avionics and other factory-installed equipment. Support PLUS+ will administer an owner’s service agreements that are provided by the manufacturers of factory-installed equipment.

Support PLUS+ Advantages

·         Eliminates risk and irregularity of maintenance costs

·         Fixed-price guarantees.  Long-term cost protection

·         Complete confidence in budgeting accuracy

·         Company assumes the cost of reliability

·         Single-source for all service and support needs

·         One convenient monthly payment

·         Program is transferable upon aircraft resale

·         Protects aircraft value

·         Available for both new and in-service aircraft *

* Program entry inspections and/or aircraft age restrictions may apply

Estimated Direct Operating Costs with Support PLUS+

                                                                                                                          Hawker 4000

Fuel

Fuel Cost @ $5.00 per U.S. Gallon.................................................................................................... 1,460.00

(Gallons per Hour) ¹..................................................................................................................................... (292)

Maintenance Cost ($):

2011 Support PLUS+ Parts & Labor over 5 years ²......................................................................... Included

Engine Restoration ($):

2011 Pratt & Whitney ( Canada ) Eagle Service Plan (ESP) Costs ³................................................. 406.80

APU (Honeywell MSP)................................................................................................................................ 40.68

Thrust Reverser Overhaul (included in SupportPlus+ Parts & Labor)................................................. Incl.

Total Direct Operating Costs per Hour ($):............................................................. $1,907.48

Average Speed (600 nm mission) ¹............................................................................................................. 419

Cost per Nautical Mile ($)........................................................................................................................... $4.55

Source:

1.        Fuel burn/speed assumes a 600 nm trip. Source: B&CA Purchase Planning Handbook (May 2011)

2.        2011 SupportPlus+ program. The first 5 years/2,500 hr (whichever is first) SupportPlus+ Parts and Labor cost is included with a new aircraft purchase.

3.        2011 Pratt & Whitney (Canada) Eagle Service Plan 'Silver' early enrollment discounted hourly rate. Rate applicable up to 3,000 hours total time.

All rates are subject to adjustment for economic escalation each year.

Hawker 4000 Weight Statement

Design Weights

Max. Ramp Weight........................................................................................... 39,700 lb.                           18,008 kg.

Max. Takeoff Weight......................................................................................... 39,500 lb.                           17,917 kg.

Max. Landing Weight....................................................................................... 33,500 lb.                           15,195 kg.

Max. Zero Fuel Weight.................................................................................... 26,000 lb.                            11,793 kg.

Fuel Capacity.................................................................................................... 14,600 lb.                              6,622 kg.

Weight Breakdown

Basic Empty Weight *....................................................................................... 22,960 lb.                           10,415 kg.

2 pilots...................................................................................................................... 400 lb.                                 181 kg.

Typical customer selected options....................................................................... 130 lb.                                   59 kg.

Operational items: manuals, water, galley provisions, etc.............................. 210 lb.                                   95 kg.

Typically Equipped Basic Operating Weight................................................ 23,700 lb.                           10,750 kg.

Max. Payload....................................................................................................... 2,300 lb.                              1,043 kg.

Max. Payload w/Full Fuel.................................................................................. 1,400 lb.                                 635 kg.

Fuel w/Max. Payload........................................................................................ 13,700 lb.                              6,214 kg.

Useful Load........................................................................................................ 16,000 lb.                              7,257 kg.

* Basic Empty Weight includes standard interior, auxiliary power unit (APU), avionics, unusable fuel and oil.

Specifications and Performance

Characteristics

Seating (Crew + Pax) .......................................................................................  2 + 8 / 10                                             

Wing Loading .............................................................................................  74.4 lb./Sq. ft.                                             

Power Loading .....................................................................................  2.86 lb./lb. thrust                                             

External Dimensions

Length.................................................................................................................. 69 ft. 6 in.                             (21.18 m)

Height.................................................................................................................. 19 ft. 9 in.                               (6.02 m)

Span..................................................................................................................... 61 ft. 9 in.                             (18.82 m)

Engines

Manufacturer......................................................................... Pratt & Whitney ( Canada )

Model.................................................................................................................... PW308A

Output .....................................................................................................  6,900/ISA+22°C

Inspection Interval (TBO)................................................................................ 6,000 hrs.

Weights

Max Ramp.......................................................................................................... 39,700 lb.                         (18,008 kg.)

Max Takeoff........................................................................................................ 39,500 lb.                         (17,917 kg.)

Max Landing...................................................................................................... 33,500 lb.                         (15,195 kg.)

Max Zero Fuel................................................................................................... 26,000 lb.                         (11,793 kg.)

Typically Equipped Basic Operating * .......................................................... 23,700 lb.                         (10,750 kg.)

* Basic Operating Weight includes standard interior, auxiliary power unit (APU), avionics, unusable fuel, oil, two crew, typical customer selected options plus allowances for manuals, water, galley provisions, etc.

Payload / Capacities

Max Payload........................................................................................................ 2,300 lb.                           (1,043 kg.)

Useful Load........................................................................................................ 16,000 lb.                           (7,257 kg.)

Max Fuel Capacity............................................................................................ 14,600 lb.                           (6,622 kg.)

(1 U.S. gal = 6.7 lb./ U.S. gal.)........................................................... 2,180 US gal.

Payload w/max fuel............................................................................................. 1,400 lb.                              (635 kg.)

Fuel w/max payload......................................................................................... 13,700 lb.                           (6,214 kg.)

Specifications and Performance (continued)

Cabin Dimensions

Length.................................................................................................................. 25 ft. 0 in.                               (7.62 m)

Height ....................................................................................................................  6 ft. 0 in.                               (1.83 m)

Width................................................................................................................... 6 ft. 5.5 in.                               (1.97 m)

Cabin Volume

Cockpit................................................................................................................. 150 cu. ft.                         (4.25 cu. m)

Passenger Cabin ..............................................................................................  762 cu. ft.                       (21.58 cu. m)

Total Volume.................................................................................................... 912 cu. ft.                      (25.83 cu. m)

Baggage Capacity (Standard Layout)

Forward Cabin Closet (fwd of entry door) ........................................  9.3 cu. ft. / 50 lb.            (0.26 cu. m./23 kg.)

Forward Cabin Closet (aft of entry door)......................................... 10.2 cu. ft. / 40 lb.            (0.29 cu. m./18 kg.)

Rear Baggage Compartment............................................................. 89 cu. ft. / 900 lb.          (2.52 cu. m./408 kg.)

Total Baggage Capacity........................................................... 108.5 cu. ft. / 990 lb.        (3.07 cu. m./449 kg.)

Pressurization

Differential............................................................................................................... 9.6 PSI

Sea Level Cabin To (ft.).................................................................................... 25,240 ft.

Specifications and Performance (continued)

Airport Performance

Takeoff Field Length

Max. TO Wt., SL, ISA........................................................................................... 5,068 ft.                             (1,545 m)

39,500 lb. TOW, 5,000 ft. elev, 25°C/77°F .....................................................  6,701 ft.                             (2,042 m)

Landing Distance

Max Landing Wt., SL, ISA ...................................................................................  2,475 ft.                                (754 m)

V_ref ..............................................................................................................................  113 kt

Climb Performance (Max Takeoff Weight)

Time to Climb / Altitude .........................................................................  14 min / FL 370                                             

FAR 25 Engine-out Rate *.................................................................................. 494 fpm                         (151 m/min)

FAR 25 Engine-out Gradient *......................................................................... 219 ft/nm                            (36 m/km)

* AFM Net Second Segment Climb, Flaps 20

Ceilings

Certified................................................................................................................ 45,000 ft.                           (13,716 m)

All Engine Service.............................................................................................. 43,100 ft.                           (13,137 m)

Engine-out Service............................................................................................ 28,400 ft.                             (8,656 m)

Cruise Performance

Mach 0.84 Cruise Speed

Speed .....................................................................................................  482 kt / 555 mph                          (893 km/hr)

Fuel Flow........................................................................................................ 2,154 lb./hr.                          (977 kg./hr)

Altitude ....................................................................................................................   FL 410

Mach 0.82 Cruise Speed

Speed .....................................................................................................  470 kt / 541 mph                          (870 km/hr)

Fuel Flow........................................................................................................ 1,852 lb./hr.                          (840 kg./hr)

Altitude .............................................................................................................   FL 430                                             

Mach 0.78 Cruise Speed

Speed...................................................................................................... 447 kt / 514 mph                          (828 km/hr)

Fuel Flow........................................................................................................ 1,653 lb./hr.                          (750 kg./hr)

Altitude ....................................................................................................................   FL 430

Specifications and Performance (continued)

Maximum Range Performance (NBAA IFR reserves) M0.78 Cruise Speed

Maximum Payload with Available Fuel (2,300 lb. payload)

Range .................................................................................................................  2,855 nm                           (5,287 km)

Average Speed....................................................................................................... 437 kt.                          (809 km/hr)

Trip Fuel............................................................................................................. 11,731 lb.                           (5,321 kg.)

Maximum Fuel with Available Payload (1,400 lb. payload)

Range .................................................................................................................  3,136 nm                           (5,808 km)

Average Speed........................................................................................................ 437 kt.                          (809 km/hr)

Trip Fuel............................................................................................................. 12,666 lb.                           (5,745 kg.)

4 passengers (800 lb. payload)

Range .................................................................................................................. 3,190 nm                           (5,908 km)

Average Speed........................................................................................................ 437 kt.                          (809 km/hr)

Trip Fuel............................................................................................................. 12,691 lb.                           (5,757 kg.)

Ferry (Zero payload)

Range .................................................................................................................  3,260 nm                           (6,038 km)

Average Speed........................................................................................................ 437 kt.                          (809 km/hr)

Trip Fuel............................................................................................................. 12,723 lb.                           (5,771 kg.)

Mission Performance (4 passengers)

300 nm mission

Flight Time...................................................................................................... 0 hr. 47 min

Trip Fuel............................................................................................................... 1,730 lb.                              (785 kg.)

Flight Level ............................................................................................................. FL 450

600 nm mission

Flight Time...................................................................................................... 1 hr. 26 min

Trip Fuel............................................................................................................... 2,803 lb.                           (1,271 kg.)

Flight Level ............................................................................................................. FL 450

1,000 nm mission

Flight Time...................................................................................................... 2 hr. 18 min

Trip Fuel............................................................................................................... 4,281 lb.                           (1,946 kg.)

Flight Level ............................................................................................................. FL 450

General Arrangement

Hawker 4000 Warranty

Warranty provided with the purchase of a new Hawker 4000 aircraft:

CAMP Systems - Factory Authorized Maintenance Tracking Program

CAMP Systems maintenance tracking system is a program that provides computerized aircraft maintenance tracking with all data being exchanged electronically.

The CAMP Systems program is a full service aviation management system that continually monitors the entire range of aircraft maintenance and inspection requirements and brings them to the attention of the operator as they become due. CAMP Systems maintenance tracking program allows you to accurately track and predict the maintenance requirements of your aircraft.  

CAMP Systems provides a dedicated analyst assigned to your aircraft to ensure that your aircraft data is as accurate and complete as possible. This is an aircraft specific program that is tailored to each specific aircraft serial number.

The first five (5) years of CAMP Systems service is provided at no charge to Buyers of a new Hawker 4000. Subsequent years of CAMP are available through an annual subscription. 

This program reflects the company’s commitment to provide all Hawker 4000 operators worldwide with the finest support services available.

Hawker Support Organizations

Support for your Hawker 4000 will be provided through a wide network of Factory Owned and Authorized Service Centers .

Each center is staffed with factory trained technicians and equipped with the tools, equipment, and parts to keep the Hawker ready for use at all times. A 24 hour AOG support will be provided as well as direct factory help on-call.

All Hawker products are fully supported by an extensive, worldwide system of service centers and field representatives strategically located throughout the world, to provide direct support liaison and on-the-spot assistance.

Wherever your travels take you, your Hawker is backed by the finest network of factory trained business jet maintenance facilities in the industry. Our authorized service centers throughout the World offer a broad range of service and support.

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