Hawker 400XPR Product Analysis

3,600 pounds of thrust per engine. The FJ44-4A-32 thrust is flat rated to 3,200 pounds at 17°C for the Hawker 400XP R to create robust temperature margin and performance. With a total thrust of 6,400 pounds, the Hawker 400XP R generates 5%, or 300 pounds, more thrust than its smaller -3AP cousin and 8% or 470 pounds more thrust than the Pratt & Whitney JT15D-5R it replaces. This significant improvement in flat rated thrust results in exceptional hot/high performance. Legacy Pratt & Whitney JT15D-5R Original introduced in 1971 Hawker 400XP - 5R variant introduced 1990 Thrust = 2,965 lb. Williams International FJ44-4A-32 Original introduced in 1992 Hawker 400XPR - 4A-32 variant introduced 2007 Thrust = 3,600 lb. capable - flat rated to 3,200 lb. 4 Hawker 400XPR data is preliminary Subject to flight test verification Hawker 400XPR Propulsion (continued) Extremely Efficient Combustion = Lower SFC and Carbon Emissions The combination of advanced internal aerodynamics and FADEC fuel management produces extremely efficient combustion that deliver a 16% reduction in specific fuel consumption (SFC) on short range missions and over a 20% SFC reduction on long range trips. This same combustion efficiency greatly reduces the aircraft’s Carbon Emissions making the Hawker 400XP R one of the most environmentally responsible neighbors on any airport. Evolutionary Design = Reliability and Low Operating Cost The FJ44-4A-32 is a proven design that delivers outstanding reliability and one of the lowest operating costs in its class based on a 5,000 hour TBO with no scheduled, intermediate off-aircraft events. Williams International FJ44-4A-32 Features Z 3,200 lb. @ ISA +17°C • Best Thrust to Weight for its class • 300 lb. > FJ44-3AP • 470 lb. > JT15D-5R Latest Technology Materials • Robust Durability • Low Weight Rugged single piece Wide-Chord Fan Highly Advanced Aerodynamics & Combustion Dual Channel FADEC • Reduced pilot workload • Integral engine synchronization • Trend monitoring • Ultra low idle 16% - 20% SFC Improvement • Lower Trip Cost 5,000 hour Time Before Overhaul • Longest TBO of its class • Lower Maintenance Cost • 1,000 hour > FJ44-3AP • 1,400 hour > JT15D-5R • No intermediate “off-aircraft” events 5 Hawker 400XPR data is preliminary Subject to flight test verification Hawker 400XPR Aerodynamics Genuine Hawker Winglets utilize composite construction which is lightweight and extremely strong. They are designed and engineered by the factory that built the legendary Beechjet/Hawker 400XP and are standard on all Hawker 400XP R aircraft. The addition of Hawker Winglets increases the aspect ratio of the wing to effectively diminish lift- induced drag. Benefits include; reduced fuel consumption, improved time-to-climb performance, faster cruise speeds and increased range. Hawker Winglets also improve low speed and high altitude handling characteristics by enhancing stabilization in flight. To ensure dispatch reliability and lower operating cost, LED position lights are incorporated into the design. The LED position lights are projected to have a Mean Time between Failure (MTBF) of 5,000 hours. Genuine Hawker Winglet Feature • Increased wing aspect ratio = Reduced lift-induced drag • Climbs higher and faster for a given power setting • Higher cruise speeds for given fuel flow - Faster block speeds • Improved low speed handling & high altitude stability • Greater thrust for the same fuel flow - Higher cruise speeds • Improved fuel efficiency • Minimal weight (25 lb./11 kg.) • Outstanding ramp appeal and aesthetics Aircraft upgraded with genuine Hawker Winglets are readily recognized for their investment in performance, range and resale value and unmistakable ramp appeal Winglet design subject to change 6 Hawker 400XPR data is preliminary Subject to flight test verification Hawker 400XPR Avionics Pioneered on the Hawker Beechcraft Premier l, Rockwell Collins Pro Line 21™ avionics are available as a Hawker 400XP R option. Featuring 8x10 in-liquid crystal, Adaptive Flight Displays (AFD), Pro Line 21™ avionics significantly improve situational awareness and reliability. The AFD combines attitude, altitude, airspeed and heading references with an easy-to-read graphical interface while the system's Multifunction Display (MFD) enables pilots to quickly reference layers of information pertinent to strategic decision making. Pro Line 21™ Features & Benefits • High-resolution Adaptive Flight Displays greatly increase flight crew situational awareness o Display TAWS, Weather Radar, TCAS, Lightning Detection and other advanced features • Seamless integration with communication, navigation and surveillance sensors • Seamless integration with Beechjet 400A / Hawker 400XP autopilot • Higher reliability reduces cost of ownership • Supports growth for future CNS/ATM requirements • Optional Integrated Flight Information System (IFIS) for electronic charts and satellite weather Hawker Beechcraft Factory Integration A production standard since 2001, Hawker Beechcraft has integrated more Pro Line 21™ avionic suites into corporate aircraft than all non-OEM avionics shops combined. This in-depth understanding of the system ensures a seamless interface with the Hawker 400XP’s legacy systems, while providing an excellent foundation for future regulatory and technology upgrades. Reduced Operating Cost Pro Line 21™ avionics installed in conjunction with a Hawker 400XP R upgrade significantly lowers your aircraft’s avionics operating cost. Pro Line 21™ new components feature a comprehensive two- year equipment warranty. When installed in conjunction with Hawker 400XP R , Rockwell Collins will extend its Collins Aviation Service Program (CASP) for all remaining Rockwell Collins installed flight deck avionics for a period of two-years. This value provides 400XP R operators with no-charge repairs and exchange services at any Rockwell Collins dealer. 7 Hawker 400XPR data is preliminary Subject to flight test verification Three (3) Display Rockwell Collins Pro-line 21 Options: • Single IFIS • XM Weather • Universal Weather • DBU 5000 • WAAS/LPV • Dual GPS • ADS-B Out • Enhanced Vision (Future Upgrade) • Synthetic Vision (Future Upgrade) • Link 2000+ (Future Upgrade) System Includes: • Three (3 each) PL-21 Adaptive Fight displays • Retains existing Standby Instrumentation • Retains existing Annunciator Panel • Integration with PL-4 IAPS System • Integration with FMS (AMS-5000) • Upgraded AHRS System (AHC-3000A) • Maintenance Diagnostic System • Electronic Engine Instrumentation on #1 MFD 8 Hawker 400XPR data is preliminary Subject to flight test verification Four (4) Display Rockwell Collins Pro-line 21 System Includes: • Four (4 each) PL-21 Adaptive Fight displays • New 3-in-One Standby Instrumentation • New Annunciator Panel • Integration with PL-4 IAPS System • Integration with FMS (AMS-5000) • Upgraded AHRS System (AHC-3000A) • Maintenance Diagnostic System • Electronic Engine Instrumentation on #1MFD Options: • Single or Dual IFIS • XM or Universal Weather • DBU 5000 • WAAS/LPV • Dual GPS • ADS-B Out • Enhanced Vision (Future Upgrade) • Synthetic Vision (Future Upgrade) • Link 2000+ (Future Upgrade) 9 Hawker 400XPR data is preliminary Subject to flight test verification Hawker 400XPR Interior / Exterior Options Hawker Beechcraft Services offers a number of interior options. Freshen-up your cabin with new leathers and fabric or completely transform your aircraft’s interior with a cabinetry re-veneer. Older Beechjet 400A aircraft owners can choose a Hawker 400XP styled window panel / arm ledge / seating upgrade. New cabinetry designs and rebuilds are also available to maximize your passengers comfort and internal baggage capacity. Your aircraft’s exterior finish protects your Hawker from the elements and makes a statement every time you land and taxi-up to the ramp. And now, Hawker 400XP R customers can choose from a number of unique XP R paint design schemes and tail art logos. Hawker Beechcraft artisans have received great praise for the flawless shine, constancy and durability of our paint application, which is backed by industry-leading warranties. Explore how Hawker Beechcraft can transform your aircraft’s exterior appearance and image. 10 Hawker 400XPR data is preliminary Subject to flight test verification Takeoff Distance Comparison With a total thrust of 6,400 pounds flat rated at ISA +17°C propelling a more aerodynamic wing with less induced drag, the Hawker 400XP R can rotate sooner and climb faster with greater payload flexibility than ever before. The Hawker 400XP R requires less takeoff field length than 400XP, especially from high elevation airports. 11 Hawker 400XPR data is preliminary Subject to flight test verification Takeoff Field Length versus Range The Hawker 400XPR delivers almost 500 nm (926 km) more range than a standard 400XP at sea level ISA conditions. At higher airport elevations, the Hawker 400XPR will require about 1,100 ft. (335 m.) less runway and fly almost 700 nm (1,296 km) farther than a standard 400XP. 12 Hawker 400XPR data is preliminary Subject to flight test verification Time-to-Climb Comparison At their respective max gross takeoff weights, the Hawker 400XP R can significantly out-climb the Hawker 400XP. In ISA conditions, the Hawker 400XP R can climb straight to FL 370 in 11 minutes, while it takes the 400XP 19 minutes to reach the same altitude. 13 Hawker 400XPR data is preliminary Subject to flight test verification Cruising Speeds, Sector Times & Fuels Improved aerodynamics and propulsion reduces Hawker 400XP R fuel consumption by 18% when compared to a standard 400XP. 300 nm (556 km) Flight Time Fuel Used 600 nm (1,111 km) Flight Time Fuel Used 1,000 nm (1,852 km) Flight Time Fuel Used Hawker 400XP 0 + 46 1,099 lb. 1 + 27 1,860 lb. 2 + 24 2,769 lb. Difference 0 minutes 202 lb. 0 minutes 345 lb. 2 minutes 484 lb. Hawker 400XP R 0 + 46 897 lb. 1 + 27 1,515 lb. 2 + 22 2,285 lb. 14 Hawker 400XPR data is preliminary Subject to flight test verification Payload versus Range Chart The Hawker 400XP R aircraft deliver greater range and/or payload performance when compared to a standard 400XP aircraft at ISA enroute conditions. 15 Hawker 400XPR data is preliminary Subject to flight test verification Range Comparison Examples With improved aerodynamics and reduced fuel consumption, the Hawker 400XPR can fly farther than ever before. Direct climb at max weight combined with lower specific fuel consumption and improved thrust at altitude generate faster trip segments and trans-continental range. The following pages show several examples of the range advantage for the Hawker 400XP R with new Williams FJ44-4A engines and composite winglets. The ranges show just a few of the world’s most popular airports including high elevation airports and ones with relatively short runways thereby demonstrating the significant improvements to the airplane. Range from Aspen, Colorado Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 16 Hawker 400XPR data is preliminary Subject to flight test verification Ranges from San Francisco and Teterboro Range from Teterboro, New Jersey Range from San Francisco, California Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 17 Hawker 400XPR data is preliminary Subject to flight test verification Ranges from Toluca and Sao Paulo Range from Toluca, Mexico Range from Sao Paulo, Brazil Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 18 Hawker 400XPR data is preliminary Subject to flight test verification Ranges from Geneva and London Range from Luton, United Kindom Range from Geneva, Switzerland Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 19 Hawker 400XPR data is preliminary Subject to flight test verification Ranges from Lanseria and Melbourne Range from Melbourne, Australia Range from Lanseria, South Africa Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 20 Hawker 400XPR data is preliminary Subject to flight test verification Ranges from Bejing and New Delhi Range from New Delhi, India Range from Beijing, China Range depiction is for information purposes only and does not incorporate common variables i.e. aircraft configuration, ATC routing, weather conditions or individual company operating procedures. It should not be used for flight planning purposes. 21 Hawker 400XPR data is preliminary Subject to flight test verification Fuel Savings Synergizing Winglets enhance aerodynamics with efficient FJ44-4A-32 engines enables Hawker 400XPR to deliver, on average, 16% reduction in specific fuel consumption (SFC) on short range missions and over a 20% SFC reduction on long range trips. Fuel Savings (600 nm trip segment) Utilization / Year = 300 hours Fuel Cost / Gallon = $5.50 Pounds / Hour Gallons / Hour Fuel Cost / Flight Hour Fuel Cost / Year 400A / XP Series (1 hour, 27 minutes) 1,860 278 gal. $1,529.00 $458,700 Delta  345 lb. 52 gal. $286.00 $85,800 Hawker 400XP R (1 hour, 27 minutes) 1,515 226 gal. $1,243.00 $372,900 A typical Hawker 400XPR is projected to save over $85,000 / year in Reduced Fuel Cost when flying an average 300 hours per year XP R is the Choice for Companies looking to:  Reduce their Operating Cost and  Reduce their Impact to the Environment 22 Hawker 400XPR data is preliminary Subject to flight test verification Estimated Direct Operating Costs Hawker 400XP R* Hawker 400A/XP Fuel $5.50 per U.S. Gallon .................................................................................. 858.00 1,050.50 (Gallons per Hour) 1 ........................................................................................ (156) (191) Maintenance Cost ($): Labor - @ $98.00 per Man-hour 2 ................................................................ 184.24 121.52 (Man-hours per Flight hour) 3 ......................................................................... (1.88) (1.24) Parts - airframe and avionics 3 ..................................................................... 122.17 98.78 Engine Restoration ($): 2012 Williams TAP “Elite” & P&W “Gold” ESP Engine Programs ................................................ 285.72 4 369.80 5 Thrust Reverser Overhaul 3 ............................................................................... NA 3.61 Total Direct Operating Costs per Hour ($):..................................... $1,450.13 $1,644.21 Average Speed (600 nm mission) 1 .................................................................. 414 414 Cost per Nautical Mile ($) .............................................................................. $3.50 $3.97 Source: 1. Fuel burn/speed assumes a 600 nm trip 2. Maintenance labor assumes a typical shop rate of $98.00 per man-hour 3. Maintenance man-hours, parts and thrust reverser from Conklin de Decker Aircraft Cost Evaluator (Spring 2012). 4. For new engines, Williams International offers a reduced rate for the first 2 years/2,000 flight hours of $142.86 per engine per hour. The standard 'Elite' rate is $285.72 per engine per hour. 5. Pratt & Whitney (Canada) Eagle Service Plan 'Gold' rate. * XPR parts costs assumes Rockwell Collins Pro-Line 4-21 Avionics upgrade All rates are subject to adjustment for economic escalation each year. 23 Hawker 400XPR data is preliminary Subject to flight test verification Hawker 400XPR Weight Statement Hawker 400XP R Design Weights Max. Ramp Weight .................................................................................. 16,500 lb. 7,484 kg. Max. Takeoff Weight ................................................................................ 16,300 lb. 7,394 kg. Max. Landing Weight ............................................................................... 15,700 lb. 7,121 kg. Max. Zero Fuel Weight ............................................................................ 13,000 lb. 5,897 kg. Fuel Capacity............................................................................................. 4,912 lb. 2,228 kg. Weight Breakdown Basic Empty Weight * .............................................................................. 10,500 lb. 4,763 kg. 2 pilots ........................................................................................................... 400 lb. 181 kg. Typically Equipped Basic Operating Weight ............................................. 10,900 lb. 4,944 kg. Max. Payload ............................................................................................. 2,100 lb. 953 kg. Max. Payload w/Full Fuel.............................................................................. 688 lb. 312 kg. Useful Load ............................................................................................... 5,600 lb. 2,540 kg. * Basic Empty Weight includes standard interior and avionics 24 Hawker 400XPR data is preliminary Subject to flight test verification Specifications and Performance Hawker 400XP R Hawker 400XP Characteristics Seating (Crew + Pax) ................................................................................ 2 + 7 / 9 2 + 7 / 9 Wing Loading (lb/sq. ft.) ................................................................................ 68.8 lb. 67.6 lb. Power Loading (lb. thrust).............................................................. 2.58 lb./lb. thrust 2.75 lb. Noise: Takeoff ............................................................................. Stage 4 Compliant 89.0 dBA External Dimensions Length....................................................................................................... 48 ft. 5 in. 48 ft. 5 in. Height ..................................................................................................... 13 ft. 11 in. 13 ft. 11 in. Span ....................................................................................................... 43 ft. 10 in. 43 ft. 6 in. Engines Manufacturer ..........................................................................Williams International P&WC Model .......................................................................................................... FJ44-4A JT15D-5R Output ........................................................................................................ 3,200 lb. 2,965 lb. ................................................................................................................. ISA+17°C ISA+12°C Inspection Interval .................................................................................... 5,000 hrs. 3,600 hrs. Weights Max Ramp ................................................................................................ 16,500 lb. 16,500 lb. Max Takeoff .............................................................................................. 16,300 lb. 16,300 lb. Max Landing ............................................................................................. 15,700 lb. 15,700 lb. Max Zero Fuel .......................................................................................... 13,000 lb. 13,000 lb. Basic Operating ........................................................................................ 10,900 lb. 10,985 lb. Payload / Capacities Max Payload ............................................................................................... 2,100 lb. 2,015 lb. Useful Load ................................................................................................ 5,600 lb. 5,515 lb. Max Fuel Capacity ...................................................................................... 4,912 lb. 4,912 lb. (1 U.S. gal = 6.7 lb/U.S. gal.) ................................................................ 733 gal. 733 gal. Payload w/max fuel ....................................................................................... 688 lb. 603 lb. Fuel w/max payload.................................................................................... 3,500 lb. 3,500 lb. 25 Hawker 400XPR data is preliminary Subject to flight test verification Specifications and Performance (continued) No difference in interior dimensions between the 400XP and 400XP R Cabin Dimensions Length...................................................................................................... 15 ft. 6 in. (4.72 m) Height ....................................................................................................... 4 ft. 9 in. (1.45 m) Width ....................................................................................................... 4 ft. 11 in. (1.50 m) Cabin Volume Cockpit....................................................................................................... 95 cu. ft. (2.69 cu. m) Passenger Cabin .................................................................................... 305 cu. ft. (8.64 cu. m) (including lav. & bag) Total Volume ............................................................................................ 400 cu. ft. (11.33 cu. m) Baggage Capacity Internal Lav / Baggage Area .................................................... 20.0 cu. ft. / 350 lb. (0.57 cu. m / 159 kg.) External Tailcone .................................................................... 26.4 cu. ft. / 450 lb. (0.75 cu. m / 204 kg.) Total ......................................................................................... 46.4 cu. ft. / 800 lb. (1.31 cu. m / 363 kg.) Pressurization Differential ................................................................................................... 9.1 PSI Sea Level Cabin To (ft.) ............................................................................ 24,000 ft. 26 Hawker 400XPR data is preliminary Subject to flight test verification Specifications and Performance (continued) Hawker 400XP R Hawker 400XP Airport Performance Takeoff Field Length Max. TO Wt., SL, ISA .................................................................................. 3,840 ft. 3,906 ft. TOW, 5,000 ft. elev, 25°C/77°F ..................................................................5,170 ft. 6,311 ft. Climb Performance (Max Takeoff Weight) Time to Climb / Altitude ................................................................... 11 min / FL 370 18 min / FL370 FAR 25 Engine-out Rate ............................................................................. 620 fpm 305 fpm FAR 25 Engine-out Gradient ..................................................................... 280 ft/nm 158 ft/nm Ceilings Certified ..................................................................................................... 45,000 ft. 45,000 ft. All Engine Service ..................................................................................... 45,000 ft. 43,450 ft. Engine-out Service .................................................................................... 31,000 ft. 20,600 ft. Cruise Performance High Speed Cruise Speed ........................................................................................... 447 kt / 514 mph 450 kt / 518 mph Fuel Flow ................................................................................................ 913 lb/hour 1,255 lb/hour Altitude ..........................................................................................................FL 450 FL 390 Long Range Cruise Speed ............................................................................................ 425 kt / 476 mph 414 kt / 476 mph Fuel Flow ................................................................................................ 761 lb/hour 938 lb/hour Altitude ..........................................................................................................FL 450 FL 430 27 Hawker 400XPR data is preliminary Subject to flight test verification Specifications and Performance (continued) Hawker 400XP R Hawker 400XP Maximum Range Performance (NBAA IFR reserves) Maximum Payload with Available Fuel ................................. (2,100 lb. payload) (2,015 lb. payload) Range ....................................................................................................... 1,170 nm 876 nm Average Speed .............................................................................................. 406 kt. 384 kt. Trip Fuel...................................................................................................... 2,508 lb. 2,420 lb. Maximum Fuel with Available Payload .................................... (688 lb. payload) (603 lb. payload) Range ....................................................................................................... 2,015 nm 1,565 nm Average Speed .............................................................................................. 415 kt. 396 kt. Trip Fuel...................................................................................................... 3,977 lb. 3,898 lb. 4 passengers (800 lb. payload) Range ....................................................................................................... 1,950 nm 1,464 nm Average Speed .............................................................................................. 415 kt. 394 kt. Trip Fuel...................................................................................................... 3,861 lb. 3,693 lb. Ferry (Zero payload) Range ....................................................................................................... 2,160 nm 1,690 nm Average Speed .............................................................................................. 413 kt. 395 kt. Trip Fuel...................................................................................................... 4,124 lb. 4,045 lb. Mission Performance (4 passengers) 300 nm mission Flight Time ............................................................................................. 0 hr. 46 min 0 hr. 46 min Trip Fuel......................................................................................................... 897 lb. 1,099 lb. Flight Level ....................................................................................................FL 370 FL370 600 nm mission Flight Time ............................................................................................. 1 hr. 27 min 1 hr. 27 min Trip Fuel...................................................................................................... 1,515 lb. 1,860 lb. Flight Level ....................................................................................................FL 410 FL410 1,000 nm mission Flight Time ............................................................................................. 2 hr. 22 min 2 hr. 24 min Trip Fuel...................................................................................................... 2,285 lb. 2,769 lb. Flight Level ....................................................................................................FL 430 FL430 28 Hawker 400XPR data is preliminary Subject to flight test verification Factory Completed Warranty The following is a summary of the Hawker 400XP R factory completed warranties: Note: Labor is covered for the specified periods provided the work is performed at a properly rated Hawker Beechcraft Authorized Service Center CAMP Systems - Factory Authorized Maintenance Tracking Program CAMP Systems is a program that reflects Hawker Beechcraft’s commitment to provide all Hawker operators worldwide with the finest support services available. CAMP Systems is a maintenance tracking system program that provides computerized aircraft maintenance tracking with all data being exchanged electronically. 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. Hawker 400XP R Williams International Engines 5 years or 2,000 hours Genuine Hawker Winglets 2 years Rockwell Collins Pro Line 21 Avionics 2 years Interior Reappointments 2 years Exterior Paint 3 years 29 Hawker 400XPR data is preliminary Subject to flight test verification Hawker Beechcraft Value Hawker Beechcraft has been successfully building and upgrading aircraft for nearly 80 years. Simply said, this is not our first aircraft or upgrade. Hawker DNA is deeply imbedded in every Hawker 400XP R upgrade. To maintain the aircraft’s legendary reputation, every Hawker 400XP R system upgrade is based on decades of Hawker core engineering and manufacturing know-how, to ensure the highest standards of quality, reliability and safety are built-in. After Delivery Support Hawker Beechcraft has been supporting the aircraft it builds and upgrades since 1932. With more than 1,000 highly-skilled and dedicated representatives strategically located around the world, Hawker Beechcraft Global Customer Support has the technical support, publications, maintenance services and parts to support 400XP R upgraded aircraft for decades to come. Operating Cost Typically, there is a trade-off between enhanced performance and operating cost. Not so with the Hawker 400XP R . In addition to greatly improved aircraft performance, the Hawker 400XP R will enjoy reduced specific fuel consumption, trip cost and engine repair maintenance cost. Resale Value Although aircraft resale values are subject to the laws of supply and demand, history has demonstrated that OEM engineered and supported performance upgrades typically realize a dollar-for-dollar return in the near term and hold their value longer than non-upgraded or non-OEM modified aircraft. 30 Hawker 400XPR data is preliminary Subject to flight test verification More Information AN EXCLUSIVE HAWKER BEECHCRAFT SERVICES PRODUCT The Hawker 400XPR upgrade is offered exclusively through Hawker Beechcraft Services, backed by the factory that built your Beechjet 400A or Hawker 400XP and supported by our commitment to quality. About Us Hawker Beechcraft Services is a functional organization of Hawker Beechcraft Global Customer Support Inc. (a wholly owned subsidiary of Hawker Beechcraft Corporation). Headquartered in Wichita Kansas, Global Customer Support (GCS) is dedicated to enhancing the ownership experience through improving the value of Hawker Beechcraft aircraft by employing products and services to simplify aircraft ownership, reduce operating cost and increase resale value. Global Customer Support is comprised of five functional organizations including:  ■ Hawker Beechcraft Services - Factory-powered service centers  ■ Hawker Beechcraft Parts & Distribution - Genuine factory parts  ■ SupportPLUS™ - Cost predictability & warranty programs  ■ Technical Support - Field support & hot-line troubleshooting experts  ■ Technical Publications - On-line and hard copy operational, service and technical information For further information on the Hawker 400XP R please contact: Hawker Beechcraft Services Randy Znamenak Mobile (316) 993-7409 Wichita, Kansas 67206 U.S.A. Email: Randy_Znamenak@hawkerbeechcraft.com Or visit: http://xpr.hawkerbeechcraft.com/ © Hawker Beechcraft Corporation 2012 The information in this report is for comparison purposes only and is based on published data from the relevant manufacturer or from independent sources. Although every attempt is made to ensure accurate data in this report, no guarantee of actual performance or cost of operation is made or implied by Hawker Beechcraft Corporation or its subsidiaries. Data is subject to change without prior notification