2002 Citation X Serial Registration N750DD. Specifications

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1 Specifications 2002 Citation X Serial Registration N750DD

2 2002 Cessna Citation X Serial Registration N750DD TOTAL TIME AIRFRAME & ENGINES: 2,847 Hours Since New LANDINGS: 1,892 ENGINES: Rolls-Royce Allison AE 300 7A equipped with FADEC (Enrolled on Rolls-Royce Corporate Care engine program) APU: 2,692 Hours Since New / 2,939 Events Honeywell GTCP AVIONICS DESCRIPTION: The ultimate flight deck for Pilots. The Citation X has always been more racehorse than showhorse. And the X s intuitive flight deck proves that the world s fastest business jet is a true pilot s airplane. The ergonomic seats were designed for comfort on transcontinental missions. Essential flight controls and flight information are all within easy reach. Systems are at once technologically advanced and simple to operate, built around a proven, integrated avionics suite designed to improve situational awareness and reduce pilot workload in flight. Citation X Primus 2000 The Model 750 is equipped with the PRIMUS 2000 Integrated Avionics System. It is an automatic flight guidance, a flight management, and an electronic display system with Five cathode ray tube (CRT) display units. These three functions are operated using an Interconnected system of cockpit controls and displays, sensors, and integrated computers. The heart of the Citation X avionics system is the PRIMUS 2000 Integrated Avionics System (IAS) which combines three subsystems into two identical interchangeable IC-800 integrated avionics computers (IACs). The subsystems are comprised of the Five-Tube Electronic Display System (EDS), the Flight Guidance System (FGS), and the Flight Management System (FMS). Five more subsystems are part of the PRIMUS 2000 system, and provide data to the major system. They are: the dual ADZ-840 Air Data System, the PRIMUS II integrated radio system, the PRIMUS 880 Weather Radar System, and the AA-300 Radio Altimeter System.

3 Long distance communication capability provided by a Bendix/King KHF-950 High Frequency (HF) transceiver and Air Cell Satellite Phone. The dual Flight Management Systems (FMSs) have GPS (Global Positioning Satellite) function. Honeywell TCAS II (Traffic Collision Advisory System), Honeywell EGPWS MKV (Enhanced Ground Proximity Warning System), Global Airborne Flight Information System (AFIS), with SATCOM capability, and a Cockpit Voice Recorder (CVR) are also installed as standard equipment. Optional systems such as a second High Frequency transceiver, an Emergency Locator Bacon, a second digital ADF, a Flight Data Recorder (FDR), are installed on the aircraft.

4 STANDARD AVIONICS INCLUDE:» Dual Honeywell Primus 2000 FMS with GPS Capability NZ 6.0» Dual Primus II Integrated Communication and Navigation Radios» Dual Honeywell Global Position Inertial Reference Systems (IRS) LASEREF IV» Dual Honeywell AZ-840 Air Data Computers» Honeywell Primus 880 Turbulence Weather Radar» Honeywell TCAS II TPU-67A» Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS)» L3/Loral FA2100 Solid State Cockpit Voice Recorder (CVR)» Dual Angle of Attack Sensors» Color Weather Radar with Turbulence Detection» Traffic Collision Avoidance System (TCAS II)» Enhanced Ground Proximity Warning System (EGPW) ADDITIONAL / OPTIONAL EQUIMENT:» L3 SSFDR Flight Data Recorder» Dual Mode S Diversity Transponders Enhanced» Data Management Unit (DMU) LH FWD Closet» FMS Performance Database» Dual Honeywell KHF950 w/kfs-594 Ctl» CSD-714 SELCAL» Microwave Oven RH Forward Cabinet» Walk-Around Oxygen Bottle in Aft Bulkhead Closet» Air Cell Iridum ST-3100 Satcom Telephone» Airshow 400 Genesis w/10.4 Monitor» Side ledge Monitor Provisions» 110V AC Universal Outlet (1)

5 INTERIOR: Stepping into a Citation X cabin can be a breathtaking experience for even the most seasoned business jet traveler. And with good reason. The aircraft is configured for eight passengers with double-club seating, the cabin can easily be mistaken for that of a larger aircraft. That sense of spaciousness is due in part to the Citation X s dropped-wing design and extensive wing fairing, which allows components to be installed outside the pressure vessel. This translates into a continuous dropped aisle as well as more space in the cabin that Cessna s interior design team can devote to passenger comfort and amenities. The Citation X s large, impressive galley provides necessary refreshment en route.

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11 Cabin Features The cabin management system features touch-screen control of environmental and entertainment components, such as dual DVD video, an improved sound system, and.mp3 player input capability. Dual-zone temperature control lets pilots and passengers alike enjoy custom comfort settings. Stand up. Move around. Make yourself comfortable. At 593 cubic feet, the Citation X s interior is significantly larger than the cabins of other jets in its class. It also out performs all of them in baggage capacity with a total of 20 cubic feet of stowage space, including a 82 cubicfoot externally loaded tail compartment and Ski Tube. An aft lavatory has sliding privacy doors and can be used as a dressing area.

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13 The Citation X s aft lavatory with solid door and large closet provides both privacy and ample additional storage.

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16 Cessna Citation X Floor Plan

17 CITATION X PERFORMANCE & SPECIFICATIONS Maximum Cruise Speed Without winglets With optional winglets installed (35,000 ft /10,668 m, mid cruise weight) 525 ktas 972 km/hr 526 ktas 974 km/hr NBAA IFR Range (NBAA 200 nm alternate, full fuel, MTOW) Without winglets 3,070 nm 5,686 km With optional winglets installed 3,220 nm 5,963 km Airport Performance (dry, level, hard-surface runway, zero wind) Takeoff distance (SL, ISA, MTOW) 5,140 ft 1,567 m Landing distance (SL, ISA, Typical Landing Weight) 2,740 ft 835 m Ceiling Maximum certified 51,000 ft 15,545 m Single engine 26,000 ft 7,925 m Rates of Climb All engines 3,650 ft/min 1,113 m/min Single engine 1,120 ft/min 341 m/min Airspeed Limits VMO from 8,000 ft (2,438 m) to 30,650 ft (9,342 m) 350 kias 648 km/hr MMO above 30,650 ft (9,342 m) M 0.92 (indicated) Stall Speed MLW, landing configuration 101 kcas 187 km/hr Pressurization Nominal pressure differential 9.3 psi.64 bar Outside Dimensions Overall length 72 ft 4 in m Overall height 19 ft 3 in 69 ft 2 in Wingspan, without winglets 19 ft 3 in 5.87 m Wingspan, with optional winglets installed 69 ft 2 in m

18 Cabin Dimensions (with typical interior installed) Length (excluding cockpit) 287 in 7.29 m Height 68 in 1.73 m Width 66 in 1.68 m Engines Two Rolls-Royce AE3007C1 FADEC -equipped Takeoff thrust 6,764 lb kn Bypass ratio 5:1 Design Weights and Capacities Maximum ramp weight 36,400 lb 16,511 kg Maximum takeoff weight 36,100 lb 16,375 kg Maximum landing weight 31,800 lb 14,424 kg Maximum zero fuel weight 24,400 lb 11,068 kg Maximum fuel capacity (6.7 lb/gal) 12,931 lb 5,865 kg Typical empty weight* 21,700 lb 9,843 kg Two pilots plus stores 400 lb 181 kg Typical basic operating weight (BOW) 22,100 lb 10,024 kg Useful load** 14,300 lb 6,486 kg Payload with full fuel1 369 lb 621 kg * Reflects standard aircraft with typical options, typical interior, and unusable fuel and oil. **Amount of payload and fuel that can be carried, over and above crew (based on ramp weight).

19 EXTERIOR: Overall Matterhorn White with Navy Metallic and Medium Blue Metallic and Gold Accent Striping. MAINTENANCE & INSPECTION: Enrolled in Rolls-Royce Corporate Care engine program Enrolled on Cessna Citation ProParts Cessna Citation Factory Maintained Enrolled in CESCOM Specifications subject to verification upon inspection. Aircraft subject to prior sale.