2002 Citation X - East Coast Jet Center€¦ · 17/6/2014 · The Citation X has always been more...

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2002 Citation X Serial 750-0185

Registration N750DD

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2002 Cessna Citation X Serial 750-0185

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 36-150

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.




2002 Citation X, 750-0185 Specifications (Cont’d)

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.





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)





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.





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 cubic-

foot externally loaded tail compartment and Ski Tube. An aft lavatory has sliding privacy doors

and can be used as a dressing area.





The Citation X’s aft lavatory with solid door and large closet provides both privacy and ample

additional storage.




SKI TUBE





Cessna Citation X Floor Plan





CITATION X PERFORMANCE & SPECIFICATIONS

Maximum Cruise Speed (35,000 ft /10,668 m, mid cruise weight)

Without winglets 525 ktas 972 km/hr

With optional winglets installed 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 22.04 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 21.09 m





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 30.09 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).




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.

2002 Citation X - East Coast Jet Center€¦ · 17/6/2014 · The Citation X has always been more...

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