Plane + Helicopter Sales and Service
Cessna CJ2 + |
[SOLD] |
Overview
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Full Details
| Base data | |
| Type: | Jet |
| Make: | Cessna |
| Model: | CJ2 + |
| Year built: | 2006 |
| Registration No.: | D-reg |
| Attributes: | IFR certified IFR equipped Always hangared EU-OPS 1 registered |
| Location: | Germany |
| Total Time (TTAF): | 500 h |
| Price: | € 4,500,000 (~ US$ 4,805,550)[SOLD] |
| No. of passengers: | 2+6 |
| Landings: | 500 |
| Engine(s) | ||
| Number of engines: | 2 | |
| Make/Model: | Williams FJ44-3A-24 | Williams FJ44-3A-24 |
| Power: | 2400 PS | - |
| Total Time: | 400 h | 400 h |
| Description/Details of engines | |
| Aircraft enrolled on Cescom Computerized Maintenance Tracking Service Total Time L/R: 400/400 Hours Total Time Estimated at Delivery Engines Fully Paid on Williams TAP Elite Engine Program |
| Avionics | |
| Rockwell Collins ProLine 21 IFCS with 3-screen EFIS, IFIS-5000 Integrated Flight Information System, Jeppesen Electronic Approach Charts and XM Weather Autopilot: Rockwell Collins ProLine 21 FMS1: Collins FMS-3000 w/ GPS FMS2: Collins FMS-3000 w/ GPS Weather Radar: Rockwell WXR-852 Doppler Radar with Turbulence Detection Stormscope: L3 Communications WX-1000E w/ Lightning Detection Communication Radios: Dual Collins RTU-4200s w/ 8.33 kHz spacing Navigation Radios: Dual Collins NAV-4500s DME: Collins DME-4000 Radio Altimeter: Collins ALT-4000 Transponders: Dual Collins TDR-94 Mode-S Diversity Transponders w/ Enhanced Surveillance JAR OPS European Kit installed Steep Approach Kit |
| Equipment | |
| This CJ2+ is in excellent condition. With a climb of 4,120 fpm a mach speed of 0.737, a range of 1,613 nm and very efficient fuel burn you will reach your destination in a safe and timely manner. Takeoff distance at SL, ISA, MTOW is 3,360ft. Landing distance at SL, ISA, MLW is a short 2,980 ft. Along with many extras this CJ2+ is equipped with two Williams FJ44-3A-24 engines integrated with FADEC. The ceiling of 45,000 will allow you to climb above traffic, weather, turbulence and icing. The Citation CJ2+ will serve single-pilot operators and offers significant enhancements in both performance and specifications. For example, maximum payload for the CJ2+ has been increased by 300 pounds over the CJ2, enabling operation in a weight environment of ‘single pilot plus 1,800 pounds.’ Improved payloads, however, are only part of the story. The CJ2+ is made even more attractive by operational enhancements, such as the ability to direct climb to 45,000 feet in 34 minutes at maximum takeoff weight; a maximum cruise speed of 413 knots at 31,000 feet; and a four-passenger, 1,550-nautical-mile NBAA IFR range. Using less runway at maximum weight limits, the CJ2+ can take off in 3,360 feet and land in less than 3,000 feet. Propulsion for the CJ2+ is generated by twin Williams FJ44-3A-24 engines equipped with dual-channel Full Authority Digital Engine Control (FADEC). The FJ44-3A-24 shares an architecture similar to the Citation CJ3’s FJ44-3A engine, but is rated at 2,400 pounds of thrust. The avionics suite on the Citation CJ2+ is the most advanced available on this class of business jet. The integrated Collins Pro Line 21 avionics suite encompasses many of the same features as the Citation CJ3 and CJ1+. The Primary Flight Displays (PFD) and enhanced Multi-Function Display (MFD) are presented on three 8-inch by 10-inch active matrix color liquid crystal displays. The copilot’s PFD with second air data computer is standard equipment and will meet reduced vertical separation minimum (RVSM) requirements. Other integrated avionics features include a file server system with cursor control panel and enhanced map overlays, Pro Line 21 Communication, Navigation, and Surveillance (CNS) radios, and Collins FMS-3000 with performance database. The CJ2+ is equipped with standard broadcast graphical weather including Next Generation Doppler Radar (NEXRAD) information, Meteorological Terminal Aviation Routine Weather Report (METARs), and textual Terminal Aerodrome Forecast (TAF). Design Weights & Fuel Capacity (English Metric) * Maximum Ramp Weight: 12,625 Lb (5,726 Kg) * Maximum Takeoff Weight: 12,500 Lb (5,669 Kg) * Maximum Landing Weight: 11,525 Lb (5,227 Kg) * Maximum Zero Fuel Weight: 9,700 Lb (4,399 Kg) * Maximum Fuel Capacity: (6.7 Lb/Gal) 3,930 Lb (1,783 Kg) * *Typical Empty Weight: 7,725 Lb (3,504 Kg) * One Pilot plus Furnishings: 200 Lb (91 Kg) * Typical Basic Operating Weight (BOW): 7,925 Lb (3,595 Kg) * ** Useful Load: 4,700 Lb (2,132 Kg) * Payload with Full Fuel: 770 Lb (349 Kg) Specifications & Weights (English Metric) * Maximum Cruise Speed: (Mid-Cruise Weight) 418 Ktas (774 Km/Hr), at 31,000Ft (9,449 m) * Ceiling: 45,000 Ft (13,716 m) Maximum Certified * Airspeed Limits o VMO at 8,000 Ft (2,438 m) to 29,123 Ft (8,877 m) 278 KIAS (515 Km/Hr) o MMO at 29,123 Ft (8,877 m) and above M 0.737 (Indicated) * Rates of Climb all Engines 4,120 Fpm (1,256 m/min) * Single Engine 1,004 Fpm (306 m/min) * Stall Speed 86 Kcas (159 Km/Hr) MLW, Landing Configuration * Pressurization Nominal Pressure Differential 8.9 Psi (61 kP) * NBAA IFR Range (100 Nm Alternate) 1,613 Nm (2,989 Km) with Full Fuel andMaximum Takeoff Weight * Airport Performance o (Dry, Level, Hard-Surfaced Runway With Zero Wind) Takeoff Distance (SL,ISA, MTOW): 3,360 Ft (1,024 m) o Landing Distance (SL, ISA, MLW): 2,980 Ft (908 m) * Engines: o Two Williams FJ44-3A-24 o Takeoff Thrust: 2,490 Lb (11.08 kN) o Bypass Ratio: 2.2:1 * Baggage Capacity Volume: 65 Ft3 (1.84 m3) * Outside Dimensions o Wingspan: 49 Ft 10 In (15.19 m) o Overall Height: 14 Ft 0 In (4.27 m) o Overall Length: 47 Ft 8 In (14.53 m) * Cabin Dimensions (with Typical Interior Installed) o Height: 57 In (1.45 m) o Width: 58 In (1.47 m) o Length (excluding Cockpit): 163 In (4.14 m) |
| Exterior | |
| like new |
| Interior | |
| like new |
| Other remarks | |
| Aircraft will be Delivered Current on all Inspections with all Ads and Mandatory SBs Complied With asking Price is 4.9 Mio EUR + 19 % German Vat = 5.8 mio EUR |
Pictures
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