CITATION CJ1 (CE-525) ASKING PRICE: US$ 1,095,000

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1 CITATION CJ1 (CE-525) ASKING PRICE: US$ 1,095,000 YOM 2003 MSN The CJ1 is the second generation of the extremely successful Citation Jet series. It comes with all of the advantages that the original Citation Jet offered, but with improvements in economy and performance. Its status as the second generation Citation gives the advantage of using a private jet design that has been tested and modified to exceed the success of the first model the Citation Jet. The design goals of the Citation Jet can be summed up in three words: simplicity, economy, and performance. Previous Citations had used a straight wing, which slows the aircraft considerably but dramatically reduces production and design costs. The Citation Jet upgraded to a natural laminar flow wing, which took four years to design in a joint venture between Cessna and NASA. This wing delays the onset of airflow separation longer, improving the lift-to-drag characteristics ten to fifteen percent when compared to earlier straight-wing designs. The CJ1 is extremely fuel-efficient, burning an average of 134 gallons per hour. The economy of its fuel burn can be largely attributed to Cessna s choice of engines. It uses two Williams FJ44-1A turbofans, each of which delivers 1,900 pounds of thrust on takeoff. Another of the CJ1 s strong points contributes to its low operating cost as well: the simplicity (but reliability) of its flight systems; it uses the Pro Line 21 avionics package. Despite the CJ1 s economy in flight, it allows for a surprisingly high payload. Its three baggage compartments can carry up to a total of 832 pounds of luggage. The CJ1 was specifically designed to be able to operate on short runways. At sea level the CJ1 can take off in 3,080 feet; on runways at an altitude of 5,000 feet, its takeoff distance increases to a mere 5,710 feet. ISSUE PAGE 1-5

2 The CJ1 has a payload capacity of 1,400 pounds; its maximum takeoff weight (MTOW) of 10,600 pounds is 100 pounds heavier than the MTOW of its predecessor the Citation Jet. The maximum fuel weight also increased 300 pounds to a total of 3,220 pounds. These alterations resulted in better range/payload flexibility, offering owners more options in flight planning. The most surprising result of the significant increase in payload is that the CJ1 is actually faster than the Citation Jet. Most owners, knowing the economical features of the CJ1, are surprised at how comfortable it is. Seats are available for five passengers, and the full-length dropped aisle gives the cabin a roomier feel. The double-sealed door uses a fastening system similar to that of a vault, which reduces cabin noise The CJ1 is ideal for small companies and individuals looking for an economical private jet for short-range missions, usually a little over one hour. (Source: Jet Advisors LLC, Bedford, MA, USA) GENERAL CHARACTERISTICS Capacity: passengers Payload: lb (279 kg) Length: ft 7 in (12.98 m) Wingspan: ft 11 in (14.30 m) Height: ft 7 in (4.19 m) Empty weight: ,765 lb (3,069 kg) Maximum payload: ,835 lb (1,740 kg) Maximum take-off weight: ,700 lb (4,853 kg) Powerplant: Williams FJ44-1AP turbofan, 1,965 lb (8.74 kn) each GENERAL PERFORMANCE Cruise speed: kts (720 km/h) Stall speed: kts (153 km/h) Range: ,300 nm (2,408 km) Service ceiling: ,000 ft (12,497 m) Rate of climb: ,290 ft/min (1,003 m/min) ISSUE PAGE 2-5

3 AIRFRAME Total time (h): ENGINES 2 x Williams FJ44-1A MSN 2054 Total time (h): MSN 2053 Total time (h): INTERIOR Light beige cabin interior with dark wood paneling; Spacious club configuration with dual executive writing tables; 6 leather passenger club seat configuration in tan leather, brown carpets; Aft belted lavatory; Latest cabin refit works in September 2014 Cockpit: sheepskin crew seat slipcovers, crew nav-chart cases, Eros crew oxygen masks ISSUE PAGE 3-5

4 AVIONICS Honeywell VHF S/E KY-196B ADC/ALT Unit AM-250 DME KN-63 ADF KR-87 VHF/UHF NAV KN-53 XPDR KT-71 2 x GPS KLN-900 Marker KMR-675 Artec ELT COSPAS-SARSAT C406-2 Kollsman STAND-BY ASI/ALT, WL102AMS6 Garmin Collins XPDR, GTX-330D EFIS/EICAS, 3-tube, Proline-21 AHRU, AHC3000 AP/FD/YD, FGC-3000 WX Radar, RTA-800 ADC-3000 Radio Altimeter, ALT-55B MISCELLANEOUS Enrolled under CAMP (Cescom) EASA Part-CAT compliant First owner - operator, Luxaviation Germany GmbH Currently registered D-IFDH (Germany), Hangared in Paderborn (EDLP) Germany No damage history, no outstanding corrosion ISSUE PAGE 4-5

5 CONTACT Bart BOURY DISCLAIMER This offering is subject, but not limited to, errors, omissions, price fluctuation, and prior sale or withdrawal without notice. All details disclosed are without guarantee and solely based on the information received by Engel & Völkers Aviation. Engel & Völkers Aviation cannot be held liable for any lack of completeness, inaccuracy, or ambiguities and/or errors contained in the information disclosed. It is the buyer s responsibility to disclose the details of any concern(s) to the seller, by the request of an independent survey, pre-purchase inspection and/or enquiry. The buyer must ensure that the purchase contract properly reflects his concern(s) and that it sets out any representations and/or details on upon which he may rely. We are at your disposal for any further information about the aircraft. Upon receipt of notice, the aircraft is available for viewing at timing to be agreed upon, accompanied by an Engel & Völkers Aviation representative. Aircraft offered under exclusive mandate by owner to EDISON S.A. (Luxembourg) in partnership with BOUTSEN S.A. (Monaco), subject to prior sale, lease, or withdrawal from the market without notice. ISSUE PAGE 5-5