|A Cessna 525 CitationJet|
|National origin||United States|
|First flight||29 April 1991|
|Status||Active, In production|
|Developed into||Cessna 526 CitationJet|
The Cessna CitationJet/M2/CJ series (Model 525) are American turbofan-powered light corporate jets built by the Cessna Aircraft Company in Wichita, Kansas. The Citation brand of business jets encompasses seven distinct "families" of aircraft. The Model 525 CitationJet was the basis for one of these families, which encompasses the CJ, CJ1, CJ1+, M2, CJ2, CJ2+, CJ3, CJ3+, CJ4 and CJ4+ models.
The original Model 525 CitationJet was developed as a replacement for the Citation and Citation I, being launched in 1989. Basically an all new aircraft, the CitationJet used a modified version of the Citation's forward fuselage, but with a new supercritical laminar flow wing, and a new T-tail configured tailplane. It is powered by two Williams FJ44 turbofans, and features EFIS avionics and single pilot certification. The CitationJet's fuselage is 11 inches (27 cm) shorter than the Citation I's, but has a lowered center aisle for increased cabin height. The CitationJet's first flight was on April 29, 1991, with its first delivery on March 30, 1993.
The Cessna Citation CJ1 (also Model 525) was developed as an improved version of the original CitationJet. The CJ1 improved on the CitationJet by adding a more-modern EFIS avionics suite and a moderate increase in maximum takeoff weight. The CJ1 has been replaced by the CJ1+, which shares the same airframe but has an additional updated avionics package, and FADEC to allow the engines to be controlled by computer rather than mechanical controls. The GE Honda HF120 engine is offered as a retrofit to the CJ1.
The Cessna Citation M2 was launched in September 2011 as a new light business jet. The M2 is based on the then out-of-production CJ1 variant and features a new cabin layout and a more efficient version of the Williams FJ44 engine. The M2 first flew on 9 March 2012. An M2 may cost around US$2-3 per nautical mile to operate, whereas the G650 and similar may cost $5-6.
The Cessna Citation CJ2 (Model 525A) is a 5-foot stretch extension of the Cessna Citation CJ1 (Model 525) first delivered in the year 2000. The 525A comes in two forms, the original CJ2 and the newer CJ2+, which has updated avionics, increased performance, and FADEC controls. The CJ2+ was first delivered in April 2006 and was out of production due to low demand in January 2016.
The Cessna Citation CJ3 (Model 525B) is part of the Citation business jet family. It is a stretch extension of the CJ2, which, in turn, was a stretch of the CJ1. The aircraft was unveiled in September 2002 at the National Business Aviation Association (NBAA) convention. It took its first and second flight on the same day on April 17, 2003. It was FAA certified in October 2004 and delivery of the CJ3 began in December of that year.
The CJ3's cabin comes standard with six club seats in a center-style configuration, although it is customizable to the owner's specifications. The cockpit was originally designed for a single-pilot operation, but it can accommodate up to two crew members. Its flight deck is composed of a Rockwell Collins state-of-the-art avionics system. It has external baggage access for added convenience. There is also a cabin baggage compartment that is accessible in flight. It also features a trailing-link tricycle landing gear.
The Cessna Citation CJ4 (Model 525C) is part of the Citation business jet family. It is a stretch extension of the CJ3, adding another two feet to the CJ3 cabin. The CJ4 also introduces a different wing design than the earlier models. It borrows the moderately swept wing from the Citation Sovereign. The CJ4 was introduced in 2006. The first CJ4 business jet lifted off from McConnell AFB at Wichita, Kansas, on Monday, May 5, 2008, with the first deliveries starting up in 2010.
We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Model 525C airplanes. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires replacing certain lithium-ion batteries installed as the main aircraft battery with either a Ni-Cad or a lead acid battery. This AD was prompted by a report of a battery fire that resulted after an energized ground power unit was connected to one of the affected airplanes equipped with a lithium-ion battery as the main aircraft battery. We are issuing this AD to correct the unsafe condition on these products.
The CitationJet is a low-wing cantilever monoplane with retractable tricycle landing gear, a pressurized cabin, a T-tail, and is powered by two Williams FJ44 turbofan engines that are pylon mounted on the rear fuselage.
- Model 525 serial numbers 0001 to 0359 are marketed as the CitationJet and are powered by two Williams International FJ-44-1A turbofans.
- CitationJet CJ1
- Model 525 serial numbers 0360 to 0599 are marketed as the CitationJet CJ1 and are powered by two Williams International FJ-44-1A turbofans
- CitationJet CJ1+
- Model 525 serial number 0600 and higher are marketed as CitationJet CJ1+ and are powered by two Williams International FJ-44-1AP turbofans
- Citation M2
- Model 525 marketed as Cessna Citation M2, powered by two Williams International FJ44-1AP-21 turbofans
- CitationJet CJ2
- Model 525A serial numbers 0001 to 0299 are marketed as the CitationJet CJ2 and are powered by two Williams International FJ44-2C turbofans
- CitationJet CJ2+
- Model 525A serial numbers 0300 and higher are marketed as the CitationJet CJ2+ and are powered by two Williams International FJ44-3A-24 turbofans. Production ended in January 2016 due to low demand.
- CitationJet CJ3
- Model 525B are marketed as the CitationJet CJ3 and are powered by two Williams International FJ-44-3A turbofans.
- CitationJet CJ3+
- Configured with Garmin G3000 avionics. FAA certified in 2014.
- Cessna Citation CJ4 (Model 525C) The largest Cessna Citation Jet (CJ) that is certified for single pilot operation. Can seat up to ten passengers. Utilizes the Williams International FJ44-4A turbofan engine and has a maximum range of 2,190 nautical miles (4,055 kilometers).
|Crew||Single Pilot Certified|
|Length||42 ft 7 in (12.98 m)||47 ft 8 in (14.53 m)||51 ft 2 in (15.59 m)||53 ft 4 in (16.26 m)|
|Height||13 ft 11 in (4.24 m)||14 ft (4.27 m)||15 ft 2 in (4.62 m)||15 ft 5 in (4.69 m)|
|Wingspan||47 ft 3 in (14.40 m)||49 ft 10 in (15.19 m)||53 ft 4 in (16.26 m)||50 ft 10 in (15.49 m)|
|Wing Area||240 sq ft (22.3 sq m)||264 sq ft (25 sq m)||294 sq ft (27.32 sq m)||330 sq ft (30.66 sq m)|
|Wing Sweep||0 degrees||12.5 degrees|
|Cabin height||57 in (1.45 m)|
|Cabin width||58 in (1.47 m)|
|Cabin length||11 ft (3.35 m)||13 ft 7 in (4.14 m)||15 ft 8 in (4.78 m)||17 ft 4 in (5.28 m)|
|Maximum Takeoff Weight||10,700 lb (4,853 kg)||12,500 lb (5,670 kg)||13,870 lb (6,291 kg)||17,110 lb (7,761 kg)|
|Maximum Landing Weight||9,900 lb (4,491 kg)||11,525 lb (5,228 kg)||12,750 lb (5,783 kg)||15,660 lb (7,103 kg)|
|Maximum Zero Fuel Weight||8,400 lb (3,810 kg)||9,700 lb (4,400 kg)||10,510 lb (4,767 kg)||12,500 lb (5,670 kg)|
|Usable Fuel Weight||3,296 lb (1,495 kg)||3,930 lb (1,783 kg)||4,710 lb (2,136 kg)||5,828 lb (2,644 kg)|
|Usable Fuel Volume||492 gal (1,862 l)||587 gal (2,221 l)||703 gal (2,661 l)||870 gal (3,293 l)|
|Basic Operating Weight||6,990 lb (3,171 kg)||8,030 lb (3,642 kg)||8,540 lb (3,874 kg)||10,280 lb (4,663 kg)|
|Useful Load||3,810 lb (1,728 kg)||4,595 lb (2,084 kg)||5,530 lb (2,508 kg)||6,950 lb (3,152 kg)|
|Maximum Payload||1,410 lb (640 kg)||1,670 lb (757 kg)||1,970 lb (894 kg)||2,220 lb (1,007 kg)|
|Full Fuel Payload||514 lb (233 kg)||665 lb (302 kg)||820 lb (372 kg)||1,122 lb (509 kg)|
|Turbofan × 2||Williams FJ44-1AP-21||Williams FJ44-3A-24||Williams FJ44-3A||Williams FJ44-4A|
|Thrust (each)||1,965 lb (8.74 kN)||2,490 lb (11.08 kN)||2,820 lb (12.54 kN)||3,621 lb (16.11 kN)|
|Maximum Cruise||404 ktas (748 km/h)||418 ktas (774 km/h)||416 ktas (770 km/h)||451 ktas (835 km/h)|
|Maximum Range||1,550 nm (2,871 km)||1,781 nm (3,298 km)||2,040 nm (3,778 km)||2,165 nm (4,010 km)|
|Takeoff Field Length||3,210 ft (978 m)||3,360 ft (1,024 m)||3,180 ft (969 m)||3,410 ft (1,039 m)|
|Landing Distance||2,590 ft (789 m)||2,980 ft (908 m)||2,770 ft (844 m)||2,940 ft (896 m)|
|Maximum Operating Altitude||41,000 ft (12,497 m)||45,000 ft (13,716 m)|
|Maximum Climb Rate||3,698 fpm (1,127 mpm)||4,120 fpm (1,256 mpm)||4,478 fpm (1,365 mpm)||3,854 fpm (1,175 mpm)|
- Related development
- Aircraft of comparable role, configuration and era
- "Textron Aviation's expansive lineup at EAA AirVenture 2016 to include debut of new SETP cabin mockup" (Press release). Textron Aviation. July 18, 2016.
- "Business Jets Specification and Performance Data" (PDF). Business & Commercial Aviation. Aviation Week. May 2015.
- "Operations Planning Guide" (PDF). Business & Commercial Aviation. Aviation Week. August 2012.
- Frawley, Gerard (2003). The International Directory of Civil Aircraft, 2003-2004. Fyshwick, ACT, Australia: Aerospace Publications Pty Ltd. p. 44. ISBN 1-875671-58-7.
- Cessna Citation CJ1+ official web site
- Chad Trautvetter (18 September 2014). "Sierra Selects GE Honda HF120 for Sapphire CitationJet Upgrade Program; Aviation International News". Ainonline.com. Retrieved 25 September 2014.
- Cessna Launches New Light Business Jet: Citation M2
- Cessna M2 makes its maiden flight
- The initial M2 prototype, which first flew on 9 March, is not considered a conforming airframe; it aircraft will serve as a conforming platform for testing of the Garmin G3000 avionics and Williams FJ44-1AP-21 turbofan engines, which will be its primary role in the certification program. The certification program will involve only one other aircraft, which is expected to join the program in May. The second aircraft (which will be considered completely conforming to the certificated design) will be used for aerodynamics testing. Launches M2 Flight Test Program&channel=busav Aviation Week & Space Technology website, accessed 22 March 2012
- Cessna Launches Aggressive Nine-Month M2 Flight Test Program
- Table Mission Costs for Turboprops Greater Than 12,500 lb., Jets Less Than 20,000 lb.
- "Cessna Ceases Production Of CJ2+ Jet". AVweb. Retrieved 8 January 2016.
- Cessna Aircraft Company CJ4 Official web page
- "Federal Register, Volume 76 Issue 211 (Tuesday, November 1, 2011)". gpo.gov. Retrieved 8 January 2016.
- Cyrus Sigari (September 2014). "A plus for the CJ3". AOPA Pilot: T-10.
- Van Wagenen, Juliet. "Cessna’s CJ3+ Receives FAA Certification" Aviation Today, 5 September 2014. Accessed: 8 September 2014.
- "Citation M2 Specifications". Cessna.
- "Citation CJ2+ Specifications". Cessna.
- "Citation CJ3+ Specifications". Cessna.
- "Citation CJ4+ Specifications". Cessna.
|Wikimedia Commons has media related to Cessna CitationJet.|
|Wikimedia Commons has media related to Cessna Citation M2.|
- Cessna Citation home page
- Cessna Citation M2 home page
- European Aviation Safety Agency - Type-Certificate Data Sheet - Cessna Aircraft Company - 525 (Citation Jet)
- Federal Aviation Administration Type Certificate Data Sheet No A1W1 - Cessna 525, 525A, 525B
- Gallery of photos
- Pilot Report, by AviationWeek
- Pilot Report, by Aviation International News
- "Citation M2: New Entry-Level Jet from Cessna". Flying Magazine. 27 September 2013. Retrieved 10 March 2014.