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Cessna Citation I

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Range
  
2,459 km

Top speed
  
749 km/h

Cruise speed
  
662 km/h

Wingspan
  
14 m

Weight
  
3,008 kg

Length
  
13 m

Cessna Citation I Cessna Citation family Wikipedia

Engine type
  
Pratt & Whitney Canada JT15D

The Cessna 500 Citation I, built by the Cessna Aircraft Company in Wichita, Kansas, is a small-sized business jet, the first turbofan powered. The Citation I is the basis for the early Cessna Citation family. The Citation I/SP aircraft is a single pilot variant.

Contents

Cessna Citation I Cessna Citation I SP Ocean Aviation

FanJet 500

Cessna Citation I CESSNA CITATION I Article Fri 29 Mar 2013 110013 PM UTC

In October, 1968, Cessna announced plans to build an eight-place business jet that, unlike its competition, would be suitable for operations from shorter airfields, essentially aiming to compete in the light-to-medium twin turboprop market, rather than the existing business jet market. First flight of the prototype aircraft, then called the FanJet 500, took place a little under a year later, on September 15, 1969.

500 Citation

Cessna Citation I Cessna 500 Citation I Specifications Technical Data Description

After a longer-than-expected development flight test program, during which the name Citation 500 was tried, and a number of changes to the design, the finished aircraft was debuted with the new name Citation (Model 500) and received its FAA certification in September, 1971. The aircraft was powered by two Pratt & Whitney Canada JT15D-1 turbofan engines after Cessna's experience with the T-37 Tweet twinjet trainer.

Cessna Citation I httpsuploadwikimediaorgwikipediacommonsthu

Turbofan rather than turbojets and straight wings rather than swept wings made it cruise slowly compared to other business jets and Learjet salesmen mocked it as the “Nearjet” vulnerable to “bird strikes from the rear”; Cessna renamed it the “Citation” after the thoroughbred but it was nicknamed as “Slowtation”.

500 Citation I

Cessna Citation I Cessna Citation I Wikiwand

In 1976, several product improvements were added to the aircraft in response to market pressures, including a longer span wing (47 ft 1 in vs 43 ft 11 in), higher maximum gross weight and thrust reversers, which made shorter landing fields available to customers. With these improvements came the name Citation I When production on the model 500 ended in 1985, 377 airframes had been built.

501 Citation I/SP

Like the Learjets, the Citation I required a crew of two. But since the Citation was intended to be marketed against twin turboprops, which can be flown by a single pilot, this restriction limited its intended market. Cessna's answer was the Model 501 Citation I/SP, with SP referring to its certified single-pilot capability. The aircraft was first delivered in early 1977, and a total of 312 aircraft were produced, and production also ended in 1985.

Civil operators

 Norway
  • FlyDirect
  • Military operators

     Argentina
  • Argentine Army
  •  People's Republic of China
  • People's Liberation Army Air Force
  •  Ecuador
  • Ecuadorian Navy
  •  Mexico
  • Mexican Air Force
  •  Venezuela
  • Venezuelan Air Force
  • Accidents

    New York Yankees catcher Thurman Munson was killed in his Citation I/SP on August 2, 1979 while practicing touch-and-go landings.

    Specifications (Cessna Citation I)

    Data from Jane's Civil and Military Aircraft Upgrades 1994-95

    General characteristics

  • Crew: Two (One pilot on I/SP)
  • Capacity: Five passengers
  • Length: 43 ft 6 in (13.26 m)
  • Wingspan: 47 ft 1 in (14.35 m)
  • Height: 14 ft 3 in (4.37 m)
  • Wing area: 278.5 ft² (25.9 m²)
  • Empty weight: 6,631 lb (3,008 kg)
  • Max. takeoff weight: 11,850 lb (5,375 kg)
  • Powerplant: 2 × Pratt & Whitney Canada JT15D-1B turbofan, 2,200 lbf (9.77 kN) each
  • Performance

  • Maximum speed: Mach 0.705 (465.3 mph) (above 28,000 ft (8,530 m))
  • Cruise speed: 357 knots (411 mph, 662 km/h) at 35,000 ft (10,670 m)
  • Stall speed: 82 knots (95 mph, 152 km/h)
  • Range: 1,328 NM (1,528 mi, 2,459 km) (45 min reserves, max fuel, 1,562 lb payload)
  • Service ceiling: 41,000 ft (12,495 m)
  • Rate of climb: 2,719 ft/min (13.8 m/s)
  • Wing loading: 42.5 lb/ft² (208 kg/m²)
  • Thrust/weight: 0.37
  • References

    Cessna Citation I Wikipedia