Cessna 526 CitationJet
American prototype jet training aircraft
From Wikipedia, the free encyclopedia
The Cessna 526 CitationJet is a twinjet trainer built by Cessna as a candidate for the United States Joint Primary Aircraft Training System. It was a twin-engined, tandem seat aircraft, based on the Cessna CitationJet executive aircraft. However, it was unsuccessful, with only two prototypes built.[1]
| 526 CitationJet | |
|---|---|
Both 526 prototypes in flight | |
| General information | |
| Type | Primary jet trainer |
National origin | United States |
| Manufacturer | Cessna |
| Status | Canceled |
| Number built | 2 |
| History | |
| First flight | 20 December 1993 |
Developed from | Cessna CitationJet |
Design and development
The United States military issued a request for proposal for a trainer to be used by the United States Air Force and United States Navy.[1] Cessna responded with the 526, based on its 525 CitationJet civilian business jet. The 526 and 525 shared 75% commonality including the wings, engines and landing gear. The electrical- hydraulic- and fuel systems were also common to the two types. The 526 had a redesigned fuselage featuring a tandem two-seat cockpit with zero-zero ejection seats; and a new empennage with a low-mounted tailplane instead of the 525's T-tail.[1]
The prototype first flew on 20 December 1993 and was followed by a second prototype with its first flight on 2 March 1994.[1]
The CitationJet did not succeed in the competition, which was won by the turboprop Beechcraft T-6 Texan II, a variant of the Pilatus PC-9.
Specifications
General characteristics
- Crew: 2
- Length: 40 ft 8 in (12.40 m)
- Wingspan: 37 ft 0 in (11.28 m)
- Height: 12 ft 6 in (3.81 m)
- Wing area: 218 sq ft (20.6 m2) est.
- Empty weight: 6,450 lb (2,925 kg)
- Gross weight: 8,500 lb (3,855 kg)
- Powerplant: 2 × Williams-Rolls F129 turbofan, 1,500 lbf (6.7 kN) thrust each
Performance
- Maximum speed: 311 mph (500 km/h, 270 kn)
- Maximum speed: Mach 0.70
- Range: 1,209 mi (1,944 km, 1,051 nmi)
- Service ceiling: 35,000 ft (10,668 m) certified
See also
Aircraft of comparable role, configuration, and era