441 Conquest II
Summary
| Category | Military Transport Aircraft |
| Origin country | 🇺🇸 United States |
| Manufacturer | Cessna |
| First flight | 26 August 1975 |
| Year introduced | 1977 |
| Number produced | 362 units |
| Average unit price | $1.2 million |
Technical specifications
| Version: 441 | |
|---|---|
| Operational range | 4,064 km (2,525 mi) |
| Maximum speed | 547 km/h (340 mph) |
| Wing area | 23.6 m² (253.6 sqft) |
| Wingspan | 15.0 m (49.3 ft) |
| Height | 4.0 m (13.2 ft) |
| Length | 11.9 m (39.0 ft) |
| Service ceiling | 10,668 m (35,000 ft) |
| Empty weight | 2,577 kg (5,681 lbs) |
| Max. takeoff weight | 4,468 kg (9,850 lbs) |
| Climb rate | 12.37 m/s (40.6 ft/s) |
| Takeoff distance | 751 m (2,464 ft) |
| Powerplant | 2 x turboprops Garrett TPE331-8-403S delivering 474 kW each |
Current operating countries
| Country | Units | ||
|---|---|---|---|
|
Mauritania | 1 | |
All operators
Description
The Cessna 441 Conquest II development commenced in November 1974, with the first delivery in September 1977. Originally conceptualized in 1972 as the Model 435 powered by Continental GTSIO-520X engines, the design evolved by 1975 into the turboprop-powered Model 441. FAA certification was achieved on August 19, 1977. Cessna built 362 of the aircraft between 1977 and 1986. The Model 441 was renamed the Conquest II in 1983. Starting with constructor number 195 in 1984, the aircraft featured lighter-weight, four-bladed McCauley propellers. While a variant with Pratt & Whitney Canada PT6A-112 turboprops was tested in 1986, it did not enter production.
The Cessna 441 Conquest II features a pressurized cabin accommodating 8–9 passengers, and its high aspect ratio wings employ bonded construction techniques. The aircraft was initially powered by two Garrett TPE331-10-403S turboprop engines, originally equipped with three-bladed propellers, and incorporates the Cessna 1000A Integrated Flight Control System. Later models, starting in 1984 with constructor number 195, were fitted with lighter-weight, four-bladed McCauley propellers. Many in-service 441s have been upgraded to TPE331-10 engines and four-bladed propellers, which improve climb performance, service ceiling, climb rate, cruise speed, and ground clearance, while also reducing cabin noise.
The Cessna 441 Conquest II has been operated by corporate owners and air charter services, as well as by organizations such as the Royal Flying Doctor Service in Australia. The aircraft has seen global use, with exports to countries including Austria, Australia, Canada, Ecuador, Finland, Germany, Iceland, Mexico, Norway, Peru, South Africa, Sweden, and the United Kingdom. Many examples of the Cessna 441 in service today have been upgraded with TPE331-10 engines and four-bladed propellers to enhance performance.
Main Variants:
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Model 435: The original 1972 design intended to be powered by Continental GTSIO-520X engines with three-bladed propellers.
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Model 441: The evolved turboprop-powered version of the initial design.
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Conquest II: The updated designation from 1983 of the Model 441.
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1984 Model: Starting with constructor number 195, these models featured lighter-weight, four-bladed McCauley propellers.
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PT6A-112 variant: A 441 model tested with Pratt & Whitney Canada PT6A-112 turboprops in 1986 which did not enter production.