Basic Aircraft Products has the BAE-14/28 turbo alternator available for Cessna Aircrafts. We currently have models available to the Cessna 182, Cessna 206 and Cessna 210. For more information on the Cessna Aircrafts please use the links below.
The Cessna 182, marketed under the name Skylane, is a four-seat, single-engine, light airplane. It has the option of adding two child seats, installed in the baggage area.
Introduced in 1956, the 182 has been produced in a number of variants, including a version with retractable landing gear, and is the second most popular Cessna model, after the 172.
The Cessna 182 was introduced in 1956 as a tricycle gear variant of the 180. In 1957, the 182A variant was introduced along with the name Skylane. Later models have added more powerful engines and bigger windows.
Cessna cites the 1990s resumption in producing general aviation aircraft such as this model due to change in U.S. liability laws. In 2005, Cessna began offering the Garmin G1000 glass cockpit as an optional upgrade to the Skylane. Subsequently the glass cockpit became standard equipment.
The Cessna 182 is an all-metal (mostly aluminum alloy) aircraft, although some parts – such as engine cowling nosebowl and wingtips – are made of fiberglass or thermoplastic material. Its wing has the same planform as the smaller Cessna 172 and the larger 205/206 series; however, some wing details such as flap and aileron design are the same as the 172 and are not like the 205/206 components.
- Crew: 1
- Capacity: 3 passengers
- Length: 29 ft 0 in (8.84 m)
- Wingspan: 36 ft 0 in (11.0 m)
- Height: 9 ft 4 in (2.8 m)
- Wing area: 174 sq ft (16.2 m²)
- Airfoil: NACA 2412
- Empty weight: 1,970 lb (894 kg)
- Loaded weight: 3,110 lb (1,411 kg)
- Useful load: 1,140 lb (517 kg)
- Max takeoff weight: 3,100 lb (1406 kg)
- Powerplant: 1× Lycoming IO-540-AB1A5 3-Bladed Constant Speed, 230 hp (172 kW)
- Never exceed speed: 175 knots (201 mph, 324 km/h)
- Maximum speed: 150 knots (173 mph, 278 km/h)
- Cruise speed: 145 knots (167 mph, 269 km/h)
- Stall speed: 49 knots (56 mph, 91 km/h)
- Range: 930 nmi (1,070 mi, 1,722 km)
- Service ceiling: 18,100 ft (5,517 m)
- Rate of climb: 924 ft/min (4.7 m/s)
- Wing loading: 17.8 lb/sq ft (87 kg/m²)
- Power/mass: 0.074 hp/lb (122 W/kg)
The above content is based on the copyrighted Wikipedia article Cessna 182; it is used under the Creative Commons Attribution-ShareAlike 3.0 Unported License (CC-BY-SA). You may redistribute it, verbatim or modified, providing that you comply with the terms of the CC-BY-SA.
The Cessna 205, 206, and 207, known variously as the Super Skywagon, Skywagon, Stationair, and Super Skylane are a family of single engine, general aviation aircraft with fixed landing gear used in commercial air service and also for personal use. The family was originally developed from the popular retractable-gear Cessna 210.
The line's combination of a powerful engine, rugged construction and a large cabin has made these aircraft popular bush planes. Cessna describes the 206 as "the sport-utility vehicle of the air." These airplanes are also used for aerial photography, skydiving and other utility purposes. They can also be equipped with floats, amphibious floats and skis. Alternatively, they can be fitted with luxury appointments for use as a personal air transport.
Between the start of production in 1962 and 2006 the total Cessna 205, 206 and 207 production has been 8509 aircraft so far.
The six-seat Model 206 was introduced as a 1964 model and was built until 1986, when Cessna halted production of its single-engine product. It was then re-introduced in 1998 and remains in production in 2008.
There were many sub-variants, including the U206, P206 all certified to CAR3 standards and later 206H certified to FAR Part 23.
The total Model 206 production between 1964 and 2004 was 6581 aircraft.
- Crew: one, pilot
- Capacity: 5 passengers
- Length: 28 ft 3 in (8.62 m)
- Wingspan: 35 ft 10 in (10.92 m)
- Height: 9 ft 7 in (2.92 m)
- Wing area: 174 ft² (16.2 m²)
- Empty weight: 2,146 lb (974 kg)
- Useful load: 1,373 lb (623 kg)
- Max takeoff weight: 3,600 lb (1,633 kg)
- Powerplant: 1× Lycoming IO-540-AC1A5, 300 bhp (224 kW)
- Maximum speed: 151 kt (285 km/h)
- Cruise speed: 142 kt (263 km/h)
- Range: 721 nm (1,335 km)
- Service ceiling: 15,700 ft (4,785 m)
- Rate of climb: 988 ft/min (301 m/min)
The above content is based on the copyrighted Wikipedia article Cessna 206; it is used under the Creative Commons Attribution-ShareAlike 3.0 Unported License (CC-BY-SA). You may redistribute it, verbatim or modified, providing that you comply with the terms of the CC-BY-SA.
The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.
The early Cessna 210 (210 and 210A) had 4 seats with a Continental IO-470 engine of 260 hp (190 kW). It was essentially a Cessna 182B to which was added a retractable landing gear, swept tail, and a new wing. In 1961 the fuselage and wing were completely redesigned - the fuselage was made wider and deeper, and a third side window was added. The wing planform remained the same (constant 64" chord from centerline to 100 inches (2,500 mm) out, then straight taper to 44" chord at 208 inches from centerline), but the semi-Fowler flaps (slotted, rear-moving) were extended outboard, from Wing Station 100 to Wing Station 122, which allowed a lower landing speed (FAA certification regulations state that a single-engine aircraft must have a flaps-down, power-off stall speed no greater than 70 miles/hour). To compensate for the reduced aileron span, the aileron profile was changed and its chord enlarged. The 1964 model 210D introduced a 285 hp (213 kW) engine and 2 small child seats, set into the cavity which contained the mainwheels aft of the passengers.
In 1967 the model 210G introduced a cantilever wing replacing the strut-braced wing. Its planform changed to a constant taper from root chord to tip chord. In 1970 the 210K became the first full 6-seat model; this was achieved by replacing the flat-leaf main gear springs with tapered tubular steel springs of greater tread width (which allowed the tires to be nested farther back in the fuselage). In 1979 the 210N model eliminated the folding doors which previously covered the retracted main gears; the retracted tubular springs lie in shallow channels along the bottom of the fuselage and the wheels fit snugly into a closed depression on the fuselage bottom. Some models featured de-icing boots as an option.
The aircraft was offered in a normally aspirated version, designated the model 210, as well as the turbocharged T210 and the pressurized P210 versions.
- Crew: One, pilot
- Capacity: Five passengers
- Length: 28 ft 2 in (8.58 m)
- Wingspan: 36 ft 9 in (12.12 m)
- Height: 9 ft 8 in (2.95 m)
- Wing area: 181 ft² (16.82 m²)
- Empty weight: 2,400 lb (1,090 kg)
- Loaded weight: 4,016 lb (1,835 kg)
- Max takeoff weight: 4,000 lb (1818 kg)
- Powerplant: 1× Continental Motors TSIO-520-R, 310 bhp (231 kW)
- Maximum speed: 172 knots (T/P Versions) (198 mph, 321 km/h)
- Range: 1,000 nm (1151 mi, 1,865 km) 75% power at 24,000 ft
- Service ceiling: 27,000 ft (8,230 m)
- Rate of climb: 930 ft/min (4.7 m/s)
- Wing loading: 22.9 lb/ft² (108.1 kg/m²)
- Power/mass: 0.0775 hp/lb (W/kg)
The above content is based on the copyrighted Wikipedia article Cessna 210; it is used under the Creative Commons Attribution-ShareAlike 3.0 Unported License (CC-BY-SA). You may redistribute it, verbatim or modified, providing that you comply with the terms of the CC-BY-SA.