Samiksha Jaiswal (Editor)

Cessna 188

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Top speed
  
195 km/h

Length
  
8 m

Unit cost
  
15,995–15,995 USD (1966)

Manufacturer
  
Cessna

Wingspan
  
13 m

Introduced
  
1966

First flight
  
February 19, 1965

Cessna 188 Cessna 188 AGseries Photos AirplanePicturesnet

Cessna 188 turbine ag husky


The Cessna 188 is a family of light agricultural aircraft produced between 1966 and 1983 by the Cessna Aircraft Company.

Contents

Cessna 188 Cessna 188 AgWagon Specifications Technical Data Description

The various versions of the 188 — the AGwagon, AGpickup, AGtruck and AGhusky, along with the AGcarryall variant of the 185, constituted Cessna's line of agricultural aircraft.

Cessna 188 CESSNA188 VINH QUANG RC MODELS

Crop dusting close up cessna 188


Development

Cessna 188 Cessna 188 Agwagon Untitled Aviation Photo 1419349 Airlinersnet

In the early 1960s Cessna decided to expand their already wide line of light aircraft by entering the agricultural aircraft market. They surveyed pilots and operators of other brands of agricultural aircraft to see what features and capabilities these operators were looking for. The resulting aircraft was a conventional single-seat, piston-engined, strut-braced low-wing agricultural airplane.

Cessna 188 httpsuploadwikimediaorgwikipediacommonsthu

The Cessna 188 borrowed heavily from the Cessna 180, the initial version using the same tail cone and fin structure as well as the same Continental O-470-R 230 hp (170 kW) powerplant. The 188’s airframe is predominantly built from 2024-T3 aluminum, with the chemical hopper constructed from fibreglass. The fuselage is of semi-monocoque construction and is pressurized on later models (using the dynamic pressure resulting from the aircraft's forward speed) to reduce induction of chemicals into the airframe.

Cessna 188 Cessna 188 Wikipedia

The Cessna 188 was first flown on 19 February 1965. The aircraft was certified and entered production in February 1966, with 241 aircraft delivered the first year.

Cessna 188 Cessna 188 Agwagon series pictures technical data history

The initial design of the Cessna 188 was so successful that over its 17-year production run the basic airframe remained unchanged. Only the engines and the agricultural products dispensing systems were upgraded, other than some minor changes to the ventilation systems.

Cessna 188 Cessna 188 Agwagon series pictures technical data history

The main use for the Cessna 188 series was for agricultural purposes, but many examples were later acquired for use as glider and sailplane tugs.

Cessna 188 Cessna Model 188 agricultural aircraft

A total of 3976 Cessna 188s of all four variants were built during its production run, made up of 53 AGpickups, 1589 AGwagons, 1949 AGtrucks and 385 AGhuskies.

Variants

188 AGwagon 230
Initial version powered by a Continental O-470-R 230 hp (172 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 3,800 lb (1,724 kg) in the restricted category. Certified on 14 February 1966.
188A AGwagon "A"
Powered by a Continental O-470-R 230 hp (172 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 3,800 lb (1,724 kg) in the restricted category. Certified on 26 September 1969.
188A AGwagon "B"
Powered by a Continental O-470-R 230 hp (172 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 3,800 lb (1,724 kg) in the restricted category. Certified on 26 September 1969.
188B AGpickup
Powered by a Continental O-470-R or O-470-S 230 hp (172 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 3,800 lb (1,724 kg) in the restricted category. Certified on 20 December 1971, production ended in 1976.
A188 AGwagon 300
Initial version powered by a Continental IO-520-D 300 hp (224 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 4,000 lb (1,814 kg) in the restricted category. Certified on 14 February 1966.
A188A AGwagon "A"
Powered by a Continental IO-520-D 300 hp (224 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 4,000 lb (1,814 kg) in the restricted category. Certified on 26 September 1969.
A188A AGwagon "B"
Powered by a Continental IO-520-D 300 hp (224 kW) powerplant, a 200 US gallon (760 liter) chemical hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 4,000 lb (1,814 kg) in the restricted category. Certified on 26 September 1969.
A188B, AGwagon "C" and AGtruck
Powered by a Continental IO-520-D 300 hp (224 kW) powerplant, a 280 US gallon (1060 liter) hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 4,000 lb (1,814 kg) in the restricted category. Certified on 20 December 1971, production of the AGwagon ended in 1981 and the AGtruck in 1985.
T188C AGhusky
Powered by a turbocharged Continental TSIO-520-T 310 hp (231 kW) powerplant, a 280 US gallon (1060 liter) hopper, with a normal category gross weight of 3,300 lb (1,497 kg) and 4,400 lb (1,996 kg) in the restricted category. Certified on 8 September 1978, production ended in 1985.

Aircraft on display

  • Museum of Transport and Technology, Western Springs, Auckland, New Zealand - Cessna A188 Agwagon ZK-COO
  • Aero Space Museum of Calgary, Alberta, Canada - Cessna AgWagon 1966 C-GXQM
  • Specifications (1976 AGtruck)

    Data from Jane's All The World's Aircraft 1976–77

    General characteristics

  • Crew: one pilot
  • Capacity: Hopper: 280 US gal (230 imp gal; 1,100 L)
  • Length: 26 ft 3 in (8.00 m)
  • Wingspan: 41 ft 8 in (12.70 m)
  • Height: 7 ft 8 12 in (2.35 m)
  • Wing area: 205 ft² (19.05 m²)
  • Airfoil: NACA 2412 (modified)
  • Empty weight:
  • With no dispersal equipment installed: 2059 lb (934 kg)
  • With liquid dispersal system: 2214 lb (1004 kg)
  • Loaded weight: 3300 lb (1497 kg)
  • Max. takeoff weight:
  • Normal category: 3300 lb (1496 kg)
  • Restricted category: 4200 lb (1905 kg)
  • Powerplant: 1 × Continental IO-520-D air-cooled flat-six, 300 hp (224 kW)
  • Performance

  • Maximum speed: 121 mph (105 knots, 195 km/h)
  • Cruise speed: 113 mph (98 knots, 182 km/h) (at 75% power)
  • Stall speed:
  • Clean: 61 mph (53 knots, 99 km/h)
  • With full flaps: 57 mph (50 knots, 92 km/h)
  • Range: 370 mi (321 nmi, 595 km)
  • Service ceiling: 11,100 ft (3,383 m)
  • Rate of climb: 690 ft/min (3.5 m/s)
  • References

    Cessna 188 Wikipedia