Weatherly 620
The Weatherly 620 is a 1970s American agricultural monoplane designed and built as an improved variant of the Weatherly 201 by the Weatherly Aircraft Company of McClellan, California.[1]
| Weatherly 620 | |
|---|---|
![]()  | |
| A Weatherly 620B in 1998 | |
| Role | Agricultural aircraft | 
| National origin | United States | 
| Manufacturer | Weatherly Aircraft Company | 
| First flight | 1979 | 
| Number built | 155 | 
| Developed from | Weatherly 201 | 
Design
    
The Weatherley 620 is an all-metal single-seat low-wing cantilever monoplane with a conventional landing gear with a tailwheel. Examples have been fitted with a Pratt & Whitney R-985 radial engine, and PT6A or TPE331 turboprop engine, driving a three-bladed tractor propeller. In the forward fuselage, the aircraft has a either a 355 US gallon hopper or a 320 US gallon hopper that feeds an agricultural dispersal system. Most pilots that fly the weatherly aircraft, prefer the 320 gallon hopper aircraft. [1]
Variants
    
- Model 620
 - 1979 initial production variant.
 - Model 620A
 - 1987 production variant with a Pratt & Whitney R-985 radial engine.
 - Model 620B
 - 1992 production variant with a Pratt & Whitney R-985 radial engine.
 - Model 620TP
 - 1980 turboprop variant with a Pratt & Whitney PT6A-11AG.
 - Model 620B-TG
 - 1997 improved turboprop variant to replace the 620TP with a Honeywell TPE331 turboprop.
 
Specifications (620BTG)
    
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Data from Jane's All The World's Aircraft 2004-05 [1]
General characteristics
- Crew: 1
 - Capacity: 355 US Gallons (1344litres) hopper
 - Length: 29 ft 8 in (9.04 m)
 - Wingspan: 46 ft 8 in (14.22 m)
 - Height: 9 ft 6 in (2.90 m)
 - Wing area: 277 sq ft (23.1 m2)
 - Empty weight: 3,030 lb (1,374 kg)
 - Max takeoff weight: 6,000 lb (2,721 kg)
 - Powerplant: 1 × Honeywell TPE331 turboprop, 500 hp (373 kW)
 
Performance
- Cruise speed: 122 kn (140 mph, 226 km/h)
 - Stall speed: 62 kn (72 mph, 115 km/h)
 - Never exceed speed: 153 kn (176 mph, 283 km/h)
 - Service ceiling: 15,000 ft (4,572 m)
 - Rate of climb: 1,400 ft/min (7.1 m/s)
 
 
References
    
- Notes
 
- Jackson 2004, p. 801
 
- Bibliography
 
- Jackson, Paul, ed. (2004). Jane's All the World's Aircraft 2004-2005. Coulsdon, Surrey, United Kingdom: Jane's Information Group. ISBN 0-7106-2614-2.
 
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