To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

Taylorcraft Ranch Wagon

From Wikipedia, the free encyclopedia

Model 20 Ranch Wagon
Role Four-seat cabin monoplane
National origin United States
Manufacturer Taylorcraft
First flight 1955
Number built 38

The Taylorcraft Model 20 Ranch Wagon was a four-seat cabin monoplane designed and built by Taylorcraft Aircraft as a development of the earlier experimental Model 18. The Model 20 was constructed of moulded fibreglass over a tubular framework. It had a conventional landing gear and a nose-mounted 225 hp (168 kW) Continental O-470-J engine.

YouTube Encyclopedic

  • 1/2
    Views:
    2 007
    3 889
  • RC Plane with 26 CC Petrol engine Not so good take off
  • Cessna 170B wing removal

Transcription

Variants

Model 20 Ranch Wagon
Utility model powered by a 225hp (168kW) Continental O-470-J engine.[1]
Model 20 Zephyr 400
Tourer variant of 1958 with detailed changes from the basic Model 20.
Model 20AG Topper
Agricultural variant. Chemical hopper or tank in rear of cabin.[1]
Model 20 Seabird
Floatplane variant.

Specifications (Ranch Wagon)

Data from Jane's All The World's Aircraft 1955–56[1]

General characteristics

  • Crew: one
  • Capacity: three passengers
  • Length: 24 ft 4 in (7.42 m)
  • Wingspan: 34 ft 8 in (10.57 m)
  • Height: 7 ft 2 in (2.18 m)
  • Wing area: 175.5 sq ft (16.30 m2)
  • Aspect ratio: 7.11:1
  • Airfoil: Goëttingen 532
  • Empty weight: 1,625 lb (737 kg)
  • Gross weight: 2,750 lb (1,247 kg)
  • Fuel capacity: 66 US gal (55 imp gal; 250 L)
  • Powerplant: 1 × Continental O-470-J air-cooled six-cylinder horizontally-opposed engine, 225 hp (168 kW)

Performance

  • Maximum speed: 160 mph (260 km/h, 140 kn)
  • Cruise speed: 150 mph (240 km/h, 130 kn)
  • Endurance: 5 hours
  • Service ceiling: 15,000 ft (4,600 m)
  • Rate of climb: 1,000 ft/min (5.1 m/s)

References

  1. ^ a b c Bridgman 1955, p. 317.
  • Bridgman, Leonard (1955). Jane's All The World's Aircraft 1955–56. New York: The McGraw Hill Book Company.
  • Simpson, R.W. (1991). Airlife's General Aviation. England: Airlife Publishing. ISBN 1-85310-194-X.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.
This page was last edited on 21 October 2022, at 03:42
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.