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
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

Air Tractor AT-300

From Wikipedia, the free encyclopedia

AT-300 family
AT-301
Role Agricultural aircraft
Manufacturer Air Tractor
First flight 1973
Introduction 1976
Status Active
Produced 1973-present

The Air Tractor AT-300 is a family of agricultural aircraft that first flew in the United States on September 1973. Type certification was awarded to Air Tractor in November the same year, and serial production commenced in 1976. Of low-wing monoplane taildragger configuration, they carry a chemical hopper between the engine firewall and the cockpit.


YouTube Encyclopedic

  • 1/3
    Views:
    14 406
    4 543
    2 044
  • Fire Fighting Pilots Needed- Association of Aerial Firefighters Dec 2017
  • Pressure Washing Chemical Sprayer (Contractor Series Video)
  • Compressor Wash

Transcription

Variants

Specifications (AT-301A)

Data from Jane's All The World's Aircraft 1988–89 [1]

General characteristics

  • Crew: 1
  • Capacity: 320 US gal (270 imp gal; 1,200 L) hopper
  • Length: 27 ft 0 in (8.23 m)
  • Wingspan: 45 ft 1+14 in (13.748 m)
  • Height: 8 ft 6 in (2.59 m)
  • Wing area: 270 sq ft (25 m2)
  • Aspect ratio: 7.5:1
  • Airfoil: NACA 4415
  • Empty weight: 3,800 lb (1,724 kg) (spray equipped)
  • Gross weight: 7,400 lb (3,357 kg)
  • Fuel capacity: 126 US gal (105 imp gal; 480 L)
  • Powerplant: 1 × Pratt & Whitney R-1340 radial engine, 600 hp (450 kW)
  • Propellers: 2-bladed Hamilton Standard 12D40/6101A-12 constant-speed propeller, 9 ft 1 in (2.77 m) diameter

Performance

  • Maximum speed: 168 mph (270 km/h, 146 kn) at sea level
  • Cruise speed: 120–140 mph (190–230 km/h, 100–120 kn) (typical working speed)
  • Stall speed: 56 mph (90 km/h, 49 kn) (normal landing weight)
  • Range: 540 mi (870 km, 470 nmi)
  • Rate of climb: 1,600 ft/min (8.1 m/s)

References

Notes

  1. ^ Taylor 1988, pp. 322–323

Bibliography

  • Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 31.
  • Taylor, John W. R., ed. (1988). Jane's All The World's Aircraft 1988–89. Coulsdon, UK: Jane's Defence Data. ISBN 0-7106-0867-5.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 44.

External links

This page was last edited on 7 December 2022, at 04:05
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.