Vehicle

Grumman Ag Cat

General Aviation and Light Aircraft

The Grumman G-164 Ag Cat is a single-engined biplane agricultural aircraft that Grumman developed in the 1950s as a purpose-built crop duster, proposed by engineers Joe Lippert and Arthur Koch in 1955 under the project name Farmair 1000. The first G-164 made its maiden flight on 27 May 1957 with a Continental W670 engine. Large military orders kept production away from Grumman's Bethpage plant, so Schweizer built the aircraft under contract from 1958, delivering 2,455 through 1981 before buying the design rights. The basic model was certified with several radial engines, and turbine versions use a Pratt and Whitney Canada PT6A turboprop.

Facts
Year
1957 1
Engine Class
Turboprop 1
Top Speed (km/h)
209 1
Mass (kg)
1429 1
Maximum Mass (kg)
3184 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Grumman Ag Cat (Wikipedia)

Of Make

Source Grumman Ag Cat (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Grumman Ag Cat (Wikipedia)Lead sentence
Quote, Lead sentence
The Grumman G-164 Ag Cat is a single-engined biplane agricultural aircraft, developed by Grumman in the 1950s.

Originated In

Also in Geography Atlas: where this subject originated.

Source Grumman Ag Cat (Wikipedia)Lead sentence, country
Quote, Lead sentence, country
Full production began in January 1959, with Schweizer delivering 12 FAA-certified airplanes to Grumman by March 1959.
Sources
1. Grumman Ag Cat (Wikipedia)
  • Lead sentence
    The Grumman G-164 Ag Cat is a single-engined biplane agricultural aircraft, developed by Grumman in the 1950s.
  • Development, maiden flight
    The aircraft had its maiden flight on May 27, 1957, with Grumman test pilot Hank Kurt at the controls.
  • Specifications (G-164B Super B Turbine), powerplant
    Pratt & Whitney Canada PT6A-34AG turboprop, 750 shp (560 kW)
  • Specifications (G-164B Super B Turbine), maximum speed
    Maximum speed: 113 kn (130 mph, 209 km/h)
  • Specifications (G-164B Super B Turbine), empty weight
    Empty weight: 3,150 lb (1,429 kg)
  • Specifications (G-164B Super B Turbine), maximum takeoff weight
    Max takeoff weight: 7,020 lb (3,184 kg)
  • Lead sentence, country
    Full production began in January 1959, with Schweizer delivering 12 FAA-certified airplanes to Grumman by March 1959.
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.

Transport Atlas

How The World Moves
Sign In
Text size
100%
Theme