Grumman American AA-1

Airplanes

Length

5.87 m

Flat Wing Span

7.46 m

Height

2.07 m

Flat Wing Area

9.11 m²

Cruise Speed

201 km/h

Max Speed

222 km/h

Max Ceiling

4191 m

Number of Engines

Aircraft Engine

First Flight

1963-07-11

Entry Into service

1968-01-01

Number Built

1820

Maximum Take-Off Weight

0.68 t (paragliders: kg)

Maximum Range

785 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Grumman American AA-1	0.68	785

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Bucciero SVIT	Continental O-200	5.55	7.5		Compare
Aviatika-900 Acrobat		5.7	7.15		Compare
Ganzavia GAK-22 Dinó	Lycoming O-235	6.1	7.7		Compare
Aero AT-3		5.88	7.55	1	Compare
Euler D.II	Oberursel U.I	5.94	7.47		Compare
Freiberger Ron's 1	Lycoming O-320	5.79	7.47		Compare

All data (23 fields)

Name: Grumman American AA-1
Manufacturer: American Aviation Corp
Description: The Grumman American AA-1 series is a family of light, two-seat aircraft.
First Flight: 1963-07-11
Entry Into service: 1968-01-01
Production End: 1978-01-01
Designer: Jim Bede
Type: Sport, personal and trainer aircraft
Length (m): 5.87
Height (m): 2.07
Max Speed (km/h): 222
Cruise Speed (km/h): 201
Min Speed (km/h): 97
Max Ceiling (m): 4191
Rate of Climb (m/s): 3.89
Capacity Description: one passenger
Number Built: 1820
Powerplant Description: 1 × Lycoming O-235-C2C flat-four engine, 81 kW (108 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Grumman_American_AA-1
Flat Wing Span (m): 7.46
Flat Wing Area (m²): 9.11
Aircraft Engine: Lycoming O-235
Number of Engines: 1