Aero A.100

Airplanes

Length

11.08 m

Flat Wing Span

14.7 m

Height

3.6 m

Flat Wing Area

44.3 m²

Max Speed

270 km/h

Max Ceiling

6500 m

Number of Engines

Aircraft Engine

First Flight

1933-01-01

Number Built

Maximum Take-Off Weight

3.219 t (paragliders: kg)

Maximum Range

900 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Aero A.100	3.219	900

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aichi E11A		10.71	14.49		Compare
De Havilland DH.14 Okapi	Rolls-Royce Condor	10.0584	15.24		Compare
Blackburn Blackburn		10.9728	13.716		Compare
Daher Kodiak	Pratt & Whitney Canada PT6	10.3632	13.716	9	Compare
Aleksandrov-Kalinin AK-1		11	14.9		Compare
Curtiss SB2C Helldiver		10.9728	14.9352		Compare

All data (23 fields)

Name: Aero A.100
Manufacturer: Aero Vodochody
Description: The Aero A.100 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s.
First Flight: 1933-01-01
Production End: 1935-01-01
Designer: Aero Vodochody
Type: Light bomber, Reconnaissance aircraft
Length (m): 11.08
Height (m): 3.6
Cockpit Crew: 2
Max Speed (km/h): 270
Max Ceiling (m): 6500
Rate of Climb (m/s): 4.2
Armament: ; 2× forward-firing 7.92 mm (0.312 in) vz. 30 (Česká zbrojovka Strakonice) machine guns ; 2× 7.92 mm vz. 30 (Česká zbrojovka Strakonice) machine guns in a ring mount for the observer; 600 kg (1,300 lb)
National Origin: Czechoslovakia
Number Built: 44
Powerplant Description: 1 × Avia Vr.36 V-12 water-cooled piston engine, 552 kW (740 hp) each
Primary Users: Czechoslovak Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Aero_A.100
Flat Wing Span (m): 14.7
Flat Wing Area (m²): 44.3
Aircraft Engine: Hispano-Suiza 12N
Number of Engines: 1