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Aero Ae-45 / Ae-145

Aero Ae-145 Super Aero, D-GASA, c/n: 19-014 © Karsten Palt
Photo ©: Karsten Palt

Ae-45 / Ae-145

Touring Aircraft

The Aero Ae-45 resp. Ae-145 is a twin-engined four-seat light touring and corporate travel aircraft with retractable landing gear produced by the Czechoslovak manufacturer AERO Vodochody a.s.. A further variant of the Ae-45 was the Ae-45S Super-Aero.
Crew1
Passengers3
 
Propulsion2 Piston Engine
Engine ModelWalter Minor 4-II
Engine Power (each)77 kW103 hp
 
Speed265 km/h143 kts
  165 mph
Service Ceiling1.350 m4.430 ft
Range1.600 km864 NM
994 mi.
 
Empty Weight960 kg2.116 lbs
max. Takeoff Weight1.600 kg3.527 lbs
 
Wing Span12,25 m40,2 ft
Wing Area17,1 m²184 ft²
Length7,54 m24,7 ft
Height2,35 m7,7 ft
 
First Flight21.07.1947
Production Statusout of production
Total Productionca. 800
 
ICAO CodeAE45
 
Data for (Version)Aero Ae-45S
Remarks
The Aero Ae-45 was the first aircraft developed by AERO after WWII. The versions Ae-45S and Ae-145 were produced by Let Kunovice. The Ae-45S was also license-built in the Peoples Republic of China.

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