Caproni Ca.104 A.A.

In 1930, the Caproni company introduced its new trainer aircraft, the Caproni Ca.104 A.A. This machine was a variant of the Caproni Ca.100, specifically designed for aerobatic maneuvers.

It differed from its predecessor, the Ca.100, by featuring wings with a larger wingspan and a more powerful powerplant. These enhancements made it ideal for demanding acrobatic displays.

Design and Purpose

The Ca.104 was a two-seater, single-strut biplane, equipped with a 240 hp Walter Castor radial engine. It also featured a two-bladed metal “Reed Caproni” propeller for optimal performance.

Technical Specifications

Throughout 1930, several units of this aircraft were built. This included single-seater versions specifically intended for aerobatic performances and competitions.

Production and Variants

Technical Specifications

Modification	Ca.10 4
Wingspan, m	10.50
Length, m	7.50
Height, m	2.75
Wing area, m2	27.00
Empty weight	680
Normal takeoff weight	845
Engine type	1 Piston engine Walter Castor
Power, hp	1 x 240
Maximum speed, km/h	220
Service ceiling, m	6500
Crew, crew	1-2

Image and diagram gallery of the Caproni Ca.104 A.A.

Ca.104	Ca.104
Ca.104	Ca.104
Ca.104	Ca.104
Ca.104