Caproni Ca 142
Development and Features
The Caproni Ca 142 aircraft represented a modification of the Ca 133 model. Key distinctions of this updated version included retractable landing gear and an increased aircraft weight. The prototype of the aircraft undertook its maiden flight at Taliedo airfield in November 1935.
Testing and Military Service
Subsequent testing of the aircraft indicated that the planned improvements in flight performance were not achieved. Despite these results, the sole example of the Ca 142 was handed over to the military in September 1937, after which it received the registration number MM 327.
Technical Specifications
| Modification | Ca.142 |
| Wingspan, m | 21.44 |
| Length, m | 15.45 |
| Height, m | 4.00 |
| Wing area, m2 | 65.00 |
| Empty weight | 4 425 |
| Normal takeoff weight | 6 925 |
| Engine type | 3 Piston engines Piaggio Stella P.VII C16 |
| Power, hp | 3 x 460 |
| Maximum speed, km/h | 286 |
| Cruising speed, km/h | 250 |
| Crew | 4 crew |
| Armament | four 7.7-mm machine guns, two 500-kg bombs |
Image and diagram gallery of the Caproni Ca 142
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ArchivoAéreo Editorial Team
A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.
Sources & Accuracy
The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.