Fiat G.8
Fiat G.8 is a topic that has captured the interest of many people over time. Its relevance is manifested in different aspects of daily life, from popular culture to politics and economics. As we explore its implications, we discover a universe of possibilities that awaken our curiosity and invite us to reflect on human nature. In this article, we will delve into the depths of Fiat G.8, exploring its origins, impact, and evolution throughout history. Through a detailed analysis, we will seek to better understand this phenomenon and its influence on the modern world.
 | This article includes a list of general references, but it lacks sufficient corresponding inline citations. (June 2009) |
| G.8 | |
|---|---|
| |
| Role | Utility aircraft |
| Manufacturer | Fiat |
| Designer | Giuseppe Gabrielli |
| First flight | 24 February 1934 |
| Retired | 1950[1] |
| Primary user | Regia Aeronautica |
| Number built | 61 |
The Fiat G.8 was a military utility aircraft produced in Italy in the mid-1930s. Its design and production were undertaken at the CMASA works in Pisa which became part of Fiat in 1930, hence the type is sometimes referred to as the CMASA G.8 or Fiat-CMASA G.8. It was a conventional biplane design with staggered wings of unequal span braced by struts arranged in a Warren truss. The pilot and a single passenger (or instructor) sat in tandem open cockpits, and the aircraft was fitted with fixed tailskid undercarriage with divided main units.
Sixty of these aircraft were purchased by the Regia Aeronautica and used for liaison and training duties.
Operators
- Italian Air Force operated three Fiat G.8s until 1950[2]
Specifications
Data from [citation needed]
General characteristics
- Crew: one, pilot
- Capacity: one passenger
- Length: 7.00 m (23 ft 0 in)
- Wingspan: 8.76 m (28 ft 9 in)
- Height: 2.50 m (8 ft 2 in)
- Wing area: 18.9 m2 (203 sq ft)
- Empty weight: 560 kg (1,230 lb)
- Gross weight: 840 kg (1,850 lb)
- Powerplant: 1 × Fiat A.54 , 99 kW (135 hp)
Performance
- Maximum speed: 212 km/h (132 mph, 115 kn)
- Range: 925 km (575 mi, 500 nmi)
- Service ceiling: 5,200 m (17,100 ft)
Notes
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 389.
- "Уголок неба".
- "Aerei Italiani - Scheda Tecnica - Cmasa G.8". aerei-italiani.net. Archived from the original on 2008-05-15.
