CNA Eta


title: "CNA Eta" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["1930s-italian-sport-aircraft", "compagnia-nazionale-aeronautica", "parasol-wing-aircraft", "single-engined-tractor-aircraft", "aircraft-first-flown-in-1933"] topic_path: "sports" source: "https://en.wikipedia.org/wiki/CNA_Eta" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0

::data[format=table title="Infobox aircraft"]

FieldValue
nameEta
aircraft_typeOne/two seat light aircraft
national_originItaly
manufacturerCompagnia Nazionale Aeronautica (CNA)
number_built1 or 2
first_flight1933
::

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The CNA Eta was a single engine Italian light aircraft, flown in the mid-1930s, that set one and two seat world records as both a landplane and a seaplane. Only one or two were built.

Design and development

During the 1920s the Compagnia Nazionale Aeronautica (CNA) were best known for their flying school in Rome, though they also manufactured experimental aircraft for the government. When they moved their Roman base from Cerveteri to Littorio in 1928, they built a factory in which they could produce both aircraft and aircraft engines; some were designed by other companies, some by themselves. The Eta was both CNA designed and powered.

The Eta was a conventional parasol wing light aircraft that could be configured as a single seater or with two seats in tandem; it could also be fitted with either a fixed conventional undercarriage or floats. It was originally powered by an uncowled, 9-cylinder CNA C-7 supercharged radial engine but later flew with an inverted 6-cylinder air-cooled supercharged inline, the CNA C.VI. The slightly tapered wing was mounted on tall faired parallel struts from the mid-fuselage, assisted by lighter diagonal struts and shorter, forward leaning supports from the upper fuselage. The single seat model placed the open cockpit just behind the wing trailing edge. The tail was conventional, with the tailplane on top of the fuselage and braced from below. The vertical surfaces were rounded. In keeping with the rest of the design, the fixed wheeled undercarriage was very simple, with unfaired wheels mounted on slender V-form struts attached to the lower fuselage.

Operational history

The Eta was chiefly distinguished by setting three lightplane world records. At the time the FAI divided the lightest aircraft between to categories: C.II, single seats with empty weights less than 200 kg (41 lb) and C.I, two seaters weighing less than 400 kg (882 lb). These categories were then each sub-divided into landplane and seaplane. A 130 kW (170 hp) CNA C-7 engine had enabled a Fiat AS.1 to gain the Category I altitude record in December 1932 and on 6 November 1933 the single seat Eta, with the same motor and fitted with floats, set a new C.II record of 8,411 m (27.595 ft). It was then fitted with its wheeled undercarriage and flown to a new C.II landplane record of 10,008 m (32,835 ft) in December 1933. On both occasions the Eta was flown by Furio Niclot Doglio.

By 1936 the Eta was flying as a two-seat seaplane, powered by the in-line, 112 kW (150 hp) CNA C-VI engine and on 15 May it set a new world C.I 100 km (62 mi) circuit speed record of 192.62 km/h (119.7 mph), flown by Gian Giacomo Chiesi with Domenico Rossetti.

Variants

It is not known if these were different aircraft or the same one modified. ;Category II: single seat, CNA C-7 engine, both landplane and seaplane. ;Category I: two seat, CNA C.VI engine, both landplane seaplane.

Specifications (tandem dual control, landplane)

|ref=Italian Civil and Military Aircraft 1930-1945 |prime units?=met General characteristics

|genhide= |crew=2 |capacity= |length m=6.50 |length note= |span m=10.0 |height m=2.49 |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb=904 |empty weight note= |gross weight kg=500 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= Powerplant

|eng1 number=1 |eng1 name=CNA C-7 |eng1 type=9-cylinder supercharged radial |eng1 hp=170 |eng1 note= |power original= |more power= |prop blade number=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=

Performance

|perfhide= |max speed mph=136 |max speed note= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= 25 min to 6,457 m (19,680 ft) |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |power/mass= |thrust/weight= |more performance=

  • Landing speed: 65 km/h; 35 kn (40 mph)

|see also= |related= |similar aircraft= |lists=

References

References

  1. Thompson, Jonathan. (1963). "Italian Civil and Military Aircraft 1930-1945". Aero Publishers, Inc.
  2. (31 March 1927). "WORLD'S RECORDS FOR LIGHT 'PLANES".
  3. "FAI records".

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1930s-italian-sport-aircraftcompagnia-nazionale-aeronauticaparasol-wing-aircraftsingle-engined-tractor-aircraftaircraft-first-flown-in-1933