CANT 26

{{Infobox aircraft

|name=CANT 26

|image=CANT 26 Aero Digest June,1930.jpg

|caption=

|type=Biplane trainer

|manufacturer=CANT

|designer=

|first_flight=1928

|introduction=

|retired=

|status=

|primary_user=

|more_users=

|produced=

|number_built=7

|variants=

}}

The CANT 26 was an Italian two-seat biplane trainer built by CANT.

Design and development

The CANT 26 was an unusual product of CANT as it was a landplane. It was a two-seat biplane with tailwheel landing gear and powered by a 60 kW (80 hp) engine. Only seven examples were built, one of which competed in the Challenge 1929 trials, and another of which was temporarily converted into a seaplane. One plane was registered in Argentina as R-183 and it was later sold to an Italian citizen resident in Paraguay, Nicola Bo in 1932. He sold it to the Paraguayan Military Air Arm. It received the serial T-6 and it was used as a liaison aircraft during the Chaco War. It was destroyed in a fatal accident during the war on May 5, 1933, killing Capt. José D. Jara (pilot) and Lt. Niemann (passenger).

Operators

;{{flag|Paraguay}}

Specifications

File:CANT_26_3-View_L'Air_January_15,1929.png

{{Aircraft specs

|ref=Jane's all the World's Aircraft 1928{{cite book |title=Jane's all the World's Aircraft 1928 |editor1-last=Grey |editor1-first=C.G. |year=1928 |publisher=Sampson Low, Marston & company, ltd |location=London |pages=160c–161c}}

|prime units?=met

|crew=2

|length m=7

|span m=10

|height m=2.67

|wing area sqm=26.2

|aspect ratio=

|airfoil=

|empty weight kg=370

|gross weight kg=650

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Isotta Fraschini Asso 80

|eng1 type=6-cyl air-cooled in-line piston engine

|eng1 hp=80

|prop blade number=2

|prop name=fixed pitch propeller

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed kmh=150

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=62

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=810

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=3800

|g limits=

|roll rate=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|wing loading kg/m2=25

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass={{cvt|0.145|hp/lb|kW/kg|order=flip}}

|more performance=

}}

References

{{reflist}}

Further reading

  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing
  • Sapienza Fracchia, Antonio Luis: "La Contribución Italiana en la Aviación Paraguaya". Author's edition. Asunción, 2007. 300pp.