Breda A.9
title: "Breda A.9" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["breda-aircraft", "1920s-italian-military-trainer-aircraft", "biplanes", "single-engined-tractor-aircraft", "aircraft-first-flown-in-1928"] topic_path: "geography/italy" source: "https://en.wikipedia.org/wiki/Breda_A.9" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::data[format=table title="Infobox aircraft"]
| Field | Value |
|---|---|
| name | A.9 |
| image | Breda A.9, scheda Aerei da Guerra.jpg |
| type | Trainer |
| manufacturer | Breda |
| first_flight | 1928 |
| primary_user | Regia Aeronautica |
| :: |
|name=A.9 |image=Breda A.9, scheda Aerei da Guerra.jpg |caption= |type=Trainer |manufacturer=Breda |designer= |first_flight=1928 |introduction= |retired= |status= |primary_user=Regia Aeronautica |more_users= |produced= |number_built= |variants=
The Breda A.9 was a biplane trainer produced in Italy in 1928 for the Regia Aeronautica. Conventional in design, it featured a single-bay, unstaggered wing cellule and fixed tailskid undercarriage. The student and instructor sat in tandem, open cockpits. A slightly smaller version, designated '*A.9-*bis''''' was developed for use in Italy's aeroclubs.
Operators
;Kingdom of Italy
Variants
;A.9 : Two-seat advanced training biplane. ;A.9bis: A slightly smaller 8.72 m span version for aeroclubs. ;A.10 : Single-seat, 8.84 m span, fighter-trainer prototype, powered by a 250 hp Isotta Fraschini V.6; one aircraft built.
Specifications (A.9)
|ref=Jane's all the World's Aircraft 1928. |prime units?=met General characteristics
|crew=2 |length m=7.95 |span m=9.32 |height m=2.97 |wing area sqm=27 |aspect ratio= |airfoil= |empty weight kg=770 |gross weight kg=1050 |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= Powerplant
|eng1 number=1 |eng1 name=Isotta Fraschini Asso 200 |eng1 type=6-cylinder water-cooled in-line piston engine |eng1 hp=250
|prop blade number=2 |prop name=fixed pitch propeller |prop dia m= |prop dia ft= |prop dia in= |prop dia note= Performance
|max speed kmh=185 |cruise speed kmh= |stall speed kmh=75 |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |range km=800 |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance=3 hours |ceiling m=6000 |g limits= |roll rate= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |wing loading kg/m2=39 |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass=0.119 hp/lb |more performance=
References
References
- (1928). "Jane's all the World's Aircraft 1928". Sampson Low, Marston & company, ltd.
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