Macchi M.70

{{Infobox aircraft begin

| name=Macchi M.70

| image=Macchi M.70.jpg

| caption=

}}{{Infobox aircraft type

| type=Light biplane

| national origin=Italy

| manufacturer=Macchi

| designer=

| first flight=Late 1920s

| introduced=

| retired=

| status=

| primary user=

| number built=

| developed from=

| variants with their own articles=

}}

The Macchi M.70, was an Italian light biplane of the late 1920s built by Macchi.

Design and development

File:Macchi M.70 line drawings.JPG magazine, 21 February 1929]]

The M.70 was a two-seat, single-bay biplane with tandem cockpits. The pilot generally sat in the rear cockpit, but both cockpits had flight controls. The fuselage was of wooden construction with plywood skin and was of rectangular section. The wings were of equal span, fairly thick section, and wooden construction; they had fabric covering, and only the lower wing had ailerons. The interplane struts were steel tubes braced with piano wire. The tail surfaces were constructed of steel frames covered by fabric. The rudder was balanced, while the ailerons and elevators were unbalanced.{{cite web|url=http://www.flightglobal.com/pdfarchive/view/1929/1929%20-%200372.html|title=AEROPLANE TYPES The Macchi " M-70 "|year=1925|publisher=Flight|accessdate=30 January 2012}}

The aircraft was powered by the Blackburn Cirrus II engine or similar engines in the 56 to 60 kilowatt (75 to 80 horsepower) range, driving a two-bladed tractor propeller. Its wings were hinged and could be folded back along the fuselage, and the aircraft could be converted from landplane to floatplane configuration by removal of its fixed, V-type, straight-axle wheeled landing gear and installation of twin, single-step floats mounted on four struts.

Operational history

An M.70 flown by an Italian pilot named Agello was among 53 aircraft entered in the 1930 Giro Aereo d'Italia ("Circuit of Italy") race, which more or less circled the Italian "boot" and was held in four stages flown on 25, 27, 29, and 31 August 1930. Rather than be held as a straightforward timed race, the Giro Aereo d{{'}}Italia used a handicapping system to determine a staggered start at the beginning of each of the four stages of the race; the system was biased against aircraft with better pure racing capabilities, adjusting start times to favor planes with other characteristics the race organizers deemed useful in general aviation. During preliminary tests held before the race, an aircraft received a higher number of points if it demonstrated a higher rate of climb, shorter takeoff run, and shorter landing distance, and if it had better "touring qualities"—folding wings, comfort, ease of control in flight, and an ability to accommodate safety features such as the wearing of parachutes, among other things; it was penalized for greater weight and higher engine power. The aircraft with the highest point total was allowed to start first in each stage, those with fewer points starting later at a rate of one minute of delay per point behind.{{cite web|url=http://www.flightglobal.com/pdfarchive/view/1930/untitled0%20-%201047.html|title=Circuit of Italy Contest Won By Italy|year=1930|publisher=Flight|pages=7 & 8|accessdate=30 January 2012}}

Agello{{'}}s M.70, powered by a {{convert|60|kW|hp|abbr=on|0}} Colombo S.53 engine, had among the three shortest takeoff runs and demonstrated the shortest landing distance of any of the 53 entrants, stopping in only 50 meters (164 feet). Overall, the point system placed the M.70 in the ninth starting position, allowing Agello to start with an 11-minute handicap.

Operators

;{{flag|Kingdom of Italy}}

Specifications

File:Macchi_M.70_3-view_Aero_Digest_June,1930.png

{{Aircraft specs

|ref=

|prime units?=met

|genhide=

|crew=two

|capacity=

|length m=7.06

|length ft=23

|length in=2

|length note=

|span m=9.95

|span ft=

|span in=

|span note=

|upper span m=

|upper span ft=

|upper span in=

|upper span note=

|mid span m=

|mid span ft=

|mid span in=

|mid span note=

|lower span m=

|lower span ft=

|lower span in=

|lower span note=

|swept m=

|swept ft=

|swept in=

|swept note=

|dia m=

|dia ft=

|dia in=

|dia note=

|width m=

|width ft=

|width in=

|width note=

|height m=2.95

|height ft=

|height in=

|height note=

|wing area sqm=28.4

|wing area sqft=

|wing area note=

|swept area sqm=

|swept area sqft=

|swept area note=

|volume m3=

|volume ft3=

|volume note=

|aspect ratio=

|airfoil=

|empty weight kg=460

|empty weight lb=

|empty weight note=

|gross weight kg=740

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|lift kg=

|lift lb=

|lift note=

|more general=

|eng1 number=1

|eng1 name=Blackburn Cirrus II

|eng1 type=4-cyl air-cooled in-line piston engine

|eng1 kw=60

|eng1 hp=

|eng1 shp=

|eng1 kn=

|eng1 lbf=

|eng1 note= (or similar)

|power original=

|thrust original=

|eng1 kn-ab=

|eng1 lbf-ab=

|eng2 number=

|eng2 name=

|eng2 type=

|eng2 kw=

|eng2 hp=

|eng2 shp=

|eng2 kn=

|eng2 lbf=

|eng2 note=

|eng2 kn-ab=

|eng2 lbf-ab=

|eng3 number=

|eng3 name=

|eng3 type=

|eng3 kw=

|eng3 hp=

|eng3 shp=

|eng3 kn=

|eng3 lbf=

|eng3 note=

|eng3 kn-ab=

|eng3 lbf-ab=

|more power=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|rot number=

|rot dia m=

|rot dia ft=

|rot dia in=

|rot area sqm=

|rot area sqft=

|rot area note=

|perfhide=

|max speed kmh=155

|max speed mph=

|max speed kts=

|max speed note=

|max speed mach=

|cruise speed kmh=

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=55

|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=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=4,600

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

  • 7 mins to 1,000 m (3,281 ft)
  • 53 mins to 4,000 m (13,123 ft)

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=26

|wing loading lb/sqft=

|wing loading note=

|disk loading kg/m2=

|disk loading lb/sqft=

|disk loading note=

|fuel consumption kg/km=

|fuel consumption lb/mi=

|power/mass=0.0764 kg/kw (0.0476 lbs/hp)

|thrust/weight=

|more performance=

|armament=

|guns=

|bombs=

|rockets=

|missiles=

|hardpoints=

|hardpoint capacity=

|hardpoint rockets=

|hardpoint missiles=

|hardpoint bombs=

|hardpoint other=

|avionics=

}}

See also

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

Notes

{{reflist}}

References

{{commons category|Macchi M.70}}

  • {{cite web|url=http://www.flightglobal.com/pdfarchive/view/1929/1929%20-%200372.html|title=AEROPLANE TYPES The Macchi " M-70 "|year=1925|publisher=Flight|accessdate=30 January 2012}}
  • {{cite web|url=http://www.flightglobal.com/pdfarchive/view/1930/untitled0%20-%201047.html|title=Circuit of Italy Contest Won By Italy|year=1930|publisher=Flight|pages=7 & 8|accessdate=30 January 2012}}

{{Macchi aircraft}}

{{Portal bar|Italy|Companies|Aviation}}

M.70

Category:Floatplanes

Category:1920s Italian civil utility aircraft

Category:Biplanes

Category:Single-engined tractor aircraft

Category:Aircraft with fixed conventional landing gear