<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = SAIMAN LB.2 | logo = | logo_size = | image = Lombardi L.B.2 photo L'Aerophile November 1937.jpg | alt = | caption = | long_caption = | other_names = | aircraft_type = Two seat light aircraft | aim = | outcome = | related = | national_origin = Italy | manufacturer = Societa Anonima Industrie Meccaniche Aeronautiche Navali SAIMAN | design_group = | designer = Francis Lombardi | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = c.1937 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}
The '''SAIMAN LB.2''' was an unconventional Italian two seat cabin side by side sport aircraft designed around 1937, with a single pusher configuration engine, twin tail booms and an early tricycle undercarriage.
==Design and development== As well as its own designs like the SAIMAN 202 cabin monoplane, SAIMAN also constructed other peoples' aircraft. The LB.2 was one of the latter, designed by Francis Lombardi who was well known for his Avia FL.3 trainer aircraft.<ref name=JAWA38/>
The unusually laid out LB.2 was largely of conventional wooden construction. It was a cantilever mid-wing monoplane, with a three section wing consisting of a centre section and two outer panels. The wing's wooden structure was plywood covered at the leading edge and fabric covered aft. Slotted flaps were fitted. Two parallel, rectangular section tail booms, mounted at the wing centre section-outer panel junctions, carried the empennage. Like the wings, the tail surfaces had wooden structures and were plywood and fabric covered. The tailplane and elevator was of constant chord and did not extend beyond the fins, which had swept, straight leading edges and carried curved rudders, cut away below.<ref name=JAWA38/>
The central nacelle of the LB.2 placed the seating well ahead of the wing leading edge and the engine at the trailing edge. It was a flat sided structure of mixed construction, with plywood covering around the nose and cabin and metal around the engine. Seating was enclosed, with access via fuselage side doors. The flat cabin top continued behind the cabin to the engine housing, where an 82 kW (110 hp) Alfa-Romeo 110-I 4-cylinder inverted air-cooled in-line engine was mounted in pusher configuration.<ref name=JAWA38/><ref name=Thompson/>
The LB.2 was one of the first Italian aircraft with a tricycle undercarriage.<ref name=Thompson/> This was non-retractable, with the mainwheels on short vertical oleo legs wing mounted at the root of the tailbooms. The nosewheel was steerable.<ref name=JAWA38/>
==Operational history==
The SAIMAN LB.2 appeared at the Milan show of 1937, though ''Flight'' dismissed it as a "freak".<ref name=Flight/> ''Jane's All the World's Aircraft 1938'' described it as "now built under licence by SAIMAN" but it is not certain that more than the prototype was constructed.<ref name=JAWA38/>
==Specifications == {{Aircraft specs |ref=Jane's All the World's Aircraft 1938<ref name=JAWA38/> |prime units?=met <!-- General characteristics --> |genhide=
|crew= |capacity=2 |length m=6.9 |length note= |span m=11.7 |height m=1.85 |height note= |wing area sqm=15.16 |wing area note= |aspect ratio=<!-- give where relevant eg sailplanes --> |airfoil= |empty weight kg=620 |empty weight note= |gross weight kg=900 |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=Alfa-Romeo 110-I |eng1 type=4-cylinder inverted in-line water-cooled |eng1 hp=110<!-- prop engines --> |eng1 note=<ref name=Thompson/> |power original=
|more power=
|prop blade number=2 |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note=
<!-- Performance --> |perfhide=
|max speed kmh=210 |max speed note= |cruise speed kmh=190 |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=<!-- aerobatic --> |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=500 |range note= |endurance=<!-- if range unknown --> |ceiling m=5500 |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |lift to drag= |wing loading kg/m2=59 |wing loading note= |power/mass=0.091 kW/kg (0.059 hp/lb) |more performance= *'''Landing speed:''' 70 km/h (44 mph; 38 kn)
}}
<!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}
<!--==Notes==-->
==References== {{Commons category|Lombardi L.B.2}}<references>
<ref name=JAWA38>{{cite book |title= Jane's All the World's Aircraft 1938|last= Grey |first= C.G. |year=1972|publisher= David & Charles|location= London|isbn=0715-35734-4|page=193c }}</ref>
<ref name=Thompson>{{cite book |title=Italian Civil and Military Aircraft 1930-1945|url=https://archive.org/details/italiancivilmili00libg|url-access=limited|last=Thompson |first=Jonathan |year=1963|publisher=Aero Publishers, Inc|location=Fallbrook, California |page=[https://archive.org/details/italiancivilmili00libg/page/n126 249]}}</ref>
<ref name=Flight>{{cite journal |date=7 October 1937 |title= Milan Review|journal= Flight|volume=XXXII |issue=1502 |page=352 |url= http://www.flightglobal.com/pdfarchive/view/1937/1937%20-%202766.html }}</ref>
</references> <!-- ==Further reading== --> <!-- ==External links== --> <!-- Navboxes go here -->
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Category:1930s Italian sport aircraft Category:Single-engined pusher aircraft Category:Mid-wing aircraft Category:Aircraft first flown in 1937