{{Short description|Italian warplane}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft |name =SM.78 |image =Savoia-Marchetti S.M.78.jpg |caption = |type =Bomber/reconnaissance flying boat |manufacturer =Savoia-Marchetti |designer = |first_flight =1932 |introduction = |retired = |status = |primary_user = |more_users = |produced = |number_built =49 |unit cost = |variants = }}

The '''Savoia-Marchetti SM.78''' was an Italian bomber/reconnaissance biplane flying boat of the early 1930s.

==Development== The SM.78 first flew at the end of 1932, designed for the role of maritime reconnaissance-bomber. It was one of the many flying boats made by SIAI (Savoia-Marchetti), that in 1915 had started building foreign aircraft under licence, followed two years later by the first of its own designs.

The SM.78 was developed from the SM.62bis. The prototype, which carried the serial number ''MM222'', made its first flight late in 1932<ref name="donald world">Donald 1997, p. 823.</ref> and then transferred the next year to Vigna di Valle for evaluation. The SM.78 was the last biplane flying boat, built or used in large numbers by Italy; 49 were completed in all (32 by Piaggio and 17 by SIAI).

===Technical description=== The SM.78 was a single-bay biplane. It had a long and slim aft fuselage, with a tall welded steel fin and a wooden horizontal tail mounted centrally. The lower hull had two steps, to aid take-off from the sea.

This aircraft evolved from the SM.62bis, retaining practically the same unmodified wings, tail and fuselage, but with a different model of Handley Page flaps.

The hull/fuselage had poplar frames, and longerons made of ash. The plywood-skinned hull had a double-layered bottom, with an external layer of cedar, while the flanks were made from orthogonally arranged laminates of cedar. The fabric-covered wings had spruce longerons and poplar ribs, utilising the low-weight and high-strength characteristics of these woods, and were painted to render them impermeable to water. Twin stabilising floats were mounted at mid-wing.

While the pilot and co-pilot were seated side-by-side in an enclosed cockpit in the prototype, this was replaced by an open cockpit in the production model.<ref name="donald world"/> A crew position mounting a 7.7&nbsp;mm (0.303&nbsp;in) Lewis Gun was situated in the nose, which also contained two cameras. This position was manned by the co-pilot when necessary, the aircraft having a three-man crew. A second, enclosed turret was fitted in the dorsal position, also armed with a 7.7&nbsp;mm (.303&nbsp;in) Lewis gun, manned by the gunner/radio operator, who was also provided with an R.A.350 transmitter and an A.R.4 receiver. The aircraft was not fitted with an intercom, but the two pilots could communicate with the nose position using a "pneumatic message" system in which messages were passed through a tube. The forward machine gun had 564 rounds of ammunition in 12 magazines, while the aft machine gun had 470 in 10 magazines. Bombs were carried in a bomb bay within the lower wing, near to the fuselage. The weapon-load was 700&nbsp;kg (1,540&nbsp;lb) maximum. Typical combinations were: 2 × 250&nbsp;kg (550&nbsp;lb) and 2 × 100&nbsp;kg (220&nbsp;lb) bombs, 6 × 100&nbsp;kg (220&nbsp;lb) bombs, 4 × 70&nbsp;kg (150&nbsp;lb) depth charges, or 6 × 12&nbsp;kg (26&nbsp;lb) training bombs. Smoke generators could also be mounted on the inner hardpoints. A "''Jozza''" bombsight was located on the right in the cockpit, behind a glazed window.

The aircraft was powered by a single Isotta Fraschini Asso 750 W18 engine, generating 671&nbsp;kW (900&nbsp;hp) at takeoff, arranged in a steel structure mounted between the two wings, driving a four-bladed propeller with variable pitch that could be set before takeoff. This, and the much refined hull of this aircraft bestowed a good performance for the time. A CO<sub>2</sub> fire extinguisher was mounted by the engine. A total of 2,200&nbsp;L (580&nbsp;US gal) of fuel could be carried in six unarmoured duralumin fuselage tanks, two aft, two central and two forward.

==Operational history== The SM.78 was built between 1932 and 1935, with only 16 by SIAI and 32 from Piaggio. It equipped the 141° ''Squadriglia'', based at La Spezia, the 144° based at Livorno, the 182° at Nisida and the 189° at Syracuse. It continued to serve until 1938,<ref name="donald world"/> being replaced by the CANT Z.501, a monoplane design with superior performance. Some aircraft remained in service during the early phase of World War II, performing in an air-sea-rescue capacity. Spain, which already operated SM.62s, tried unsuccessfully to acquire a licence to build the SM.78, leaving Italy as the only operator.

==Operators== ; {{flag|Kingdom of Italy}} *Regia Aeronautica

==Specifications (SM.78)== {{Aircraft specs |ref=''Italian Civil and Military Aircraft 1930–1945'' <ref name=Thompson>{{cite book |last=Thompson |first=Jonathon W. |title=Italian Civil and Military Aircraft 1930–1945 |url=https://archive.org/details/italiancivilmili00libg |url-access=limited |year=1963 |publisher=Aero Publishers Inc. |location=USA |isbn=0-8168-6500-0 |page=[https://archive.org/details/italiancivilmili00libg/page/n131 262]}}</ref> |prime units?=met <!-- General characteristics --> |crew=3 |length m=12.26 |length note= |span m=16.66 |span note= |height m=4.34 |height note= |wing area sqft=707.8 |wing area note= |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight lb=6490 |empty weight note= |gross weight lb=11110 |gross weight note= |max takeoff weight kg= |max takeoff weight note= |fuel capacity= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Isotta Fraschini Asso 750 R.C.35 |eng1 type=W-18 liquid-cooled piston engine |eng1 hp=955 |eng1 note=

|prop blade number=3 |prop name=constant-speed propellers |prop dia m=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |max speed kmh=245 |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh=220 |cruise speed note= |stall speed kmh= |stall speed note= |never exceed speed kmh= |never exceed speed note= |minimum control speed kmh= |minimum control speed note= |range km=2400 |range note= |combat range km= |combat range note= |ferry range km= |ferry range note= |endurance=11.5 hours |ceiling m=4000 |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |climb rate ms= |climb rate note= |time to altitude=<br> :*{{cvt|1000|m}} in 5 min 37s :*{{cvt|2000|m}} in 14 min 30 s :*{{cvt|3000|m}} in 29 min 43 s :*{{cvt|3800|m}} in 53 min 40 s |wing loading kg/m2= |wing loading note= |disk loading kg/m2= |disk loading note= |fuel consumption kg/km= |power/mass= |thrust/weight= |more performance= <!-- Armament --> |guns= 4 × 7.7 mm (.303 in) machine guns |bombs= 6 × 100 kg bomb load }}

==See also== {{aircontent <!-- designs which were developed into or from this aircraft: --> |related= *Savoia-Marchetti S.59 *Savoia-Marchetti SM.62 <!-- aircraft similar in appearance or function to this design: --> |similar aircraft= <!-- any lists that are appropriate: --> |lists= *List of Interwar military aircraft *List of flying boats and floatplanes <!-- other articles that could be useful to connect with: --> |see also= }}

==References== {{reflist}}

==Further reading== {{commons category|Savoia-Marchetti SM.78}} * Donald, David, ed. ''The Encyclopedia of World Aircraft''. London: Aerospace Publishing, 1997. {{ISBN|1-85605-375-X}}. * Lembo, Daniele. "SM.78 (in Italian)." ''Storia Militare'' N.19, Westward editions, p.&nbsp;43–49.

{{Savoia-Marchetti aircraft}} {{Portal bar|Italy|Companies|Aviation}}

SM.078 Category:1930s Italian patrol aircraft Category:Biplanes Category:Single-engined pusher aircraft Category:Flying boats Category:Aircraft first flown in 1932