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Société Aéroplanes
SPAD S.XIII


SPAD S.XIII in the colors and markings of Capt. Eddie Rickenbacker, U.S. 94th Aero Squadron. This aircraft is on display at the National Museum of the U.S. Air Force near Dayton, Ohio.
Role biplane fighter
National origin France
Manufacturer SPAD
Designer Louis Béchéreau
First flight 4 April 1917
Primary users Aéronautique Militaire
Royal Flying Corps (Royal Air Force from April 1918)
United States Army Air Service
Number built 8,472
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History Société de Production des Aéroplanes Deperdussin
SPAD S.XIII  



The SPAD S.XIII was a single-engine biplane fighter aircraft. In terms of its construction, it shared a similar configuration and layout to the earlier S.VII,featuring a mainly wooden structure complete with a fabric covering; however, it was generally larger and heavier than its predecessor. Other changes included the tapered chord of its ailerons, the rounded tips of the tailplanes, bulkier cowling accommodating the gear-drive Hispano-Suiza 8B engine choice, and enlarged fin and rudder. The S.XIII was armed with a pair of forward-mounted Vickers machine guns with 400 rounds per gun, which took the place of the single gun that had been used on the earlier aircraft..

The SPAD S.XIII is a French biplane fighter aircraft of the First World War, developed by Société Pour L'Aviation et ses Dérivés (SPAD) from the earlier and highly successful SPAD S.VII...

Variants

The SPAD S.XIII was a single-engine biplane fighter aircraft. In terms of its construction, it shared a similar configuration and layout to the earlier S.VII, featuring a mainly wooden structure complete with a fabric covering; however, it was generally larger and heavier than its predecessor. Other changes included the tapered chord of its ailerons, the rounded tips of the tailplanes, bulkier cowling accommodating the gear-drive Hispano-Suiza 8B engine choice, and enlarged fin and rudder. The S.XIII was armed with a pair of forward-mounted Vickers machine guns with 400 rounds per gun, which took the place of the single gun that had been used on the earlier aircraft.

The S.XIII featured relatively conventional construction, that being a wire-braced biplane with a box-shaped fuselage and a front-mounted engine, except for its interposed wing struts located half-way along the wing span, which gave the fighter the deceptive appearance of being a double-bay aircraft instead of a single bay. This change prevented the landing brace wires from whipping and chafing during flight, and was attributed by Andrews as a key factor for the aircraft's high rate of climb. Otherwise, it had an orthodox structure, comprising wooden members attached to metal joint fixtures. The fuselage consisted of four square-section longerons, complete with wooden struts and cross-members while braced with heavy-gauge piano wire; wire cable was instead used for the flying and landing wires.

A SPAD S.XIII of the American 103rd Aero Squadron - note exposed aileron bellcrank protruding from lower wing, also used for the A.2 "pulpit fighter" and S.VII.
A SPAD S.XIII at Air Service Production Center No. 2, Romorantin Aerodrome, France, 1918
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Avions Marcel Dassault-Breguet Aviation

Dassault Aviation SA Avions
Société de Production des Aéroplanes Deperdussin
SPAD S.XIII

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General Info

    • Crew: 1
    • Length: 6.25 m (20 ft 6 in)
    • Wingspan: 8.25 m (27 ft 1 in) late examples had a span of 8.08 m 
    • Height: 2.60 m (8 ft 6 in)
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Powerplant

  • Empty weight: 601.5 kg (1,326 lb)
  • Gross weight: 856.5 kg (1,888 lb)
  • Powerplant: 1 × Hispano-Suiza 8Ba, Bb or Bd Water cooled 8-cylinder vee-type, 150 kW (200 hp)
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Specifications

  • Maximum speed: 211 km/h (131 mph, 114 kn) at 1,000 m (3,300 ft)
    • Endurance: 2 hours
    • Service ceiling: 6,800 m (22,300 ft)
    • Time to altitude:
      • 2 minutes 20 seconds to 1,000 m (3,300 ft)
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    SPAD S.XIII

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