The Amiot 110 was designed as a contender in the so-called "Jockey" lightweight interceptor contest, competing against nine other types. It was a braced parasol wing monoplane with an all-metal structure and metal skinned fuselage. The first prototype had a fabric covered wing, replaced by metal skinning in the second. It had fixed, conventional landing gear; the stub wing behind the gear was part of a jettisonable fuel tank.^[1][2]

It first flew in June 1928 and looked a promising candidate to win the "Jockey" contest. However it crashed on 1 July 1929, killing the pilot^[1] due to several loose rivets and integrity flaws. No further production went ahead after a second prototype was deemed inferior to the Nieuport-Delage NiD 62.^{[citation needed]}

Data from Les Ailes,May 1929^[2] unless noted

General characteristics

• Crew: One
• Length: 6.50 m (21 ft 4 in)
• Wingspan: 10.50 m (34 ft 5 in)
• Height: 2.80 m (9 ft 2 in)
• Wing area: 21 m² (230 sq ft)
• Empty weight: 1,120 kg (2,469 lb)
• Gross weight: 1,500 kg (3,307 lb)
• Powerplant: 1 × Hispano-Suiza 12Mb water-cooled V-12, 370 kW (500 hp) ^[1]
• Propellers: 2-bladed

Performance

• Maximum speed: 290 km/h (180 mph, 160 kn) at ground level, 275 km/h (171 mph; 148 kn) at 4,000 m (13,000 ft)
• Stall speed: 95 km/h (59 mph, 51 kn) minimum speed
• Range: 500 km (310 mi, 270 nmi) ^[1]
• Service ceiling: 8,000 m (26,000 ft)
• Time to altitude: 8 min to 4,000 m (13,000 ft)
• Wing loading: 71.4 kg/m² (14.6 lb/sq ft)
• Landing speed: 80 km/h (50 mph; 43 kn)

Armament

• Guns: 2 × 0.303 in (7.70 mm) Vickers machine guns.^[1]