|Role||Long-range night bomber|
The F.130 was a single-engined biplane design in the BN.3 category based on the larger twin-engined F.60 Goliath. The F.130 had a conventional tailskid landing gear and three open tandem cockpits. It was powered by a nose-mounted 447 kW (600 hp) Farman 18 Wd W-18 piston engine.
Following a series of test flights it was underpowered with only one engine and it failed to arouse any interest from either domestic or export customers and was not ordered into production.
- F.130 BN.3
- Three seater night bomber, one built.
- The almost identical transport variant of the F.130 bomber. one built.
Data from 
- Crew: 3
- Wingspan: 25.30 m (83 ft 0 in)
- Wing area: 150 m2 (1614.64 ft2)
- Empty weight: 3230 kg (7121 lb)
- Gross weight: 5570 kg (12,280 lb)
- Powerplant: 1 × Farman 18 Wd W-18 water-cooled piston engine, 447 kW (600 hp)
- Maximum speed: 195 km/h (121 mph)
- Service ceiling: 5200 m (17,060 ft)
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- Orbis 1985, p. 1740
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.