The Armstrong Whitworth F.K.3 was a British two seat general purpose biplane built by Armstrong Whitworth Aircraft during the First World War.
By the end of the war it was considered obsolete for combat.
The Dutch aircraft designer Frederick Koolhoven joined Armstrong Whitworth in 1914.
He designed a series of aircraft that had his initials in their designation.
The F.K.3 followed the basic layout of the Royal Aircraft Factory B.E.2c, which Armstrong Whitworth were building for the Royal Flying Corps.
It was designed as an improvement, with a simplified structure that was easier to build.
The prototype, first flown by Norman Spratt was powered by a 70 hp (52 kW) air-cooled Renault 70 hp V-8.
This aircraft differed from the B.E.2 in eliminating welded joints and complex metal components in the structure, and having greater dihedral on the upper wing.
It retained the seating layout of the B.E.2, with separate cockpits for the pilot and observer, with the latter in front.
An initial batch of seven aircraft to this standard, sometimes referred to as the F.K.2 were built.
This initial batch offered little improvement over the BE.2, and was rejected for service in France.
Aircraft following this initial batch were completed to a revised design, with a new fin and rudder, its leading edge straight and lacking the earlier comma shaped horn balance, and powered by the Renault-related but more powerful 90 hp (67 kW) RAF 1a engine.
Both crew were placed in a single, extended cockpit with the pilot forward, allowing the observer a more effective field of fire, although in the event few F.K.3s were flown with armament.
Trials at Upavon in May 1916 proved that the F.K.3 had a better performance in some respects than the B.E.2c, although it had a smaller useful load.
Armstrong Whitworth were given a contract to build 150 aircraft with another 350 being built by Hewlett & Blondeau Limited at Luton.
Some of the early batch had twin high exhaust pipes that exited above the upper wing in B.E.2 style, but these were later replaced with rams’ horns forward stubs.
Specifications
Crew
2
Length
29 ft 0 in (8.84 m)
Wingspan
40 ft 0 5⁄8 in (12.208 m)
Height
11 ft 10 3⁄4 in (3.626 m)
Wing area
442 sq ft (41.1 m2)
Empty weight
1,386 lb (629 kg)
Gross weight
2,056 lb (933 kg)
Fuel capacity
28 imp gal (34 US gal; 130 L)
Powerplant
1 × RAF 1A air-cooled V-8 engine,
90 hp (67 kW)
Performance
Maximum speed
87 mph (140 km/h, 76 kn) at sea level
Endurance
3 hr
Service ceiling
12,000 ft (3,700 m)
Time to altitude
19 min to 5,000 ft (1,500 m)
Armament
Guns
1 × 0.303 in (7.7 mm) Lewis Gun in rear cockpit
Bombs
Up to 112 lb (51 kg) bombs (if flown as single seater).
