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History Brief, by Johan Visschedijk

March 19, 2004

FFA P-16.04


In July 1952 the Flug- und Fahrzeugwerke A.G. (FFA) received a development contract from the Swiss authorities for a single-seat interceptor/strike fighter capable of operating from small, alpine airfields. The first prototype P-16.04 made its maiden flight on April 28, 1955 powered by a 7,900 lb (3583 kg) st Armstrong Siddeley Sapphire A.S.Sa.6 turbojet, but was completely destroyed in September 1955.

The second prototype first flew June 16, 1956 incorporating numerous modifications like the wing thickness/chord ratio reduced from 5.5% to 4%; wing fences at the trailing edge; and reshaped and relocated air intakes. The wing carried extensive high-lift devices to suit the aircraft for operations from short runways situated in high-altitude valleys.

The first of three pre-series aircraft P-16 Mk.II flew for the first time April 15, 1957, this time the power plant was an 11,000 lb (4,990 kg) st Sapphire S.A.Sa.7 turbojet. The aircraft could be fitted with two 1.18 in (30 mm) Oerlikon 302RK cannons and various combinations of Matra air-to-air, Oerlikon air-to-ground missiles, and bombs in the fuselage bay.

In March 1958 a contract for 100 P-16 Mk.III was approved by the Swiss Parliament, and two pre-series aircraft were converted to this configuration, incorporating two 1.18 in (30 mm) Hispano-Suiza 825 cannons and a Matra 1000 launcher for 44 2.68 in (68 mm) rockets and an external load of up to 4,940 lb (2,240 kg).

The first Mk.III flew on July 8, 1959 with the second following on March 24, 1960, but the contract had been cancelled already and the program was ended in June 1960.

However, the data and experience gathered from this project was not all lost as much of it was used by William (Bill) P. Lear in the Learjet twin-engine business aircraft.

Photo Johan Visschedijk Collection

Specifications (P-16 Mk.III)

Type:

Single-seat interceptor/strike fighter

Engine:

One 11,000 lb (4,990 kg) st Armstrong Siddeley Sapphire A.S.Sa.7 turbojet

Span:

36 ft 6.5 in (11.14 m)

Length:

46 ft 11 in (14.30 m)

Height:

13 ft 11.33 in (4.25 m)

Wing area:

sq.ft (323 sq.m)

Empty Wt:

15,520 lb (7.040 kg)

Max T/O Wt:

25,838 lb (11,720 kg)

Max speed:

620 mph (998 km/h) at 26,247 ft (8,000 m)

Max climb:

12,795 ft (3,900 m)/min

Ceiling:

50,000 ft (15,240 m)

Range:

920 mls (1,480 km) on internal fuel

Models

P-16.04:

two prototypes

P-16 Mk.II:

pre-production, three built

P-16 Mk.III:

two converted from Mk.II pre-production aircraft