Polaris Motor FIB

FIB – Flying Inflatable Boat

With Polaris made wings, the flexiwing seaplane is welded steel and uses a Rotax 503 or 582. Three sizes of wings are used: 14, 16, and 18 sq.m.

FIB 503

Stall: 26 kt / 30 mph / 48 kmh
Cruise: 38 kt / 43 mph / 70 kmh
VNE: 43 kt / 50 mph / 80 kmh
Empty Weight: 216 kg / 476 lbs
MTOW Weight: 406 kg / 895 lbs

FIB 503
Empty weight: 182 kg
Wing span: 11 m
Wing area: 21 sq.m
Fuel capacity: 35 lt
Certification: S; J
Engine: Rotax IV DCDI, 48 hp
MAUW: 362 kg
Seats: 2
Max speed: 85 kph
Cruise speed: 65 kph
Minimum speed: 54 kph
Climb rate: 1.8 m/s
Fuel consumption: 11 lt/hr
Price (1998): 27 200 000 L

FIB 582
Empty weight: 170 kg
Wing span: 10 m
Wing area: 14 sq.m
Fuel capacity: 50 lt
Engine: Rotax 582, 64 hp
MAUW: 368 kg
Seats: 2
Max speed: 115 kph
Cruise speed: 90 kph
Minimum speed: 45 kph
Climb rate: 3 m/s
Price (1998): 33 800 000 L

PWS 8

First flown in the autumn of 1929 the PWS-9 was a two/three seat sports and touring biplane. The seating was pilot and one passenger in the rear open cockpit, and the second passenger in the front cockpit. Behind the rear cockpit was a luggage compartment.

The PWS-8 was not built in large numbers.

One PWS-8, SPADA, took part in the 1930 European Challenge Cup and Completion ‘Rundflug’.

Engine: 85 hp Walter Vega
Span upper: 32 ft 9.5 in
Span lower: 24 ft 8 in
Height: 9 ft 8 in
Cruise: 80 mph
Range: 435 mi

PWS 3

The PWS 3 was the first sports aircraft manufactured by the Polish aerospace industry not counting earlier amateur designs. It was designed by Stanislaw Cywinski in the PWS factory in 1927. The fuselage is built upon a bottom boom, what made possible changing of upper fuselage part with cockpits, and developing single-seater, two-seater or other specialized variants.

The PWS 3 was a two-seater parasol wing braced monoplane of wooden construction. The fuselage was built around a box-section wooden boom, with a superstructure of wooden laths, covered with plywood and fabric the front fairing of the aircraft in the rear. The engine compartment was covered with duralumin plating. The empennage was wooden, with a fixed surface, made of plywood and fabric on the control surfaces. The rectangular wooden wings had two spars and was covered with plywood in front and cloth in rear. Originally slotted ailerons on the whole wingspan, later to be shortened. The fuselage had a cockpit for two in tandem, with windscreens and dual controls. The chassis consisted of a fixed split axle conventional chassis, with a rear skid. Both main landing gear and wing struts were installed a small horizontal winglets at the bottom of the fuselage. Fuel in two tanks, 100 litres in total, in the Central section of the wing.

The 5-cylinder Walter NZ 60 radial air-cooled engine provides a nominal power of 60 HP and take-off power of 65 HP, driving a two-bladed wooden fixed pitch propeller. The cruise fuel consumption was 22 l / h.

Prototype 3 PVA designated 3B and issued registration number R-PWSS, was flown on May 20, 1927 in Biała Podlaska. After testing, the handling improved. In 1928, the aircraft underwent modifications, having a rounded tip rather than square, and less aileron.

It took part in the 1st competition of the Polish light aircraft from 6 to 9 October 1927, finishing in 2nd place.

Re-registered SP-ACJ in 1930.

Later it was bought by the Lopp paramilitary organization in Lublin and used for propaganda flights.

PWS 33 Wyzel

Reconnaissance and Liaison Aircraft, Poland, 1936

Engines: 2 x De Havilland Gipsy Major 4 B, 128 hp
Length: 22.769 ft / 6.94 m
Height: 8.399 ft / 2.56 m
Wingspan: 30.381 ft / 9.26 m
Wing area: 136.703 sq.ft / 12.7 sq.m
Max take off weight: 3219.3 lb / 1460.0 kg
Weight empty: 1014.3 lb / 460.0 kg
Max. speed: 170 kts / 315 km/h
Cruising speed: 140 kts / 260 km/h
Service ceiling: 14764 ft / 4500 m
Wing loading: 23.58 lb/sq.ft / 115.0 kg/sq.m
Range: 626 nm / 1160 km
Crew: 2
Armament: 2x MG