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FFA AS.202 Bravo
ffaas202bravo

The Bravo first flew in March 1969, with a 112kW engine, as the 202/15. After completing an agreement with SIAI-Marchetti to produce the AS.202 Bravo, the Swiss developed the AS.202/18A. This suffix indicated its uprated 180-hp (134-kW) Lycoming engine and full aerobatic capability. The Swiss company Flug und Fahrzeugwerke AG Altenrhein flew the first example (HB-HEY) of the AS.202/18A, a two/three-seat aerobatic development of the Italian SIAI-Marchetti AS.202 Bravo on 22 August 1974. These were followed by the 195kW 202/26 in 1978. Civilian and military operators have bought 166 Bravos up to 1987.

AS.202 Bravo
Engine: 1 x Lycoming AEIO-540, 195 kW.
Span: 9.8 m.
Length: 7.5 m.
Wing area: 13.9 sq.m.
Empty wt: 795 kg.
MTOW: 1200 kg.
Warload: 195 kg.
Max speed: 265 kph.
Initial ROC: 360 m / min.
Ceiling: 5700 m.
T/O run: 185 m.
Ldg run: 210 m.
Fuel internal: 160 lt.
Range: 850 km.

FFA AS 202 / 18A Bravo
Length: 24.606 ft / 7.5 m
Height: 9.186 ft / 2.8 m
Wingspan : 32.152 ft / 9.8 m
Wing area : 149.62 sqft / 13.9 sq.m
Max take off weight : 2381.4 lb / 1080.0 kg
Weight empty : 1565.6 lb / 710.0 kg
Max. weight carried : 815.9 lb / 370.0 kg
Max. speed : 130 kts / 241 km/h
Landing speed : 49 kts / 90 km/h
Cruising speed : 110 kts / 203 km/h
Initial climb rate : 787.40 ft/min / 4.00 m/s
Service ceiling : 16995 ft / 5180 m
Wing load : 15.99 lbs/sq.ft / 78.00 kg/sq.m
Range : 616 nm / 1140 km
Engine :
Lycoming AEIO 360 B1F, 132 hp
Crew : 2

AS 202-18A-3 Bravo

AS.202/26 Bravo
Engine: 1 x Lycoming AEIO-540, 195 kW.
Span: 9.8 m.
Length: 7.5 m.
Wing area: 13.9 sq.m.
Empty wt: 795 kg.
MTOW: 1200 kg.
Warload: 195 kg.
Max speed: 265 kph.
Initial ROC: 360 m / min.
Ceiling: 5700 m.
T/O run: 185 m.
Ldg run: 210 m.
Fuel internal: 160 lt.
Range: 850 km.
 


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