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.

 

 

 

Engine: Lycoming O-320-E2A, 150 hp

Wingspan: 31 ft 11.75 in / 9.75 m

Length: 24 ft 7.25 in / 7.50 m

Empty weight: 1388 lb / 630 kg

Max payload: 595 lb / 270 kg

Max cruise 75% 8000ft/2440m: 114 kt / 131 mph / 211 kph

ROC SL: 633 fpm / 193 m/min

Service ceiling: 14.000 ft / 4265 m

Max range: 498 nm / 574 mi / 925 km

Seats: 2

Cabin length: 7 ft 0.5 in / 2.15 m

Cabin width: 3 ft 4.25 in / 1.02 m

Cabin height: 3 ft 7.25 in / 1.10 m

Rear baggage: 220 lb / 100 kg

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.

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

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.