FFA AS 202 Bravo

AS/SA 202 Bravo
Role	Civil light aircraft
National origin	Switzerland/Italy; Germany NG models
Manufacturer	FFA/SIAI-Marchetti; GOMOLZIG Flugzeug und Maschinenbau
First flight	9 March 1969
Retired	Patria Pilot Training 2011
Status	Active
Primary users	Indonesian Air Force; Ugandan Air Force
Produced	1969–1991; 2020-today
Number built	214
Variants	FFT Eurotrainer 2000

The AS/SA 202 Bravo is a two to three-seat civil light aircraft jointly designed and manufactured by the Swiss company Flug- und Fahrzeugwerke Altenrhein (FFA) and the Italian company Savoia-Marchetti. The aircraft was designated the AS 202 in Switzerland, and the SA 202 in Italy.

Savoia-Marchetti manufactured the wings, undercarriage and engine installation, while FFA manufactured the fuselage, tail and controls, while both companies had assembly plants manufacturing the complete aircraft.

The first Swiss model flew on 9 March 1969, the first Italian aircraft following on 8 May.

Bravo is a rugged all-metal low-wing monoplane with a full vision canopy. Its tricycle landing gear is fixed.

34 15s and 180 18s were built, with most in service with military customers. The biggest civil operator was Patria Pilot Training at Helsinki-Malmi Airport, Finland during 2000–2011.

Variants

AS/SA 202/10: With 115 hp Lycoming O-235-C2A engine
AS/SA 202/15: With 150 hp Lycoming O-320-E2A engine, fixed pitch propeller, optional third aft seat
AS/SA 202/18A: With 180 hp Lycoming AEIO-360-B1F engine, constant speed propeller, third aft seat, fully aerobatic.
AS/SA 202/26A: With 195 kW (260hp) Lycoming AEIO-540 engine. Only one aircraft was manufactured so far.
AS 32T Turbo Trainer: Two-seat tandem trainer aircraft, powered by a 268 kW (360-hp) Allison 250-B17C turboprop engine. Only one aircraft was manufactured.
FFA 2000 / FFT 2000 / Eurotrainer 2000: Composite derivative
Gomolzig AS-202 BRAVO NG

modern version of the FFA AS 202 Bravo, since 2020

Operators

Civil operators

Finland
- Patria Pilot Training – 7 aircraft in 2000–2011. Patria's Bravos are ex-British Aerospace Flying College aircraft. BAE Flying College owned 11 aircraft, but 1 was lost in Scotland claiming 2 lives. Remaining 10 aircraft were sold to private Finnish flying school Pilot Factory, which merged with Patria in 2004–2005.

7 aircraft out of original 10 remain in service. During merger with Patria, one aircraft was sold to private owner. Night-time accident at Helsinki-Malmi airport in 2002 claimed no lives but hull was damaged beyond repair. In August 2010 one aircraft veered off the runway at Helsinki-Malmi and was written off.

Patria's Bravos were replaced with Tecnam P2002JF.

Uganda
- Uganda Central Flying School – 8 aircraft.

Military operators

Uganda
- Ugandan Air Force – 1 aircraft in 2012

Former military operators

Indonesia
- Indonesian Air Force – 40 aircraft. Replaced by G 120TP in 2013 – 2014
Iraq
- Iraqi Air Force
Jordan
- Royal Jordanian Air Force
Morocco
- Royal Moroccan Air Force – 10 aircraft.
- Royal Air Maroc – 5 aircraft.
Oman
- Royal Air Force of Oman
- Royal Flight of Oman – 4 aircraft.

Specifications (202/15)

Data from Jane's All the World's Aircraft 1976-77 ^[1]

General characteristics

Crew: 1 or 2
Length: 7.5 m (24 ft 7 in)
Wingspan: 9.75 m (32 ft 0 in)
Height: 2.81 m (9 ft 3 in)
Wing area: 13.86 m² (149.2 sq ft)
Airfoil: root: NACA 63₂618 modified 17.63%; tip: NACA 63₂415 modified 15%
Empty weight: 630 kg (1,389 lb)
Max takeoff weight: 885 kg (1,951 lb) (and MLW) aerobatic

999 kg (2,202 lb) (and MLW) utility

Fuel capacity: 140 L (37.0 US gal; 30.8 imp gal) in two wing leading-edge tanks
Powerplant: 1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston engine, 112 kW (150 hp)
Propellers: 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller

Performance

Maximum speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) at sea level
Cruise speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) maximum; 75% power at 2,440 m (8,000 ft)

203 km/h (126 mph; 110 kn) (utility at MTOW) economical; 66% power at 3,050 m (10,000 ft)

Stall speed: 110 km/h (68 mph, 59 kn) flaps up

89 km/h (55 mph; 48 kn) flaps down

Never exceed speed: 322 km/h (200 mph, 174 kn) (utility at MTOW)
Range: 890 km (550 mi, 480 nmi) max fuel no reserve
Service ceiling: 4,265 m (14,000 ft)
Rate of climb: 3.22 m/s (633 ft/min)
Wing loading: 72.2 kg/m² (14.8 lb/sq ft)
Power/mass: 0.112 kW/kg (0.068 hp/lb)

References

^ Taylor, John W.R., ed. (1976). Jane's All the World's Aircraft 1976-77 (67th ed.). London: Jane's Yearbooks. pp. 164–165. ISBN 0-3540-0538-3.

[JAWA1976-77-1] Taylor, John W.R., ed. (1976). Jane's All the World's Aircraft 1976-77 (67th ed.). London: Jane's Yearbooks. pp. 164–165. ISBN 0-3540-0538-3.

[1]