FORCETALLY
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At a glance
Measured figures
Beechcraft 1900D · Length
Single source57 ft 8 in (17.62 m)[source]
202/15 · Length
Single sourceConfiguration
| Specification | Beechcraft 1900 | FFA AS 202 Bravo |
|---|---|---|
| Type | Regional airliner , cargo , and corporate aircraft[source] | Civil light aircraft[source] |
| Manufacturer | Beech Aircraft Corporation Raytheon Aircraft Company[source] | FFA / SIAI-Marchetti GOMOLZIG Flugzeug und Maschinenbau[source] |
| Status | In service[source] | Active[source] |
| Primary users | Ameriflight Alpine Air Express Central Mountain Air Propair[source] |
7.5 m (24 ft 7 in)[source]
Empty; Beechcraft 1900D · Empty weight
Single sourceGross; Beechcraft 1900D · Gross weight
Single sourceMaximum take-off; Beechcraft 1900D · Max takeoff weight
Single source10,874 lb (4,932 kg)[source]
17,227 lb (7,814 kg)[source]
17,120 lb (7,764 kg)[source]
Empty; 202/15 · Empty weight
Single sourceMaximum take-off; 202/15 · (and MLW) aerobatic
Single sourceCruise; Beechcraft 1900D · at 20,000 ft (6,100 m)
Single source280 kn (322 mph, 518 km/h) at 20,000 ft (6,100 m)[source]
Cruise; 202/15 · (utility at MTOW) maximum; 75% power at 2,440 m (8,000 ft)
Single sourceMaximum; 202/15 · (utility at MTOW) at sea level
Single source211 km/h (131 mph, 114 kn) (utility at MTOW) at sea level[source]
211 km/h (131 mph, 114 kn) (utility at MTOW) maximum; 75% power at 2,440 m (8,000 ft)[source]
Beechcraft 1900D · with 19 passenger payload
Single sourceFerry; Beechcraft 1900D · Ferry range
Single source382 nmi (439 mi, 707 km) with 19 passenger payload[source]
1,245 nmi (1,432 mi, 2,306 km)[source]
202/15 · max fuel no reserve
Single source890 km (550 mi, 480 nmi) max fuel no reserve[source]
Beechcraft 1900D · 2 × Pratt & Whitney Canada PT6A-67D turboprops , 1,279 shp ( ) each
Single source2 × Pratt & Whitney Canada PT6A-67D turboprops , 1,279 shp (955 kW) each[source]
202/15 · 1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston engine, 112 kW (150 hp)[source]
202/15 · Wing area
Single source13.86 m 2 (149.2 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Indonesian Air Force Ugandan Air Force[source] |
| Number built | 695[source] | 214[source] |
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| Manufactured | 1982–2002[source] | 1969–1991 2020-today[source] |
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| Introduction date | February 1984[source] | — |
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| First flight | September 3, 1982[source] | 9 March 1969[source] |
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| Developed from | Beechcraft Super King Air[source] | — |
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| Capacity | 19 passengers and 6,356 lb (2,882 kg) useful load[source] | — |
|---|
| Fuel capacity | 4,458 lb (2,022 kg)[source] | 140 L (37.0 US gal; 30.8 imp gal) in two wing leading-edge tanks[source] |
|---|
| Fuel type | Jet A recommended, others usable[source] | — |
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| National origin | United States[source] | Switzerland / Italy Germany NG models[source] |
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| Retired | — | Patria Pilot Training 2011[source] |
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| Variant | — | FFT Eurotrainer 2000[source] |
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| Airfoil | — | root: NACA 63 2 618 modified 17.63% ; tip: NACA 63 2 415 modified 15%[source] |
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| Propellers | — | 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller[source] |
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| Stall speed | — | 110 km/h (68 mph, 59 kn) flaps up[source] |
|---|
| Never exceed speed | — | 322 km/h (200 mph, 174 kn) (utility at MTOW)[source] |
|---|
| Wing loading | — | 72.2 kg/m 2 (14.8 lb/sq ft)[source] |
|---|
| Power/mass | — | 0.112 kW/kg (0.068 hp/lb)[source] |
|---|
| Former operator · Indonesia | — | Indonesia[source] |
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| Former operator · Iraq | — | Iraq[source] |
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| Former operator · Jordan | — | Jordan[source] |
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| Former operator · Morocco | — | Morocco[source] |
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| Former operator · Oman | — | Oman[source] |
|---|
| Role | — | two to three-seat civil light aircraft jointly[source] |
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| Source measurement | — | 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.[source]FFA AS 202 Bravo · Lead; only the objects and conditions stated in this passage With 115 hp Lycoming O-235 -C2A engine[source]FFA AS 202 Bravo · Variants; only the objects and conditions stated in this passage With 150 hp Lycoming O-320 -E2A engine, fixed pitch propeller, optional third aft seat[source]FFA AS 202 Bravo · Variants; only the objects and conditions stated in this passage With 180 hp Lycoming AEIO-360 -B1F engine, constant speed propeller, third aft seat, fully aerobatic.[source]FFA AS 202 Bravo · Variants; only the objects and conditions stated in this passage With 195 kW (260hp) Lycoming AEIO-540 engine. Only one aircraft was manufactured so far.[source]FFA AS 202 Bravo · Variants; only the objects and conditions stated in this passage Two-seat tandem trainer aircraft, powered by a 268 kW (360-hp) Allison 250-B17C turboprop engine. Only one aircraft was manufactured.[source]FFA AS 202 Bravo · Variants; only the objects and conditions stated in this passage Length: 7.5 m (24 ft 7 in)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Wingspan: 9.75 m (32 ft 0 in)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Height: 2.81 m (9 ft 3 in)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Wing area: 13.86 m 2 (149.2 sq ft)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Empty weight: 630 kg (1,389 lb)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Max takeoff weight: 885 kg (1,951 lb) (and MLW) aerobatic[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage 999 kg (2,202 lb) (and MLW) utility[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Powerplant: 1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston engine, 112 kW (150 hp)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Propellers: 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Maximum speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) at sea level[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Cruise speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) maximum; 75% power at 2,440 m (8,000 ft)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage 203 km/h (126 mph; 110 kn) (utility at MTOW) economical; 66% power at 3,050 m (10,000 ft)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Stall speed: 110 km/h (68 mph, 59 kn) flaps up[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage 89 km/h (55 mph; 48 kn) flaps down[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Never exceed speed : 322 km/h (200 mph, 174 kn) (utility at MTOW)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Range: 890 km (550 mi, 480 nmi) max fuel no reserve[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Service ceiling: 4,265 m (14,000 ft)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage Rate of climb: 3.22 m/s (633 ft/min)[source]FFA AS 202 Bravo · Specifications (202/15); only the objects and conditions stated in this passage |
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| Reported operators | — |
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