Credit
Airwolfhound · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Cruise; C-47B-DK · Cruise speed
Single sourceMaximum; C-47B-DK · at 10,000 ft (3,000 m)
Single source224 mph (360 km/h, 195 kn) at 10,000 ft (3,000 m)[source]
160 mph (260 km/h, 140 kn)[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]
C-47B-DK · 2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines takeoff rating
Single sourceC-47B-DK · normal rating at 14,500 ft (4,400 m)
Single source2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines 1,200 hp (890 kW) takeoff rating 1,000 hp (750 kW) normal rating at 14,500 ft (4,400 m)[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 · 633 ft/min
Single source3.22 m/s (633 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Douglas C-47 Skytrain | FFA AS 202 Bravo |
|---|---|---|
| Type | Military transport aircraft[source] | Civil light aircraft[source] |
| National origin | United States[source] | Switzerland / Italy Germany NG models[source] |
| Manufacturer | Douglas Aircraft Company[source] | FFA / SIAI-Marchetti GOMOLZIG Flugzeug und Maschinenbau[source] |
| Status | In service[source] | Active[source] |
| Primary users | United States Army Air Forces Royal Air Force United States Navy Royal Canadian Air Force See operators[source] | Indonesian Air Force Ugandan Air Force[source] |
| Number built | 10,174[source] | 214[source] |
| First flight | 23 December 1941 ( 1941-12-23 )[source] | 9 March 1969[source] |
| Developed from | Douglas DC-3[source] | — |
| Variants | Douglas XCG-17 Douglas AC-47 Spooky Douglas R4D-8[source] | — |
| Capacity | 28 troops or 6,000 lb (2,700 kg) of cargo[source] | — |
| Airfoil | root: NACA 2215 ; tip: NACA 2206[source] | root: NACA 63 2 618 modified 17.63% ; tip: NACA 63 2 415 modified 15%[source] |
| Propellers | 3-bladed constant-speed propellers[source] | 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller[source] |
| Time to altitude | 10,000 ft (3,000 m) in 9 minutes 30 seconds[source] | — |
| Wing loading | 26.3 lb/sq ft (128 kg/m 2 )[source] | 72.2 kg/m 2 (14.8 lb/sq ft)[source] |
| Power/mass | 0.0926 hp/lb (0.1522 kW/kg)[source] | 0.112 kW/kg (0.068 hp/lb)[source] |
| Manufactured | — | 1969–1991 2020-today[source] |
| Retired | — | Patria Pilot Training 2011[source] |
| Variant | — | FFT Eurotrainer 2000[source] |
| Fuel capacity | — | 140 L (37.0 US gal; 30.8 imp gal) in two wing leading-edge tanks[source] |
| 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] |
| Former operator · Indonesia | — | Indonesia[source] |
| Former operator · Iraq | — | Iraq[source] |
| Former operator · Jordan | — | Jordan[source] |
| Former operator · Morocco | — | Morocco[source] |
| Former operator · Oman | — | Oman[source] |
| Role | — | two to three-seat civil light aircraft jointly[source] |
| 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 |
| Reported operators |
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