FORCETALLY
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At a glance
FFA AS 202 Bravolarger figure on 0 of 5
Pilatus PC-24larger figure on 5 of 5
Measured figures
202/15 · Length
Single source7.5 m (24 ft 7 in)[source]
Length
Single sourceConfiguration
| Specification | FFA AS 202 Bravo | Pilatus PC-24 |
|---|---|---|
| Crew | 1 or 2[source] | one or two[source] |
| Type | Civil light aircraft[source] | Light business jet[source] |
| National origin | Switzerland / Italy Germany NG models[source] | Switzerland[source] |
| Manufacturer | FFA / SIAI-Marchetti GOMOLZIG Flugzeug und Maschinenbau[source] | Pilatus Aircraft |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
16.85 m (55 ft 3 in)[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]
Cruise; Cruise speed
Single source810 km/h (510 mph, 440 kn)[source]
202/15 · max fuel no reserve
Single source890 km (550 mi, 480 nmi) max fuel no reserve[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]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | Active[source] | In production[source] |
|---|
| Primary users | Indonesian Air Force Ugandan Air Force[source] | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Number built | 214[source] | 212 (Q1 2024)[source] |
|---|
| Manufactured | 1969–1991 2020-today[source] | 2015–present[source] |
|---|
| First flight | 9 March 1969[source] | 11 May 2015[source] |
|---|
| Retired | Patria Pilot Training 2011[source] | — |
|---|
| Variant | FFT Eurotrainer 2000[source] | — |
|---|
| Airfoil | root: NACA 63 2 618 modified 17.63% ; tip: NACA 63 2 415 modified 15%[source] | — |
|---|
| Fuel capacity | 140 L (37.0 US gal; 30.8 imp gal) in two wing leading-edge tanks[source] | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Propellers | 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller[source] | — |
|---|
| Stall speed | 110 km/h (68 mph, 59 kn) flaps up[source] | 154 km/h (96 mph, 83 kn)[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] | 259 kg/m 2 (53 lb/sq ft)[source] |
|---|
| Power/mass | 0.112 kW/kg (0.068 hp/lb)[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 | — |
|---|
| Introduction date | — | 1 April 2018[source] |
|---|
| Capacity | — | 10 passengers[source] |
|---|
| Aspect ratio | — | 9.35[source] |
|---|
| Cabin | — | 7.01 m × 1.69 m × 1.55 m long × wide × high ( 23 ft 0 in × 5 ft 7 in × 5 ft 1 in)[source] |
|---|
| Cabin altitude | — | 2,438 m at 13,716 m (8,000 ft at 45,000 ft), 8.78 psi (0.605 bar)[source] |
|---|
| Time to altitude | — | 45,000 ft (14,000 m) 27.1 mins[source] |
|---|
| Fuel consumption | — | 0.58 kg/km (2.1 lb/mi) Mach 0.72/416 kn (770 km/h) cruise, 15,375 lb (6,974 kg) weight, FL 450, ISA+3C[source] |
|---|
| Thrust/weight | — | 0.36[source] |
|---|
| Take-off | — | 942 m; 3,091 ft (MTOW, ISA, sea level, dry paved runway)[source] |
|---|
| Landing | — | 734 m; 2,408 ft (Over 50 ft obstacle, MLW, ISA, sea level, dry paved runway)[source] |
|---|
| Reported operators |
| — |
|---|
Maximum take-off; Max takeoff weight
Single source