Credit
Stephan Widmer · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source16.85 m (55 ft 3 in)[source]
SM92 · Length
Single sourceConfiguration
| Specification | Pilatus PC-24 | Technoavia SM92 Finist |
|---|---|---|
| Type | Light business jet[source] | Light utility transport[source] |
| National origin | Switzerland[source] | Russia[source] |
| Manufacturer | Pilatus Aircraft[source] | Technoavia[source] |
| Status | In production[source] | Production |
9.13 m (29 ft 11 in)[source]
Empty; Empty weight
Single sourceMaximum take-off; Max ramp weight
Single sourceMaximum take-off; Max takeoff weight
Single source5,244 kg (11,561 lb)[source]
8,500 kg (18,739 lb) Max ramp weight: 8,545 kg (18,839 lb)[source]
Empty; SM92 · Empty weight
Single sourceMaximum take-off; SM92 · Max takeoff weight
Single source6 passengers (1,200 lb payload)
Single sourceFerry; Ferry range
Single source3,700 km (2,300 mi, 2,000 nmi) , 6 passengers (1,200 lb payload)[source]
3,932 km (2,443 mi, 2,123 nmi)[source]
SM92 · max fuel, 40 minutes reserves
Single source1,380 km (860 mi, 750 nmi) max fuel, 40 minutes reserves[source]
SM92 · 1 × Vedeneyev M14P 9-cylinder air-cooled radial piston engine
Single source1 × Vedeneyev M14P 9-cylinder air-cooled radial piston engine, 269 kW (361 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.
| Primary users | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] | — |
|---|
| Number built | 212 (Q1 2024)[source] | about 30[source] |
|---|
| Manufactured | 2015–present[source] | — |
|---|
| Introduction date | 1 April 2018[source] | — |
|---|
| First flight | 11 May 2015[source] | 28 December 1993[source] |
|---|
| Capacity | 10 passengers[source] | 6 passengers or 2 stretchers plus attendant 600 kg (1,323 lb) cargo[source] |
|---|
| Aspect ratio | 9.35[source] | — |
|---|
| Fuel capacity | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[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] | — |
|---|
| Stall speed | 154 km/h (96 mph, 83 kn)[source] | 100 km/h (62 mph, 54 kn) flaps down[source] |
|---|
| Time to altitude | 45,000 ft (14,000 m) 27.1 mins[source] | — |
|---|
| Wing loading | 259 kg/m 2 (53 lb/sq ft)[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] | — |
|---|
| Propellers | — | 3-bladed constant-speed propeller[source] |
|---|
| Never exceed speed | — | 290 km/h (180 mph, 160 kn)[source] |
|---|