Credit
FlugKerl2 · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Alto TG European ultralight · Length
Single source6.15 m (20 ft 2 in)[source]
Length
Single sourceConfiguration
| Specification | Direct Fly Alto | Pilatus PC-24 |
|---|---|---|
| Crew | one[source] | one or two[source] |
| Type | Light sport aircraft[source] | Light business jet[source] |
| National origin | Czech Republic[source] | Switzerland[source] |
| Manufacturer | Direct Fly s.r.o.[source] | Pilatus Aircraft |
16.85 m (55 ft 3 in)[source]
Alto TG European ultralight · 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (101 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]
Service ceiling
Single source14,000 m (45,000 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In production[source] | In production[source] |
|---|
| Primary user | Ukrainian Air Force[source] | — |
|---|
| Number built | 41 (2015)[source] | 212 (Q1 2024)[source] |
|---|
| Introduction date | 2008[source] | 1 April 2018[source] |
|---|
| Capacity | one passenger[source] | 10 passengers[source] |
|---|
| Fuel capacity | 118 litres (26 imp gal; 31 US gal)[source] | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Stall speed | 65 km/h (40 mph, 35 kn)[source] | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Never exceed speed | 270 km/h (170 mph, 150 kn)[source] | — |
|---|
| g limits | +4/-2[source] | — |
|---|
| Wing loading | 46.6 kg/m 2 (9.5 lb/sq ft)[source] | 259 kg/m 2 (53 lb/sq ft)[source] |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Manufactured | — | 2015–present[source] |
|---|
| First flight | — | 11 May 2015[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] |
|---|
Maximum take-off; Max takeoff weight
Single source