Credit
Stephan Widmer · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Pilatus PC-24larger figure on 6 of 6
Tecnam P-Mentorlarger figure on 0 of 6
Measured figures
Length
Single source16.85 m (55 ft 3 in)[source]
Length
Single sourceConfiguration
| Specification | Pilatus PC-24 | Tecnam P-Mentor |
|---|---|---|
| Crew | one or two[source] | one[source] |
| Type | Light business jet[source] | Light aircraft[source]P-Mentor |
| National origin | Switzerland[source] | Italy[source]P-Mentor |
| Manufacturer | Pilatus Aircraft[source] | Tecnam |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
6.74 m (22 ft 1 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; Empty weight
Single sourceGross; Gross weight
Single source430 kg (948 lb)
1 × Rotax 912iSc four cylinder, liquid and air-cooled, four stroke aircraft engine
Single source1 × Rotax 912iSc four cylinder, liquid and air-cooled, four stroke aircraft engine , 75 kW (100 hp)[source]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[source]
Wing area
Single source30.91 m 2 (332.6 sq ft)[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
(3,960 ft/min) MTOW, at Sea level
Single source20.1 m/s (3,960 ft/min) MTOW, at Sea level[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 (2022)[source]P-Mentor |
|---|
| Primary users | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] | — |
|---|
| Number built | 212 (Q1 2024)[source] | — |
|---|
| Manufactured | 2015–present[source] | — |
|---|
| Introduction date | 1 April 2018[source] | April 2022[source]P-Mentor |
|---|
| First flight | 11 May 2015[source] | — |
|---|
| Capacity | 10 passengers[source] | one passenger[source] |
|---|
| Aspect ratio | 9.35[source] | — |
|---|
| Fuel capacity | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] | 130 litres (29 imp gal; 34 US gal)[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] | 81 km/h (51 mph, 44 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 | — | 2-bladed variable pitch[source] |
|---|
720 kg (1,587 lb)[source]