Credit
Stephan Widmer · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Configuration
| Specification | Pilatus PC-24 | Shaanxi KJ-200 |
|---|---|---|
| Crew | one or two[source] | — |
| Type | Light business jet[source] | Airborne early warning and control[source] |
| National origin | Switzerland[source] | China[source] |
| Manufacturer | Pilatus Aircraft[source] | Shaanxi Aircraft Corporation[source] |
Wingspan
Single source17.0 m (55 ft 9 in)[source]
Cruise; Cruise speed
Single source810 km/h (510 mph, 440 kn)[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]
Service ceiling
Single source14,000 m (45,000 ft)[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 service[source] |
|---|
| Primary users | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] | — |
|---|
| Number built | 212 (Q1 2024)[source] | 11[source] |
|---|
| Manufactured | 2015–present[source] | — |
|---|
| Introduction date | 1 April 2018[source] | 2007[source] |
|---|
| First flight | 11 May 2015[source] | 2005[source] |
|---|
| Capacity | 10 passengers[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] | — |
|---|
| 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] | — |
|---|
| Primary user | — | People's Liberation Army Air Force People's Liberation Army Navy[source] |
|---|
| Developed from | — | Shaanxi Y-8[source] |
|---|