Credit
Samuel King Jr. · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Cruise; AT-802U · patrolling speed at 10,000 feet (3,000 m)
Single sourceMaximum; AT-802U · at 10,000 feet (3,000 m) with no weapons
Single source213 kn (245 mph, 394 km/h) at 10,000 feet (3,000 m) with no weapons[source]
180 kn (210 mph, 330 km/h) patrolling speed at 10,000 feet (3,000 m)[source]
Cruise; Cruise speed
Single source810 km/h (510 mph, 440 kn)[source]
AT-802U · full fuel at 8,000 feet (2,400 m)
Single source1,303 nmi (1,499 mi, 2,413 km) full fuel at 8,000 feet (2,400 m)[source]
AT-802U · 1 × Pratt & Whitney PT6A -67F turboprop
Single source1 × Pratt & Whitney PT6A -67F turboprop , 1,600 hp (1,200 kW)[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]
(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.
Configuration
| Specification | L3Harris OA-1K Skyraider II | Pilatus PC-24 |
|---|---|---|
| Crew | — | one or two[source] |
| Type | Attack and Surveillance aircraft[source] | Light business jet[source] |
| National origin | United States[source] | Switzerland[source] |
| Manufacturer | Air Tractor / L3Harris[source] | Pilatus Aircraft[source] |
| Status | In service and production[source] | In production[source] |
| Primary user | United States Air Force[source] | — |
| Number built | 18 as of May 2026[source] | 212 (Q1 2024)[source] |
| Introduction date | 2025[source] | 1 April 2018[source] |
| Developed from | Air Tractor AT-802[source] | — |
| Fuel capacity | wing tanks: 380 U.S. gallons (1,400 L; 320 imp gal) and fuselage tanks: 360 U.S. gallons (1,400 L; 300 imp gal)[source] | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
| Hardpoints | 10 (2 centerline and 8 wing) , with provisions to carry combinations of: Missiles: AGM-114 Hellfire , AGR-20 APKWS carried in LAU-131 A/A rocket pods Bombs: GBU-12 Paveway II[source] | — |
| Propellers | 5-bladed Hartzell Propeller Titanium Dome[source] | — |
| Stall speed | 91 kn (105 mph, 169 km/h) at max gross weight[source] | 154 km/h (96 mph, 83 kn)[source] |
| Missiles | AGM-114 Hellfire , AGR-20 APKWS carried in LAU-131 A/A rocket pods[source] | — |
| Bombs | GBU-12 Paveway II[source] | — |
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
| Manufactured | — | 2015–present[source] |
| First flight | — | 11 May 2015[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] |
| 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] |