Credit
Tomás Del Coro · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
EA-330LT · Length
Single source7.01 m (23 ft 0 in)[source]
Length
Single sourceConfiguration
| Specification | Extra EA-300 | Pilatus PC-24 |
|---|---|---|
| Crew | 1 or 2[source] | one or two[source] |
| Type | Aerobatic monoplane[source] | Light business jet[source] |
| National origin | Germany[source] | Switzerland[source] |
| Manufacturer | Extra Flugzeugbau[source] | Pilatus Aircraft[source] |
16.85 m (55 ft 3 in)[source]
Empty; EA-330LT · typ. equipped
Single sourceGross; EA-330LT · Gross weight
Single sourceGross; EA-330LT · normal category (+6/
Single sourceMaximum take-off; EA-330LT · Max takeoff weight
Single sourceMaximum take-off; EA-330LT · single-pilot acro (+10/
Single source677 kg (1,493 lb) typ. equipped[source]
950 kg (2,094 lb) normal category (+6/-3g)[source]
820 kg (1,808 lb) single-pilot acro (+10/-10g)[source]
Empty; Empty weight
Single sourceMaximum take-off; Max ramp weight
Single sourceEA-330LT · 1 × Lycoming AEIO-580 -B1A 6-cylinder air-cooled horizontally-opposed piston engine
Single source1 × Lycoming AEIO-580 -B1A 6-cylinder air-cooled horizontally-opposed piston engine, 235 kW (315 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]
(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.
| Designer | Walter Extra[source] | — |
|---|
| Status | Active[source] | In production[source] |
|---|
| Manufactured | 1988-present[source] | 2015–present[source] |
|---|
| First flight | May 1988[source] | 11 May 2015[source] |
|---|
| Fuel capacity | 209 L / 55,2 gal (usable)[source] | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Airfoil | root: MA 15S; tip: MA 12S[source] | — |
|---|
| Propellers | 3-bladed Muehlbauer MTV 9-B-C/C198-25[source] | — |
|---|
| Stall speed | 110 km/h (69 mph, 60 kn) at 820 kg / 1,808 lbs[source] | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Never exceed speed | 410 km/h (250 mph, 220 kn)[source] | — |
|---|
| g limits | +10/-10g at 820 kg / 1,808 lbs[source] | — |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Number built | — | 212 (Q1 2024)[source] |
|---|
| Introduction date | — | 1 April 2018[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] |
|---|
Maximum take-off; Max takeoff weight
Single source