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ZLEA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
De Havilland Canada DHC-6 Twin Otterlarger figure on 1 of 5
Pilatus PC-24larger figure on 4 of 5
Measured figures
Length
Single source49 ft 6 in (15.09 m)[source]
Length
Single sourceConfiguration
| Specification | De Havilland Canada DHC-6 Twin Otter | Pilatus PC-24 |
|---|---|---|
| Type | Utility aircraft[source] | Light business jet[source] |
| Manufacturer | de Havilland Canada Viking Air De Havilland Canada[source] | Pilatus Aircraft[source] |
| Status | In production[source] | In production[source] |
| Number built | March 2026: 1000 (844 DHC, 156 Viking)[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
16.85 m (55 ft 3 in)[source]
578 shp (
Single source578 shp (431 kW)[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]
(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.
212 (Q1 2024)[source] |
| Manufactured | 1965–1988 (Series 100–300) 2008–present (Series 400) 2023–present (Series 300-G)[source] | 2015–present[source] |
|---|
| Introduction date | 1966[source] | 1 April 2018[source] |
|---|
| First flight | 20 May 1965[source] | 11 May 2015[source] |
|---|
| Developed from | de Havilland Canada DHC-3 Otter[source] | — |
|---|
| Passengers | 20[source] | — |
|---|
| Wing geometry | 65 ft 0 in (19.81 m) span, 420 sq ft (39 m 2 ) area (10.05 AR)[source] | — |
|---|
| Powerplant | P&WC PT6 A-20[source] | — |
|---|
| Stall Speed | 65 mph (56 kn; 105 km/h)[source] | 154 km/h (96 mph, 83 kn)[source] |
|---|
| National origin | Canada[source] | Switzerland[source] |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[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] |
|---|
| 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