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At a glance
Measured figures
C-47B-DK · Length
Single source63 ft 9 in (19.43 m)[source]
EA-330LT · Length
Single sourceConfiguration
| Specification | Douglas C-47 Skytrain | Extra EA-300 |
|---|---|---|
| Type | Military transport aircraft[source] | Aerobatic monoplane[source] |
| National origin | United States[source] | Germany[source] |
| Manufacturer | Douglas Aircraft Company[source] | Extra Flugzeugbau[source] |
| Status | In service[source] | Active |
7.01 m (23 ft 0 in)[source]
Empty; C-47B-DK · Empty weight
Single sourceGross; C-47B-DK · Gross weight
Single sourceMaximum take-off; C-47B-DK · Max takeoff weight
Single source18,135 lb (8,226 kg)[source]
26,000 lb (11,793 kg)[source]
31,000 lb (14,061 kg)[source]
Empty; EA-330LT · typ. equipped
Single sourceGross; EA-330LT · Gross weight
Single sourceC-47B-DK · 2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines takeoff rating
Single sourceC-47B-DK · normal rating at 14,500 ft (4,400 m)
Single source2 × Pratt & Whitney R-1830-90C Twin Wasp 14-cylinder air-cooled radial piston engines 1,200 hp (890 kW) takeoff rating 1,000 hp (750 kW) normal rating at 14,500 ft (4,400 m)[source]
EA-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]
C-47B-DK · Service ceiling
Single source26,400 ft (8,000 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | United States Army Air Forces Royal Air Force United States Navy Royal Canadian Air Force See operators[source] | — |
|---|
| Number built | 10,174[source] | — |
|---|
| First flight | 23 December 1941 ( 1941-12-23 )[source] | May 1988[source] |
|---|
| Developed from | Douglas DC-3[source] | — |
|---|
| Variants | Douglas XCG-17 Douglas AC-47 Spooky Douglas R4D-8[source] | — |
|---|
| Capacity | 28 troops or 6,000 lb (2,700 kg) of cargo[source] | — |
|---|
| Airfoil | root: NACA 2215 ; tip: NACA 2206[source] | root: MA 15S; tip: MA 12S[source] |
|---|
| Propellers | 3-bladed constant-speed propellers[source] | 3-bladed Muehlbauer MTV 9-B-C/C198-25[source] |
|---|
| Time to altitude | 10,000 ft (3,000 m) in 9 minutes 30 seconds[source] | — |
|---|
| Wing loading | 26.3 lb/sq ft (128 kg/m 2 )[source] | — |
|---|
| Power/mass | 0.0926 hp/lb (0.1522 kW/kg)[source] | — |
|---|
| Designer | — | Walter Extra[source] |
|---|
| Manufactured | — | 1988-present[source] |
|---|
| Fuel capacity | — | 209 L / 55,2 gal (usable)[source] |
|---|
| Stall speed | — | 110 km/h (69 mph, 60 kn) at 820 kg / 1,808 lbs[source] |
|---|
| Never exceed speed | — | 410 km/h (250 mph, 220 kn)[source] |
|---|
| g limits | — | +10/-10g at 820 kg / 1,808 lbs[source] |
|---|
| Reported operators |
| — |
|---|
Gross; 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 source