Credit
Airwolfhound · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
C-47B-DK · Length
Single source63 ft 9 in (19.43 m)[source]
Configuration
| Specification | Douglas C-47 Skytrain | C-130H |
|---|---|---|
| Type | Military transport aircraft[source] | — |
| National origin | United States[source] | — |
| Manufacturer | Douglas Aircraft Company[source] | — |
| Status | In service[source] | — |
| Primary users | United States Army Air Forces Royal Air Force United States Navy Royal Canadian Air Force See operators[source] | — |
| Number built | 10,174 |
C-47B-DK · Wingspan
Single source95 ft 6 in (29.11 m)[source]
C-47B-DK · Height
Single source17 ft 0 in (5.18 m)[source]
C-47B-DK · pilot, co-pilot, navigator, radio operator
Single source4 (pilot, co-pilot, navigator, radio operator)[source]
C-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]
C-47B-DK · Wing area
Single source987 sq ft (91.7 m 2 )[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.
| — |
| First flight | 23 December 1941 ( 1941-12-23 )[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] | — |
|---|
| Propellers | 3-bladed constant-speed propellers[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] | — |
|---|
| Variant description | — | C-130H[source]Only the source-declared variant C-130H Identical to the C-130E but with more powerful Allison T56-A-15 turboprop engines. Introduced in June 1964 with 308 ordered.[source]Only the source-declared variant C-130H |
|---|
| Reported operators |
| — |
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