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 | Hava SOJ |
|---|---|---|
| Type | Military transport aircraft[source] | Electronic warfare aircraft[source] |
| National origin | United States[source] | Turkey[source] |
| Manufacturer | Douglas Aircraft Company[source] | Bombardier Global 6000 (airframe modified by TUSAŞ ) Aselsan (mission systems)[source] |
| Status | In service[source] |
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.
| — |
| 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] | 4 planned[source] |
|---|
| First flight | 23 December 1941 ( 1941-12-23 )[source] | — |
|---|
| Developed from | Douglas DC-3[source] | Bombardier Global 6000[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] | — |
|---|
| Primary user | — | Turkish Air Force Pakistan Air Force[source] |
|---|
| Introduction date | — | 2026[source] |
|---|
| Source measurement | — | HAVA SOJ is designed to provide stand-off jamming and electronic attack capabilities against enemy radar and command-and-control systems. It was developer within the Turkish airborne electronic warfare programme, a joint effort between Turkish Aerospace Industries (TUSAŞ) and Aselsan. TUSAŞ is responsible for aircraft modification and certification, while Aselsan develops the electronic warfare suite, which includes wideband receivers, digital radio frequency memory (DRFM) jammers, and signal processing systems. A total of 4 aircraft are planned. The first aircraft was scheduled for delivery in 2026, with final delivery expected in 2028. In addition to its primary electronic attack role, the system is planned to have signals intelligence ( SIGINT ) and electronic intelligence ( ELINT ) capabilities. The aircraft is capable of operating at altitudes of up to approximately 51,000 feet (15,500 m).[source]Hava SOJ · Description; only the objects and conditions stated in this passage |
|---|
| Country of origin | — | Turkey[source]Inventory Origin column; table 1, row 53, cell 4; revision 1377423821; retrieved 2026-10-02 |
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| Reported operators |
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