| General Data | |||
| First Flown: | 1953 | Length: | 11.57 m |
| Lift Capability: | Height: | 3.12 m | |
| Range: | 392 km | Rotor Span: | 14.64 m |
| Top Speed: | 138 km/h | Empty Weight: | 1297 kg |
| Service Ceiling: | 5490 m | Max Gross Weight: | 2363 kg |
| Engines: | 1 Lycoming 580-D rated at 400 shp | ||
| Armament: | n/a | ||
| Accommodations: | 2 pilots and 4 passengers | Cargo: | |
| Operators: | |||
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| Similar Aircraft: | LZ-4,YH-31,D-10B | ||
| Other Features: | |||
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| Notes | |||
| The production version of the LZ-4. The engine was mounted below the pilots compartment and was connected to the rotors by a fluid coupling | |||




