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Bulgaria - Aircraft |
DAR 6
Training aircraft DAR-6 (Laz-1)
It was used also as a communications aircraft. DAR-6 was built up, using the basis of FW 44. 62 were produced since 1932. This biplane had two modifications - DAR-6 (with engine Walter Mars - 145 hp) and DAR-6A (base-training version with engine Walter Vega - 85 hp).
Specifications of DAR-6: engine - 1 x Walter Mars (145 hp) or 1 x Siemens Sh-14A (7 cyl., 160 hp); wing span - 9.05 m; length - 6.85; height - 2.85 m; wing area - 19.30 sq.m; empty weight - 510 kg; flying weight - 770-920 kg; speed - 175-185 km/h (at the ground); rate of climb - 3000 m for 12 min; range - 715 km; ceiling - 4200-4500 m; crew - 1 + 1.
It was used also as a communications aircraft. DAR-6 was built up, using the basis of FW 44. 62 were produced since 1932. This biplane had two modifications - DAR-6 (with engine Walter Mars - 145 hp) and DAR-6A (base-training version with engine Walter Vega - 85 hp).
Specifications of DAR-6: engine - 1 x Walter Mars (145 hp) or 1 x Siemens Sh-14A (7 cyl., 160 hp); wing span - 9.05 m; length - 6.85; height - 2.85 m; wing area - 19.30 sq.m; empty weight - 510 kg; flying weight - 770-920 kg; speed - 175-185 km/h (at the ground); rate of climb - 3000 m for 12 min; range - 715 km; ceiling - 4200-4500 m; crew - 1 + 1.