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First Flight :
No. of Aircrafts :
Serial-Number :
Tactical Code :
Span :
Length :
Height :
Engine :
Weight empty :
Max.TO-Weight :
Speed :
Range :
Rate of Climb :
Service ceiling :
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20.09.1954
26 H-34 G I
25 H-34 G II
70 H-34 G III
H-34 G I
58-532, 58-583, 58-690, 58-701, 58-721, 58-727, 58-740
58-748 to 58-750, 58-782, 58-783, 58-801, 58-802
58-827, 58-828, 58-833, 58-834, 58-854 to 58-857, 58-879
58-881 to 58-883
H-34 G II
58-1089 to 58-1112, 58-1135
H-34 G III
58-1548, 58-1549, 58-1502 to 58-1505, 58-1512 to 58-1516
58-1523 to 58-1527, 58-1536 to 58-1539, 58-1547, 58-1548
58-1553, 58-1557, 58-1561 to 58-1570, 58-1575 to 58-1578
58-1582 to 58-1584, 58-1588, 58-1589, 58-1594, 58-1596, 58-1605
58-1617, 58-1618, 58-1630 to 58-1632, 58-1658
58-1662 to 58-1665, 58-1671 to 58-1673, 58-1677 to 58-1679
58-1732, 58-1813, 58-1590, 58-1602, 58-1619, 58-1733, 58-1737
80+01 to 81+11, 82+01 to 82+05
Rotordiameter 17,07 m
14,37 m
4,54 m
Wright R-1820-84 with 1525 PS
3740 kg
6325 kg
273 km/h
435 km
360 m/min at sea-level
3200 m
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