| Type |
V1 D-AERE 4 + 26 airliner |
V1 D-ACON 4 + 6 record trials |
V2 D-AETA 4 + 26 airliner |
| Engine |
4 Pratt & Whitney s 1 E-G |
4 BMW 132 L |
4 BMW 132 G |
| Dimensions |
Length 23,85 m , height 6,00 m , span 32,84 m , wing area 118,0 m2 , aspect ratio 9,14 |
| Weights |
Empty 9200 kg, loaded 14000 kg , max. take off weight fuel 1800 kg, oil 200 kg, |
Empty 8800 kg, loaded 21220 kg , max. take off weight fuel 11500 kg, oil 450 kg, |
Empty 9200 kg, loaded 14000 kg , max. take off weight fuel 1800 kg, oil 200 kg, |
| Performance |
Max.. speed 375 km/h at sea level , cruising speed 355 km/h at 1000 m , range 1250 km , endurance 4 h, service ceiling 6100 m , climb 7,2 m/sec, .start runway 400 m, landing speed 105 km/h |
Max.. speed 310 km/h at sea level , cruising speed 280 km/h at 1000 m , range 6500 km , endurance 25 h, service ceiling 3000 m , climb 3,0 m/sec., start runway 1200 m, landing speed 100 km/h |
Max.. speed 350 km/h at sea level , cruising speed 320 km/h at 1000 m , range 1250 km , endurance 4 h, service ceiling 6000 m , climb 6,0 m/sec., start runway 400 m, landing speed 105 km/h |
| Type |
A-0 4 + 26 airliner |
B-1 4 + 16 airliner |
B-2 4 + 26 airliner |
| Engine |
4 BMW 132 L |
4 BMW 132 Dc |
4 BMW 132 H-1 |
| Dimensions |
Length 23,85 m , height 6,00 m , span 32,84 m , wing area 118,0 m2 , aspect ratio 9,14 |
| Weights |
Empty 10925 kg, loaded 17000 kg , max. take off weight fuel 2600 kg, oil 280 kg, |
Empty 11300 kg, loaded 17000 kg , max. take off weight fuel 3700 kg, oil 280 kg, |
Empty 11300 kg, loaded 17500 kg , max. take off weight fuel 2800 kg, oil 280 kg, |
| Performance |
Max.. speed 340 km/h at sea level , cruising speed 325 km/h at 1000 m , range 1700 km , endurance 5,4 h, service ceiling 6000 m , climb 6,0 m/sec., start runway 420 m, landing speed 110 km/h |
Max.. speed 418 km/h at 2600 m, cruising speed 376 km/h at 3000 m , range 2000 km , endurance 5,35 h, service ceiling 7400 m , climb 6,2 m/sec., start runway 400 m, landing speed 118 km/h |
Max.. speed 405 km/h at 1100 , cruising speed 365 km/h at 3000 m , range 1700 km , endurance 4,10 h, service ceiling 7200 m , climb 7,57 m/sec., start runway 420 m, landing speed 118 km/h |
| Type |
C-2 Long range reconaissance |
C-2 Bomber |
C-3/U4 |
| Engine |
4 BMW 132 H-1 |
4 BMW 132 H-1 |
4 BMW 132 R-2 |
| Dimensions |
Length 23,85 m , height 6,00 m , span 32,84 m , wing area 118,0 m2 , aspect ratio 9,14 |
| Weights |
Empty 12950 kg, loaded 22700 kg , max. take off weight fuel 5948 kg, oil 511 kg, |
Empty 12950 kg, loaded 22700 kg , max. take off weight fuel 2214 kg, oil 311 kg, |
Empty 13080 kg, loaded 17500 kg , max. take off weight fuel 5437 kg, oil 513 kg, |
| Performance |
Max.. speed 378 km/h at 1600 m , cruising speed 306 km/h at 4000 m , range 4500 km , endurance 14,7 h, service ceiling 6600 m , climb 4,1 m/sec., start runway 900 m, landing speed 130 km/h |
Max.. speed 378 km/h at 1600 m, cruising speed 320 km/h at 4000 m , range 1570 km , endurance 5 h, service ceiling 6600 m , climb 4,1 m/sec., start runway 900 m, landing speed 130 km/h |
Max.. speed 380 km/h at 5000 m , cruising speed 325 km/h at 5000 m , range 4500 km , endurance 14,50 h, service ceiling 6600 m , climb 4,1 m/sec., start runway 900 m, landing speed 130 km/h |
| Armament |
|
|
1 7.92 mm MG 15 machine gun in Drehkranz D-30 forward dorsal turret with 1,125 rounds
1 13 mm MG 131 machine gun in aft dorsal turret with 1,000 rounds, 1 20 mm (0.79 in) MG 151 cannon in forward ventral gondola position with 800 rounds, 1 7.92 mm MG 15 machine gun in rear ventral gondola position with 750 rounds, 2 7.92 mm MG 15 machine gun in flexible mountings firing laterally, one on each side of the fuselage with 1,500 rounds
Bombs: Up to 1,000 kg of bombs internally or up to 5,400 kg externally on four PVC 1006 underwing racks |
| Type |
C-6 Long range reconaissance |
F Long range reconaissance |
|
| Engine |
4 BMW 132 R-2 |
4 BMW 132 R-2 |
|
| Dimensions |
Length 23,85 m , height 6,00 m , span 32,84 m , wing area 118,0 m2 , aspect ratio 9,14 |
| Weights |
Empty 13225 kg, loaded 22826 kg , max. take off weight fuel 6765 kg, oil 510 kg, |
Empty 13447 kg, loaded 25260 kg , max. take off weight fuel 8795 kg, oil 600 kg, |
|
| Performance |
Max.. speed 380 km/h at 5000 m , cruising speed 325 km/h at 5000 m , range 5500 km , endurance 17 h, service ceiling 6600 m , climb 4,1 m/sec., start runway 900 m, landing speed 130 km/h |
Max.. speed 360 km/h at 5000 m, cruising speed 300 km/h at 4000 m , range 6900 km , endurance 23 h, service ceiling 6000 m , climb 3,5 m/sec., start runway 900 m, landing speed 130 km/h |
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| Armament |
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