| Type | Aircraft | |
| Company | Junkers Flugzeug- und Motorenwerke AG | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.5
88.7
|
|
| Height (m) |
0.6
6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
102
925
|
|
| Wingspan (Beam) (m) |
0.1
30.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
5,250
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
8,500
575,000
|
|
| Loaded weight (kg) |
5
8,500
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
one radio operator and one steward |
| Capacity passengers (per.) |
1
15
400
|
15 day passengers or 10 night passengers |
| Speeds | ||
| Max. Speed (km/h) |
25
210
28,165
|
|
| Сruise Speed (km/h) |
52
170
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
1,575
60,000
|
3 powerplants |
| Performance | ||
| Service ceiling (m) |
0.6
4,400
161,544
|
|
| Range (Ferry range) (km) |
4
850
40,700
|
|
| Endurance (h) |
0.0
5
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
180
36,000
|
|
| Stat | ||
| Number built (qt) |
0
13
43,000
|
|
| Introduction | 1926 | |
| First flight | 1926 | |
