| Type | Aircraft | |
| Company | Fokker Aviatik GmbH VFW-Fokker | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
20.6
88.7
|
|
| Height (m) |
0.6
7.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
64
925
|
|
| Wingspan (Beam) (m) |
0.1
21.5
95
|
|
| Weights | ||
| Empty weight (kg) |
8
12,179
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
19,958
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Capacity passengers (per.) |
1
44
400
|
40-44 passengers in 4 abreast seating |
| Speeds | ||
| Max. Speed (km/h) |
25
704
28,165
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
6,320
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
66.4
1,914
|
2 powerplants 33,2 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
7,620
161,544
|
|
| Range (Ferry range) (km) |
4
1,195
40,700
|
with 40 passengers |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
945
36,000
|
|
| Stat | ||
| Introduction | 1971 | |
| First flight | 14.07.1971 | |
