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 |