Search filter

    • Year
      1906
      2018
    • Length
      20 m
      31 m
    • Height
      6 m
      11 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      56 m2
      84 m2
    • Wingspan (Beam)
      23 m
      35 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      8963 kg
      13445 kg
    • Max. takeoff weight (Gross weight)
      15818 kg
      23728 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      44 per.
      68 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      368 km/h
      552 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      4112 l
      6168 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      3600 hp
      5400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      4876 m
      7314 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2080 km
      3120 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      353 m/min
      531 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      468 qt
      704 qt
    • Price
      41 USD
      750000000 USD

Fokker F27 Friendship

TypeAircraft
Company

Fokker Aviatik GmbH

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
25.1
88.7
Height (m)
0.6
 
8.7
50.1
Wings
Wing area (m2)
1.1
 
70
925
Wingspan (Beam) (m)
0.1
 
29
95
Weights
Empty weight (kg)
8
 
11,204
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
19,773
575,000
Capacity
Crew (per.)
1
 
3
112
2 or 3
Capacity passengers (per.)
1
 
56
400
48-56 passengers
Speeds
Сruise Speed (km/h)
52
 
460
3,087
Fuel
Fuel Capacity (l)
23
 
5,140
320,000
Power
Total Power (hp)
0.4
 
4,500
60,000
2 powerplants 2250 hp each
Performance
Service ceiling (m)
0.6
 
6,095
161,544
Range (Ferry range) (km)
4
 
2,600
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
442.2
36,000
Stat
Number built (qt)
0
 
586
43,000
Introduction 1955
First flight 24.11.1955

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