Search filter

    • Year
      1906
      2018
    • Length
      7 m
      12 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      10 m
      17 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
      784 kg
      1176 kg
    • Max. takeoff weight (Gross weight)
      1306 kg
      1960 kg
    • Loaded weight
      1306 kg
      1960 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      297 kg
      447 kg
    • Capacity passengers
      3 per.
      5 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      156 km/h
      236 km/h
    • Сruise Speed
      52 km/h
      3087 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
      23 l
      320000 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
      160 hp
      240 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2800 m
      4200 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      901 km
      1353 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
      139 m/min
      209 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
      144 qt
      216 qt
    • Price
      41 USD
      750000000 USD

Fairchild FC-2

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
9.5
88.7
Height (m)
0.6
 
2.7
50.1
Wings
Wing area (m2)
1.1
 
26.9
925
Wingspan (Beam) (m)
0.1
 
13.4
95
Weights
Empty weight (kg)
8
 
980
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,633
575,000
Loaded weight (kg)
5
 
1,633
242,500
Capacity
Crew (per.)
1
 
2
112
Payload (kg)
23
 
372
122,470
Capacity passengers (per.)
1
 
4
400
Speeds
Max. Speed (km/h)
25
 
196
28,165
Power
Total Power (hp)
0.4
 
200
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,500
161,544
Range (Ferry range) (km)
4
 
1,127
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
174
36,000
Stat
Number built (qt)
0
 
180
43,000
Introduction 1926
First flight 14.06.1926

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