Search filter

    • Year
      1906
      2018
    • Length
      9 m
      14 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      26 m2
      40 m2
    • Wingspan (Beam)
      13 m
      21 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
      1647 kg
      2472 kg
    • Max. takeoff weight (Gross weight)
      2651 kg
      3977 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      164 km/h
      248 km/h
    • Сruise Speed
      164 km/h
      248 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
      440 hp
      660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3779 m
      5670 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      152 km
      228 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
      304 m/min
      458 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
      9 qt
      15 qt
    • Price
      41 USD
      750000000 USD

Fairchild F-11

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
11.6
88.7
Height (m)
0.6
 
5.0
50.1
Wings
Wing area (m2)
1.1
 
33.0
925
Wingspan (Beam) (m)
0.1
 
16.7
95
Weights
Empty weight (kg)
8
 
2,059.3
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
3,314
575,000
Capacity
Crew (per.)
1
 
2
112
Capacity passengers (per.)
1
 
10
400
depending on configuration of seats
Speeds
Max. Speed (km/h)
25
 
205.9
28,165
at 2438 m
Сruise Speed (km/h)
52
 
206
3,087
Power
Total Power (hp)
0.4
 
550
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,724.4
161,544
Range (Ferry range) (km)
4
 
190
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
381
36,000
Stat
Number built (qt)
0
 
12
43,000
Introduction 1946
First flight 14.06.1946

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