Search filter

    • Year
      1906
      2018
    • Length
      21 m
      32 m
    • Height
      6 m
      10 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      104 m2
      157 m2
    • Wingspan (Beam)
      26 m
      40 m
    • Wing loading
      172 kg/m2
      260 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
      14514 kg
      21773 kg
    • Max. takeoff weight (Gross weight)
      26852 kg
      40280 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      4 per.
      6 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      3628 kg
      5444 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      360 km/h
      540 km/h
    • Сruise Speed
      257 km/h
      387 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
      7940 l
      11911 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
      5600 hp
      8400 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5827 m
      8742 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2936 km
      4404 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
      246 m/min
      370 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
      946 qt
      1420 qt
    • Price
      41 USD
      750000000 USD

Fairchild C-119 Flying Boxcar

TypeAircraft
Company

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
26.4
88.7
Height (m)
0.6
 
8.1
50.1
Wings
Wing area (m2)
1.1
 
130.1
925
Wingspan (Beam) (m)
0.1
 
33.3
95
Wing loading (kg/m2)
3.1
 
216
829
Weights
Empty weight (kg)
8
 
18,143.7
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
33,565.8
575,000
Capacity
Crew (per.)
1
 
5
112
Payload (kg)
23
 
4,535.9
122,470
Speeds
Max. Speed (km/h)
25
 
450
28,165
Сruise Speed (km/h)
52
 
322
3,087
Fuel
Fuel Capacity (l)
23
 
9,925.3
320,000
Power
Total Power (hp)
0.4
 
7,000
60,000
2 powerplants 3500 hp each
Performance
Service ceiling (m)
0.6
 
7,284.7
161,544
Range (Ferry range) (km)
4
 
3,670
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
307.9
36,000
Stat
Number built (qt)
0
 
1,183
43,000
Introduction 1947
First flight 17.11.1947
Stop production 1995

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