Search filter

    • Year
      1906
      2018
    • Length
      16 m
      26 m
    • Height
      5 m
      9 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      32 m2
      48 m2
    • Wingspan (Beam)
      16 m
      26 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
      7136 kg
      10704 kg
    • Max. takeoff weight (Gross weight)
      10928 kg
      16392 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      2760 kg
      4140 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      26 per.
      40 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      496 km/h
      744 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
      0 hp
      60000 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      7564 m
      11346 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1048 km
      1572 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
      1 m/min
      36000 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
      173 qt
      261 qt
    • Price
      9600000 USD
      14400000 USD

Dornier Do 328

TypeAircraft
Company

Dornier Flugzeugwerke

Fairchild Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
21.1
88.7
Height (m)
0.6
 
7.2
50.1
Wings
Wing area (m2)
1.1
 
40
925
Wingspan (Beam) (m)
0.1
 
21.0
95
Weights
Empty weight (kg)
8
 
8,920
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
13,660
575,000
Capacity
Crew (per.)
1
 
3
112
two Pilots, one Flight Attendant
Useful load (kg)
26.4
 
3,450
90,700
Capacity passengers (per.)
1
 
33
400
30 to 33 (14 in First Class Config)
Speeds
Сruise Speed (km/h)
52
 
620
3,087
Performance
Service ceiling (m)
0.6
 
9,455
161,544
Range (Ferry range) (km)
4
 
1,310
40,700
Stat
Number built (qt)
0
 
217
43,000
Price (USD)
41.5
 
12.0 million
750.0 million
Introduction 1991
First flight 06.12.1991

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