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    • 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
      7536 kg
      11304 kg
    • Max. takeoff weight (Gross weight)
      12528 kg
      18792 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      2 per.
      4 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      2612 kg
      3920 kg
    • Capacity passengers
      26 per.
      40 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      592 km/h
      888 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
      0 hp
      60000 hp
    • Thrust
      43 kN
      65 kN
    • Service ceiling
      8536 m
      12804 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      2964 km
      4446 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
      88 qt
      132 qt
    • Price
      41 USD
      750000000 USD

Dornier Fairchild-Dornier 328JET

TypeAircraft
Company

Dornier Flugzeugwerke

Fairchild Aircraft

Scheme

Monoplane

High wing

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
 
9,420
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
15,660
575,000
Capacity
Crew (per.)
1
 
3
112
2 pilots + flight attendant
Payload (kg)
23
 
3,266
122,470
Capacity passengers (per.)
1
 
33
400
Speeds
Max. Speed (km/h)
25
 
740
28,165
Power
Thrust (kN)
1.5
 
53.8
1,914
2 powerplants 26,9 kN each
Performance
Service ceiling (m)
0.6
 
10,670
161,544
Range (Ferry range) (km)
4
 
3,705
40,700
with optional long range fuel tank
Stat
Number built (qt)
0
 
110
43,000
Introduction 1998

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