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    • Year
      1906
      2018
    • Length
      5 m
      9 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      12 m2
      19 m2
    • Wingspan (Beam)
      7 m
      12 m
    • Wing loading
      51 kg/m2
      78 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
      435 kg
      654 kg
    • Max. takeoff weight (Gross weight)
      780 kg
      1171 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      344 kg
      516 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      2 per.
      4 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      184 km/h
      276 km/h
    • Сruise Speed
      160 km/h
      240 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
      120 hp
      180 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3520 m
      5280 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      688 km
      1034 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
      160 m/min
      242 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      2 qt
    • Prop diameter
      1 m
      3 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
      26222 qt
      39334 qt
    • Price
      41 USD
      750000000 USD

Piper PA-28 Arrow

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
7.2
88.7
Height (m)
0.6
 
2.3
50.1
Wings
Wing area (m2)
1.1
 
15.1
925
Wingspan (Beam) (m)
0.1
 
9.2
95
Wing loading (kg/m2)
3.1
 
64.4
829
Weights
Empty weight (kg)
8
 
544.8
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
975.2
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
430
90,700
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
230
28,165
Сruise Speed (km/h)
52
 
200
3,087
Power
Total Power (hp)
0.4
 
150
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,400
161,544
Range (Ferry range) (km)
4
 
861.2
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
201.2
36,000
Propellers
Propellers (qt)
1
 
1
8
Prop diameter (m)
1.8
 
1.9
5.8
Stat
Number built (qt)
0
 
32,778
43,000
Introduction 1960
First flight 14.01.1960

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