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    • Year
      1906
      2018
    • Length
      4 m
      8 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      1 m2
      925 m2
    • Wingspan (Beam)
      7 m
      11 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
      308 kg
      463 kg
    • Max. takeoff weight (Gross weight)
      598 kg
      899 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      289 kg
      435 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
      162 km/h
      244 km/h
    • Сruise Speed
      150 km/h
      226 km/h
    • Stall Speed
      64 km/h
      96 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      180 km/h
      270 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
      92 hp
      138 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      2708 m
      4062 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      622 km
      934 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
      141 m/min
      213 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
      588 qt
      884 qt
    • Price
      2396 USD
      3594 USD

Piper PA-16 Clipper

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

High wing

Geometry
Length (m)
1.9
 
6.1
88.7
Height (m)
0.6
 
1.9
50.1
Wings
Wingspan (Beam) (m)
0.1
 
8.9
95
Weights
Empty weight (kg)
8
 
385.6
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
748.4
575,000
Capacity
Crew (per.)
1
 
1
112
Useful load (kg)
26.4
 
362
90,700
Capacity passengers (per.)
1
 
3
400
Speeds
Max. Speed (km/h)
25
 
203
28,165
Сruise Speed (km/h)
52
 
188
3,087
Stall Speed (km/h)
40
 
80
257.7
Never exceed speed (km/h)
108.0
 
225
1,050
Power
Total Power (hp)
0.4
 
115
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
3,385
161,544
Range (Ferry range) (km)
4
 
778
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
176.8
36,000
Stat
Number built (qt)
0
 
736
43,000
Price (USD)
41.5
 
2,995
750.0 million
Introduction 1949
First flight 1947

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