Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      1 m
      3 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      13 m2
      20 m2
    • Wingspan (Beam)
      8 m
      12 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
      648 kg
      974 kg
    • Max. takeoff weight (Gross weight)
      1271 kg
      1907 kg
    • Loaded weight
      1233 kg
      1851 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      4 per.
      6 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      224 km/h
      336 km/h
    • Сruise Speed
      217 km/h
      327 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
      240 hp
      360 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      3960 m
      5940 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1072 km
      1608 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
      254 m/min
      382 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
      6273 qt
      9411 qt
    • Price
      41 USD
      750000000 USD

Piper PA-32 Cherokee 6

TypeAircraft
Company

Piper Aircraft

Scheme

Monoplane

Low wing

Geometry
Length (m)
1.9
 
8.4
88.7
Height (m)
0.6
 
2.4
50.1
Wings
Wing area (m2)
1.1
 
16.5
925
Wingspan (Beam) (m)
0.1
 
10
95
Weights
Empty weight (kg)
8
 
811
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
1,589
575,000
Loaded weight (kg)
5
 
1,542
242,500
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
5
400
Speeds
Max. Speed (km/h)
25
 
280
28,165
Сruise Speed (km/h)
52
 
272
3,087
Power
Total Power (hp)
0.4
 
300
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
4,950
161,544
Range (Ferry range) (km)
4
 
1,340
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
318
36,000
Stat
Number built (qt)
0
 
7,842
43,000
Introduction 1965
First flight 06.12.1963

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