Search filter

    • Year
      1906
      2018
    • Length
      10 m
      16 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      21 m2
      33 m2
    • Wingspan (Beam)
      11 m
      18 m
    • Wing loading
      149 kg/m2
      225 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
      2480 kg
      3722 kg
    • Max. takeoff weight (Gross weight)
      4064 kg
      6097 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      2 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      7 per.
      11 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      465 km/h
      699 km/h
    • Сruise Speed
      418 km/h
      628 km/h
    • Stall Speed
      132 km/h
      198 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
      1152 hp
      1728 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      8739 m
      13109 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      3365 km
      5049 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
      580 m/min
      872 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
      153 qt
      231 qt
    • Price
      343200 USD
      514800 USD

Piper PA-42 Cheyenne

TypeAircraft
Company

Piper Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
13.2
88.7
Height (m)
0.6
 
4.5
50.1
Wings
Wing area (m2)
1.1
 
27.2
925
Wingspan (Beam) (m)
0.1
 
14.5
95
Wing loading (kg/m2)
3.1
 
186.7
829
Weights
Empty weight (kg)
8
 
3,101.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
5,080.2
575,000
Capacity
Crew (per.)
1
 
1
112
or 2
Capacity passengers (per.)
1
 
9
400
1-9 passengers
Speeds
Max. Speed (km/h)
25
 
582
28,165
Сruise Speed (km/h)
52
 
523
3,087
at 10700 m
Stall Speed (km/h)
40
 
165
257.7
flaps and undercarriage down
Power
Total Power (hp)
0.4
 
1,440
60,000
2 powerplants 720 hp each
Performance
Service ceiling (m)
0.6
 
10,924.0
161,544
Range (Ferry range) (km)
4
 
2,614
40,700
4
 
4,207
40,700
Dynamic Performance
Rate of climb (m/min)
1.9
 
726
36,000
Stat
Number built (qt)
0
 
192
43,000
Price (USD)
41.5
 
429,000
750.0 million
Introduction 1980
First flight 18.05.1979

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