Search filter

    • Year
      1906
      2018
    • Length
      6 m
      11 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      15 m2
      24 m2
    • Wingspan (Beam)
      9 m
      15 m
    • Wing loading
      83 kg/m2
      125 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
      1165 kg
      1749 kg
    • Max. takeoff weight (Gross weight)
      1723 kg
      2586 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
      4 per.
      8 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      302 km/h
      454 km/h
    • Сruise Speed
      278 km/h
      418 km/h
    • Stall Speed
      90 km/h
      136 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
      352 hp
      528 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6096 m
      9144 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1288 km
      1934 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
      377 m/min
      567 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
      4000 qt
      6000 qt
    • Price
      639200 USD
      958800 USD

Piper PA-34 Seneca

TypeAircraft
Company

Piper Aircraft

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
8.7
88.7
Height (m)
0.6
 
3.0
50.1
Wings
Wing area (m2)
1.1
 
19.4
925
Wingspan (Beam) (m)
0.1
 
11.9
95
Wing loading (kg/m2)
3.1
 
104
829
Weights
Empty weight (kg)
8
 
1,456.9
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,154.6
575,000
Capacity
Crew (per.)
1
 
1
112
Capacity passengers (per.)
1
 
6
400
Speeds
Max. Speed (km/h)
25
 
378
28,165
at 7000 m
Сruise Speed (km/h)
52
 
348
3,087
econ cruise at 7600 m
Stall Speed (km/h)
40
 
113
257.7
wheels and flaps down
Power
Total Power (hp)
0.4
 
440
60,000
2 powerplants 220 hp each
Performance
Service ceiling (m)
0.6
 
7,620
161,544
Range (Ferry range) (km)
4
 
1,611
40,700
max fuel, econ cruise at 5500 m, no reserves
Dynamic Performance
Rate of climb (m/min)
1.9
 
472.4
36,000
Stat
Number built (qt)
0
 
5,000
43,000
Price (USD)
41.5
 
799,000
750.0 million
Introduction 1972
First flight 25.04.1967

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