Search filter

    • Year
      1906
      2018
    • Length
      8 m
      14 m
    • Height
      2 m
      4 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      24 m2
      37 m2
    • Wingspan (Beam)
      12 m
      20 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      6
      11
    • 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
      1016 kg
      1524 kg
    • Max. takeoff weight (Gross weight)
      2240 kg
      3360 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      112 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      904 kg
      1356 kg
    • Capacity passengers
      8 per.
      12 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      185 km/h
      279 km/h
    • Сruise Speed
      52 km/h
      3087 km/h
    • Stall Speed
      76 km/h
      116 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
      439 hp
      660 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      6557 m
      9837 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      584 km
      876 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
      230 m/min
      346 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
      464 qt
      698 qt
    • Price
      41 USD
      750000000 USD

Fairchild Fairchild-Hiller PC-6 Porter

TypeAircraft
Company

Fairchild Aircraft

Pilatus Aircraft

Scheme

High wing

Monoplane

Geometry
Length (m)
1.9
 
11
88.7
Height (m)
0.6
 
3.2
50.1
Wings
Wing area (m2)
1.1
 
30.2
925
Wingspan (Beam) (m)
0.1
 
15.9
95
Aspect ratio
1.7
 
8.4
25.6
Weights
Empty weight (kg)
8
 
1,270
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
2,800
575,000
Capacity
Payload (kg)
23
 
1,130
122,470
Capacity passengers (per.)
1
 
10
400
Speeds
Max. Speed (km/h)
25
 
232
28,165
Stall Speed (km/h)
40
 
96
257.7
flaps down, power off
Power
Total Power (hp)
0.4
 
549.6
60,000
1 powerplant
Performance
Service ceiling (m)
0.6
 
8,197
161,544
Range (Ferry range) (km)
4
 
730
40,700
with maximum payload
Dynamic Performance
Rate of climb (m/min)
1.9
 
288
36,000
Stat
Number built (qt)
0
 
581
43,000
First flight 04.05.1959

Similar aircraft

Get more

Museums on map

Museums

Comments