PZL Kania
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Author: Marek Ślusarczyk (Tupungato) www.wyprawa.info Permission (Reusing this file) Outside Wikipedia projects you must attribute the work to the author: Marek Ślusarczyk or www.microstock.pl. In case of any doubts feel free to e-mail me: marek (at) microstock pl.

The PZL Kania is a follow-up to the Mil Mi-2 helicopter developed by the PZL-Świdnik in Poland.

human-powered helicopter is a subclass of helicopter (]) PZL Kania is a subclass of helicopter (]) Mil Mi-40 is a subclass of helicopter (]) Backpack helicopter is a subclass of helicopter (]) 1
Two PZL Kania helicopters were originally acquired by the Ministry of Environment, Agriculture and Natural Resources in 2
The PZL Kania (Polish Kitty Hawk) is a follow-up to the Mil Mi-2 helicopter, developed by the PZL-Świdnik in Poland. PZL SW-4 The PZL SW-4 Puszczyk (pl.3

Made by PZL-Świdnik.

It is the successor of the Mil Mi-2 .

The specific helicopter is PZL Kania , a improved copy of the Mi-2. Differences on the front part.4
^^^^ PZL Kania crash in Sweeden. ^^^^ Mi-8/17 Crash during Chernobyl rescue attempt.5
Height Main
3.75 m
Height Alt
12
Predecessor
Mil Mi-2
Length Alt
39
Ferry Range Alt
32160.0
Jet Or Prop
prop
Range Main
493.0
Max Speed Alt
8040.0
Type Of Prop
turboshafts
Max Speed Main
215.0
Developed From
Mil Mi-2
Capacity
9
Cruise Speed Main
190.0
Max Takeoff Weight Alt
7826.0
Ceiling Main
4
000 m
Number Built
19
Crew
One
Max Takeoff Weight Main
3550.0
Span Main
14.56 m
Cruise Speed Alt
7080.0
Area Main
167 m²
Primary user
Span Alt
1
Plane Or Copter?
Power Alt
420.0
Engine(prop)
Allison Model 250
Manufacturer
Ceiling More
82500.0
Number Of Props
2
First Flight
3
Production End Year
2006
Climb Rate Main
8.75 m-s
Power Main
313.0
Production Start Year
1986
Climb Rate Alt
1725.0
Length Main
12.03 m
Area Alt
1792.0
Range Alt
18360.0
Related
* Mil Mi-2
Empty Weight Main
2000.0
Ceiling Alt
13120.0
Ferry Range Main
863.0
Produced
1986
Empty Weight Alt
4409.0
Category

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