List of Different Types of Airplanes in the World
Kamov Ka-126 - airplanes
Kamov Ka-126
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Original source: Own work Author Allocer [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
Author: Allocer [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
Original source: Own work Author Allocer [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
Author: Allocer [edit] Licensing I, the copyright holder of this work, hereby publish it under the following licenses: This file is licensed under the Creative Commons Attribution-Share Alike 3.0 Unported license. You are free: to share – to copy, distribute and transmit the work
The Kamov Ka-126 is a Soviet light utility helicopter with co-axial rotors. Evolved from Ka-26 with engine pods removed from stub wings fitted with one TVO-100 turboshaft engine positioned on top of fuselage modified rotor blades new fuel system.
Made by Industria Aeronautică Română.
It is the successor of the Kamov Ka-26 .
Height Main
4.15 m
Designer
Kamov
Predecessor
Kamov Ka-26
Length Alt
774.7
Jet Or Prop
prop
Range Main
660.0
Loaded Weight Main
3000.0
Height Alt
13
Type Of Prop
turboshaft
Developed Into
Kamov Ka-226
Endurance
18000.0
Introduced
1989
Max Speed Main
190.0
Developed From
Kamov Ka-26
Payload Main
1000.0
Capacity
6
Status
Cruise Speed Main
170.0
Ceiling Main
4650 m
Number Built
17
Crew
2
Span Main
780.0
Area Main
265.5 m²
Span Alt
1300.48
Plane Or Copter?
Power Alt
720 hp
Engine(prop)
1
Manufacturer
Number Of Props
1
First Flight
22
Production End Year
1991
Loaded Weight Alt
6613.0
Power Main
530.0
Production Start Year
1989
Empty Weight Alt
4300.0
Length Main
7.75 m
Payload More
1000
Area Alt
2856.0
Range Alt
215
Similar Aircraft
*K-MAX
Related
* Kamov Ka-26* Kamov Ka-226
Empty Weight Main
1950.0
Produced
1989
Category