Photo from the personal collection of Redstar.gr
Technical specifications Photos Video
The Mi-26 served as a base for deriving the Mi-26T civilian transport (1995).
The Mi-26Tis designed for transporting cargo weighing up to 20 tons, constructing-and-mounting operations, extinguishing and localizing fires, for rendering medical aid, supply and distribution of fuel to consumers.
TECHNICAL SPECIFICATIONS
DESIGNER
|
OKB Mil
|
TYPE
|
Transport helicopter
|
CREW
|
5
|
POWER-PLANT
|
Two Progress D-136
|
Power, kW
|
2 x 8.380
|
DIMENSIONS
|
|
Length, m
|
33,73
|
Main rotor diameter , m
|
32,00
|
Tail rotor diameter, m
|
7,61
|
Height, m
|
8,145
|
WEIGHT
|
|
Empty, kg
|
28.200
|
Normal take-off, kg
|
49.650
|
Maximum take-off, kg
|
56.000
|
Internal fuel, kg
|
-
|
PERFORMANCE
|
|
Maximum speed, km/hh
|
295
|
Cruising speed, km/h
|
255
|
Range, km
|
2.000
|
Service ceiling, m
|
4.500
|
Static ceiling, m
|
1.800
|
Payload, kg | 120 passengers or 20.000 kg freight in cabin |
- or on hook |
18.500
|
VIDEO
Mi-26T © www.Redstar.gr