Mi-26TS. First flight: 1995 © Konstantinos Panitsidis

Photos from the personal collection of Kostas Panitsidis


 Technical specifications      Photos      Video

 

 

In 1995, the Mi-26T obtained a IAC Aviaregister certificate under the FAR-29 and was redesignated as Mi-26TS.

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Mil
TYPE
Multipurpose Transport helicopter
CREW
5
POWER-PLANT
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
8,15
WEIGHT
 
Empty, kg
28.200
Normal take-off, kg
49.600
Maximum take-off, kgg
56.000
PERFORMANCE
 
Maximum speed, km/h
295
Cruising speed, km/h
255
Range, km
2.000
Service ceiling, m
6.500
Static ceiling, m
1.520
Payload, kg 70 passengers or 20 passengers VIP or or 60 litters or 20.000 kg freight in cabin.
or with on hook, kg
18.500

 


PHOTOS  Mi-26TS

 


VIDEO

Mi-26T © www.Redstar.gr
(take off 57.000 kg!)