Mil Mi-26

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Mil Mi-26

Mil Mi-26 “Halo”


Type: Heavy transport helicopter.

Country of Origin: Russia

Accommodation: Four crew. Two pilots seat side-by-side along with one one engineer in the cockpit. A load master is usually carried in the cabin. Upto 85 fully equipped troops can be embarked in the cabin.

Design Features: A conventional semi-monocoque structure of pod and boom type. Vital areas protected by with titanium armor plating. Eight-blade titanium main rotor. The helicopter has a retractable tricycle type landing gear with carbon disc brakes. Differential braking for steering. Fully pressurized cabin.

Rotor Span: 32m, length – 40m, height – 8.15m and disc area – 804 m2

Weights: Empty – 25,000 kg (55,000 lbs.)
…………Normal – 49,000 kg (107,800 lbs.)
…………Maximum – 56,000 kg (123,200 lbs.)

Avionics: INS, flight computer, Map display, weather radar, TFR, and full blind/adverse weather instrumentation. Four axis auto stabilization.

Engine(s): Two Loratev D-136 free turbine turbo-shafts rated at 11, 600 shp. Auto synchronization and boosters for emergencies.

Speed: Maximum – 306 km/h (184 mph; 160 knots)
……….Max. cruising speed 240 km/h (144 mph, 125 knots)

Service Ceiling: 8000 meters (26,240 ft.)

Range: Maximum – 338 nautical miles (650km; 390 miles).
……….Operational – 167 nautical miles (320 km; 192 miles).

Service Life: 1200 Flight Hours or Eight Calendar Years









Number Procured: 4
……………………..Two (Z2897, Z2898) in May 86
……………………..Two (Z3075, Z3076) in Feb 89

Units Equipped: 1
………………….. 126 Helicopter Flight “Feather Weights”

Brief History:

The Mi-26 was procured to meet the Heavy Lift requirements of the IAF. A requirement of six helicopters was projected and the first two Helicopters were procured at a cost of Rs 18 Cr each in May 1986. No. 126 Helicopter Flight was raised the same month to operate the type. The Flight has a Unit Establishment of 18 Officers, 142 airmen and 28 NCs(E) and four Helicopters.  The other two helicopters were procured and inducted in February 1989 at a cost of approx Rs 22.71 Cr each. Due to low utilisation, the plan to procure two more helicopters was dropped. For the total fleet of four helicopters, twelve engines were procured.

Serviceability of the Helicopter suffered in the 90s, at one point of time in 1995-96,  as many as three of the four helicopters remaining on ground.  Serviceability gradually fell in the mid 90s from a high of 61% down to 40%.  The helicopters also remained underutilized. Against a projected utilization rate of 50 hours per month per helicopter, the average utilization hovered around 11 to 22 hours per month.

The first two Helicopters procured in 1986 were due for an overhaul in 1990. The two helicopters were ferried to Russia for overhaul in June 1991 and were returned in August 1993.

The fourth Helicopter came up for overhaul in October 1996 and was given an extension of an year after maintenance by the Base Repair Depot. However the helicopter suffered some damage after one of the undercarriage struts failed in August 1997.  The damaged helicopter was subsequently overhauled by the manufacturer in January 2003 at a cost of Rs 16.8 Crores.

During the Kargil Operations, two Mi-26s logged about 25 hours airlifting heavy equipment and guns to the Kargil area.

In July 2005, a Helicopter of the unit landing at Rampur in Himachal Pradesh was damaged after the rotor got entangled in high tension electrical cables. The aircraft was being used in helilifting heavy road building equipment in the area.

One Mi-26 (Z3076) was written off after it crashed at Jammu airport on 14 Dec 2010. It was involved in the heavy lift of tunneling equipment for the Northern Railways. The crew escaped with injuries. This was the first and till date the only major airframe loss for the Mi-26 in nearly 25 years of service.

The Mi-26s have been utilised in the sky-crane role over the years. 

– Feb 89, MI-26 helicopter undertook the only of its kind underslung operation taking Pontoon bridge form Ludhiana to Sirhind canal.
– Early 1999, a crashed MiG-21 was airlifted by the Unit to Chandigarh.
– 21 Nov 2001, the Mi-8 which crashed in the Rann of Kutch was helilifted by the Mi-26s to Bhuj.
– 2002, a MiG-21 Bison which crashed in the fields near Ambala was airlifted by the Unit to Ambala Air Force Station.
– In Jul 2002 the Mi-26 recovered the first civilian aircraft (Beechcraft), which had met with an accident at Kangra airfield. Another first was achieved as the unit flew the longest ever underslung flight (3:15 hrs).
– 22 Feb 2006 – An Mi-26 flown by the CO, Wg Cdr Sushil Ghera, airlifted an Mi-17 that forcelanded in a river bed a few days earlier to Chandigarh Air Force Station.
-Sept 2007 – Mi-17 1V airlifted from Bandipore to Awantipura
-In 2010, the helicopter was actively used to lift heavy equipment for the Katra-Quazigand Railway project providing rail connectivity to the Srinagar Valley.


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