The Mi-2AM-1 is modernized version accordingly to the international requirements and standards. In particular Mi-2AM-1 has new digital flight-navigation system, radio and electrical equipments, renovated hull with use of polymer composite materials.
Helicopter has latest digital equipment including all control sensors for engine and gearboxes operations. Lightweight fuselage design allowed to increase the capacity of the helicopter and improved flight characteristics.
Мi-2АМ-1 has completely new logbook with the true year of manufacture.
Total Time Since New - accordingly to the made flight hours;
Time Since Overhaul - 0 hours.
Logbooks for engines is original with true year of manufacture.
Total Time Since New - accordingly to the data in the logbook;
Time Since Overhaul - accordingly to the data in the logbook.
Logbooks for main assemblies and units are original for true years of manufacture.
The fulfilled overhaul is mentioned in the logbook of engine, assemblies and units.
Commencement year of operation of the helicopter – 2019.
Year of manufacture of electrical equipment and avionics - 2019.
Production year of the pilot seats - 2019.
NEW DESIGN OF THE AVIONICS AND RADIO OF EQUIPMENT MI-2AM-1 INCLUDES:
- flight-navigation complex;
- GPS satellite navigation system;
- instrumental approach system;
- radio station VHF NAV / VOR / COM - audio panel
- radio altimeter
- attitude indicator
- magnetic compass
PILOT SEATS SAB-1 FROM COMPOSITE MATERIAL WITH FOUR-POINT TETHERED INERTIAL SYSTEM.
More ergonomic design, including Glass Cockpit, more safety and comfortability.
The new aerodynamic shape of nose and replacing of glass cockpit windows with use of modern composite materials.
Also, have been redesigned:
- front body element;
- section shapes of doorways;
- two spars;
- cockpit doors at the right and left.
Manufacturer Country – Ukraine Engines – GTD-350 х 2 units;
Take off power – 2 х 410 HP;
Fuel consumption – 260 l/h;
Cruising Speed Fuel Consumption – 240-260 l/h;
Practical altitude – 4000 m;
Static altitude – 1620 m;
Maximal speed – 220 кm/h;
Cruising speed – 180 кm/h;
Number of crew and passengers – 8 people;
Payload characteristics: Load in the cabin – 1000 kg;
Load on external suspension – 1000 kg;
Maximal take off weight – 3 550 kg; Volume of main fuel tank – 600 liters;
The volume of outboard fuel tanks - 2 x 240 liters;
The maximum flight distance is 900 km (with installed outboard fuel tanks).
The blades of the main and tail rotor are new and made of a composite material. Protection against icing and abrasive wear is implemented by use of special polished forged metal at the edge and coating the surface of the blade with wear-resistant and low adhesion paint cover.