Back Mil Mi-58
project

Mil Mi-58

TYPE: Twin-turbine passenger helicopter.

PROGRAMME: Announced at 1995 Paris Air Show; based on Mi-28 gunship; planned certification to Russian and FAR Pt 29 requirements. No further progress reported.

DESIGN FEATURES: Conventional pod and boom configuration; five-blade main rotor, two independent 'scissors'-type tail rotors and dynamic system similar to those of Mi-28.

LANDING GEAR: Non-retractable tricycle type; single wheel on each main unit, carried on long sponson on each side of fuselage; twin nosewheels.

POWER PLANT: Two Klimov TV3-117VMA-SB3 turboshafts, each with contingency rating of 2,088kW.

ACCOMMODATION: Basic version for 20 passengers, with four rearward-facing seats at front of cabin, 12 seats three-abreast with aisle and four seats at rear. Door on each side of flight deck; main cabin door at front on port side; emergency exit each side over sponson. VIP version projected. No other data available.

Jane's Helicopter Markets and Systems

Mil Mi-58


Fatal error: Uncaught mysqli_sql_exception: Connection timed out in /data03/virt15346/domeenid/www.aviastar.org/htdocs/helicopters_eng/mi-58.php:66 Stack trace: #0 /data03/virt15346/domeenid/www.aviastar.org/htdocs/helicopters_eng/mi-58.php(66): mysqli_connect('mysql5.zone.ee', 'd14657sa18989', Object(SensitiveParameterValue)) #1 {main} thrown in /data03/virt15346/domeenid/www.aviastar.org/htdocs/helicopters_eng/mi-58.php on line 66