Preowned Helicopters

 

Wide range of preowned helicopters in excellent shape can meet the demands of cost aware clients.

MD500

MD500

Specific models for sale:

  • UH-60 Blackhawk
  • MD 500E
  • MD 520
  • MD 600N
  • MD 902
  • Bell 206
  • Bell 412
  • Bell UH-1
  • Bell Huey II
  • Bell OH-58
  • Mil Mi-2
  • Mil Mi-8
  • Mil Mi-17
  • Mil Mi-24

UH-60 Blackhawk

  • Four-bladed, twin-engine, medium-lift utility helicopter
  • Used primarily for the transport of people and materials, troop insertion, and armed escorts, MEDEVAC, SAR operations
  • Operated in 23 countries
  • Produced more then 4.000 pcs

    Sikorsky UH-60 Blackhawk

  • Spare parts available
  • Optional weapons installation kit

Length: 64 ft 10 in (19.76 m)

Rotor diameter: 53 ft 8 in (16.36 m)

Height: 16 ft 10 in (5.13 m)

Disc area: 2,260 ft² (210 m²)

Empty weight: 10,624 lb (4,819 kg)

Max. takeoff weight: 23,500 lb (10,660 kg)

Powerplant: 2 × GE T700-GE-701C turboshaft, 1,890 hp (1,410 kW) each

Maximum speed: 159 kn (183 mph; 294 km/h)

Cruise speed: 150 kn (170 mph; 280 km/h)

Service Ceiling: 19,000 ft (5,790 m)

 

MD 500E

  • Based on mission proved military design

    MD500

  • Greater Visibility
  • Highest speed, manoeuvrability, payload and productivity in its class
  • Five-bladed main rotor and the 450-shp Rolls-Royce 250-C20R turbine engine
  • Military kit available

Length: 30.81 ft (9.4 m)

Rotor diameter: 26.4 ft (8.1 m)

Height: 8.4 ft (2.6 m)

Disc area: 586.8 ft² (54.5 m²)

Empty weight: 1,481 lb (672 kg)

Max. takeoff weight: 3,000 lb (1,361 kg)

Powerplant: 1 × Allison 250-C20B Turboshaft, 420 hp (313 kW)

Maximum speed: 152 knots (175 mph, 282 km/h)

Cruise speed: 135 kn (155 mph, 250 km/h)

Range: 267 mi (429 km)

Service Ceiling: 16,000 ft (4,877 m)

Rate of Climb: 1,770 ft/min (9 m/s)

MD 520

  • Fast, agile, lightweight, turbine powered, all purpose helicopter
  • NOTAR anti-torque system

    MD 600

  • One of the safest, quietest helicopters in the world
  • MD 520N features the improved 450-shaft-horse-power Rolls-Royce 250-C20R for increased performance

Empty weight: 719 kg

Maximum Gross Weight: 1502 kg

Useful Load: 800 kg

Powerplant: RR250-C20R

Maximum speed: 245 kph

Range: 389 km

Service Ceiling: 6097 m

MD600N

  • Eight-place, light, single-turbine engine helicopter
  • Provides high performance and increased capacity
  • NOTAR anti-torque system
  • Dramatically low operating costs

Length: 35 ft 5 in (11.79 m)

Rotor diameter: 27 ft 6 in (8.38 m)

Height: 8 ft 9 in (2.65 m)

Disc area: 594.0 sq ft (55.2 m²)

Empty weight: 2,100 lb (952 kg)

Max. takeoff weight: 4,100 lb (1,860 kg)

Powerplant: 1 × Allison Model 250-C47 Turboshaft, 600 hp (447 kW)

Maximum speed: 152 knots (175 mph, 282 km/h)

Cruise speed: 135 knots (155 mph, 250 km/h)

Range: 357 nmi (411 mi, 661 km)

Service ceiling: 18,700 ft (5700 m)

MD902 Explorer

  • Affordable, Dependable, High-Performance

    MD 902

  • Multipurpose light twin-engine -Suited for rapid role change from an Offshore/Onshore six-place passenger transport to Emergency Medical Services or Law Enforcement missions
  • Certified by FAA and JAA for day/night VFR and single pilot IFR with full Category A design standards to JAR-OPS 3 performance Class I.
  • NOTAR system – lowest noise & vibration levels, excellent for surveillance and transport
  • Six-place cabin – the largest in the light twin class; Large baggage compartment
  • Heavy-duty cargo hook permits 1360-KG external load operations
  • Standard passenger transport
  • Emergency medical service
  • Law enforcement
  •  VIP passenger transport

Length: 32 ft 4 in (9.85 m)

Rotor diameter: 33 ft 10 in (10.31 m)

Height: 12 ft 0 in (3.66 m)

Disc area: 899.0 sq ft (83.52 m2)

Empty weight: 3,375 lb (1,531)

Max. takeoff weight: 6,250 lb (2,835 kg) (internal load), 6,900 lb (3,129 kg) (slung load)

Powerplant: 2 × Pratt & Whitney Canada PW206E turboshaft, 550 shp (410 kW) (continuous) each

Cruise speed: 134 knots (154 mph, 248 km/h) at sea level (max. cruise)

Range: 293 nmi (337 mi, 542 km) at 5,000 ft (1,500 m)

Service ceiling: 17,500 ft (5,335 m)

Bell 206

  • High-inertia two-bladed rotor system

    Bell 206

  • Patented suspension system that delivers a smooth ride

Length: 39 ft 8 in (12.11 m)

Rotor diameter: 33 ft 4 in (10.16 m)

Height: 9 ft 4 in (2.83 m)

Disc area: 872 ft² (81.1 m²)

Empty weight: 2,331 lb (1,057 kg)

Max. takeoff weight: 3,200 lb (1,451 kg)

Powerplant: 1 × Allison 250-C30P turboshaft, 420 shp; derated to 317 shp due to drivetrain limitations (310 kW)

Never exceed speed: 130 knots (241 km/h, 150 mph)

Maximum speed: 120 knots (222 km/h, 138 mph)

Range: 374 nmi (430 mi, 693 km)

Service ceiling: 13,500 ft (4,115 m)

Rate of climb: 1,350 ft/min (6.9 m/s)

Disc loading: 4 lb/ft² (177 N/m²)

Power/mass: 0.26 hp/lb (430 W/kg)

Bell 412

  • Daily workhorse that reliably performs in some of the most extreme climates around the world
  • Expansive cabin provides multi-mission flexibility

Length: 56 ft 1 in (17.1 m)

Bell 412

Rotor diameter: 46 ft (14.0 m)

Height: 15 ft (4.6 m)

Disc area: 1,662 ft² (154.4 m²)

Empty weight: 6,789 lb (3,079 kg)

Max. takeoff weight: 11,900 lb (5,397 kg)

Powerplant: 2 × Pratt & Whitney Canada PT6T-3D or PT6T-3DF Twin-Pac turboshafts, 900 shp (671 kW) each

Maximum speed: 140 knots (161 mph, 259 km/h)

Cruise speed: 122 knots (140 mph, 226 km/h)

Range: 609 mi (up to 980km)

Service ceiling: 20,000 ft (6,096 m)

Bell UH-1

  • Military helicopter powered by a single turbo shaft engine, with two-bladed main and tail rotors
  • Most versatile helicopter

    Bell UH-1

  • Introduced during Vietnam war
  • Spare parts available
  • Optional weapons installation kit
  • Still in active service

Length: 57ft

Height: 14ft

Rotor Diameter: 48.00ft

Empty Weight: 5,215lbs

Gross Weight: 9,040lbs

Maximum Speed: 135mph

Cruise Speed: 125mph

Power Plant: Lycoming T53-L-13 engine

Range: 315miles

Huey II

Bell Huey II

  • Only OEM approved and supported Bell UH-1H performance upgrade available
  • Combines commercial Bell 212 dynamic components with the reliable Honeywell T53-L-703 engine

Empty Weight: 2,552 kg

Gross Weight: 4,763 kg

Maximum Cruise Speed: 196 km/h

Cruise Speed: 125mph

Range: 455 km

Bell OH-58

  • single-engine, single-rotor, military helicoptersused for observation, utility and direct fire support
  • primarily operated in an armed reconnaissance role in support of ground troops

    Bell OH-58

Length32 ft 2 in (9.80 m)

Height9 ft 7 in (2.92 m)

Rotor diameter: 35 ft 4 in (10.77 m)

Empty weight: 3,829 lb (1,737 kg)

Max takeoff weight: 3,000 lb (1,360 kg)

Maximum speed: 120 knots (222 km/h, 138 mph)

Cruise speed: 102 knots (188 km/h, 117 mph)

Range: 299 mi (481 km, 260 nmi)

Powerplant1 × Allison T63-A-700 turboshaft, 317 shp (236 kW)

Service ceiling: 19,000 ft (5,800 m)

Mil Mi-2

  • One of the most widely used light helicopters

    Mil Mi-2 By Radomil talk (Own work) GFDL or CC-BY-SA-3.0, via Wikimedia Commons

  • Twin-engined light utility helicopter
  • Could also provide close air supportwhen armed with 57 mm rockets and a 23 mm cannon

Capacity:8 passengers or 700 kg (1,543 lb) internal, 800 kg (1,764 lb) external cargo

Length:11.40 m (37 ft 4¾ in)

Rotor diameter:14.50 m (47 ft 6⅞ in)

Height:3.75 m (12 ft 3½ in)

Disc area:165.13 m² (1,777.44 ft²)

Empty weight:2,372 kg (5,218 lb)

Max takeoff weight:3,700 kg (8,157 lb)

Max speed:200 km/h (108 knots, 124 mph)

Range:440 km (237 nmi, 273 mi)

Service ceiling:4,000 m (13,125 ft)

Mil Mi-8

  • Medium twin-turbine helicopter

    Mil Mi-8

  • Most common role as a transport helicopter
  • Also used as an airborne command post, armed gunship, and reconnaissance platform
  • As of 2015, it is the third most common operational military aircraft in the world

Length:18.17 m (59 ft 7 in)

Rotor diameter:21.29 m (69 ft 10 in)

Height:5.65 m (18 ft 6 in)

Disc area:356 m² (3,832 ft²)

Empty weight:7,260 kg (16,007 lb)

Max takeoff weight:12,000 kg (26,455 lb)

Powerplant:2 × Klimov TV3-117Mtturboshafts, 1,454 kW (1,950 shp) each

Max speed:260 km/h (140 kt)

Range:450 km (280 mi)

Service ceiling:4,500 m (14,765 ft)

Mil Mi-17

Mil Mi-17

  • Extreme weather condition
  • Heavy load
  • High altitude
  • No ITAR restriction

Length: 18.465 m (60 ft 7 in)

Rotor diameter: 21.25 m (69 ft 10½ in)

Height: 4.76 m (15 ft 7¼ in)

Empty weight: 7,489 kg (16,510 lb)

Max takeoff weight: 13,000 kg (28,660 lb)

Powerplant: 2 × Klimov TV3-117VMturboshafts, 1,633 kW (2,190 shp) each

Max speed: 250 km/h (135 knots, 155 mph)

Range: 465 km (251 nmi, 289 mi)

Service ceiling: 6,000 m (19,690 ft)

Mil Mi-24

  • multi-role large military helicopter gunship, attack helicopter and low-capacity troop transport with room for eight passengers
  • combination of reduced size and increased power gives this aircraft improved manoeuvrability and performance

Length: 17.5 m (57 ft 4 in)

Mil Mi-24

Rotor diameter: 17.3 m (56 ft 7 in)

Wingspan: 6.5 m (21 ft 3 in)

Height: 6.5 m (21 ft 3 in)

Empty weight: 8,500 kg (18,740 lb)

Max takeoff weight: 12,000 kg (26,500 lb)

Powerplant: 2 × Isotov TV3-117turbines, 1,600 kW (2,200 hp) each

Max speed: 335 km/h (208 mph)

Range: 450 km (280 miles)

Service ceiling: 4,900 m (16076 ft)