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AMD Alarus
Role Personal use & Trainer aircraft
Manufacturer Aircraft Manufacturing and Development
Designed by Chris Heintz, Zenair, Ltd.
Introduced 1995
Primary user Iraqi Air Force
Produced Eastman, Georgia
Unit cost $139,000[1]
Center panel and radio stack

The AMD Alarus CH2000 is a two-seat, fixed tricycle gear general aviation airplane, used primarily for flight training. It is manufactured by Aircraft Manufacturing and Design Co. in Eastman, Georgia. It is a low-wing aircraft, with one door located above each wing, respectively.[2] It can be considered a competitor to similar aircraft used for flight training, such as the Diamond DA20.

The Alarus features Garmin avionics and a 46-inch wide cabin.[2]

Contents

[edit] Variants

Currently the Alarus is offered in two variants: the AMD Alarus CH2000 general aviation aircraft[2] and the SAMA CH2000 Military Tactical Surveillance Aircraft (MTSA).[3]

[edit] SAMA CH2000

The SAMA CH2000 is a military surveillance variant of the Alarus. It is equipped with forward looking infrared – a multi sensor imager offering high performance, precision and high level imaging..[3]

The aircraft is also equipped with state-of-the-art communications systems for secure air-to-air and air-to-ground communications and is equipped for day and night missions. The aircraft is manufactured in Amman, Jordan and Baghdad, Iraq.[3][4]

The first SAMA CH2000s were delivered to the Iraqi Air Force 70th Squadron, based in in Basrah on 29 October 2004. The Iraqi Air Force acquired between 8 and 16 aircraft at a cost of USD$5.8M with deliveries completed by the end of March 2005.[3][4]

[edit] Operators

The Alarus can currently be found operating at some flight schools in the USA. Operating costs are generally low, and the aircraft is easy to maintain, allowing flight schools to keep costs low for students.[2]

In February 2008 there were 113 CH2000 Alarus registered in the USA[5] and four in Canada.[6]

The only confirmed military user of the CH2000 is the Iraqi Air Force, currently operating 16 aircraft. Aircraft are operated by the Iraqi 70th Reconnaissance squadron.

[edit] Specifications

Data from AMD Website [7]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 23 ft 0 in (7.01 m)
  • Wingspan: 28 ft 10 in (8.79 m)
  • Height: 6 ft 10 in (2.08 m)
  • Wing area: 137 sq ft (12.7 m2)
  • Empty weight: 1,085 lb (492 kg) basic VFR-equipped
  • Max takeoff weight: 1,692 lb (767 kg)
  • Fuel capacity: 28 US Gallons (106 litres)
  • Powerplant: 1 × Lycoming O-235-N2C four cylinder, horizontally opposed, four stroke aircraft engine, 116 hp (87 kW)
  • Propellers: 2-bladed Sensenich fixed pitch, 6 ft 0 in (1.83 m) diameter

Performance

  • Cruise speed: 99 kn (114 mph; 183 km/h)
  • Stall speed: 48 kn (55 mph; 89 km/h)
  • Never exceed speed: 143 kn (165 mph; 265 km/h)
  • Range: 486 nmi (559 mi; 900 km)
  • G limits: +4.4/-2.2 (utility category 1,606 lbs) +3.8/-1.9 (normal category 1,692 lbs)
  • Rate of climb: 750 ft/min (3.8 m/s)
  • Wing loading: 12.3 lb/ft² (60.29 kg/m²)
  • Power/mass: 14.6 lb/hp (0.11 kW/kg)

Avionics

  • Garmin GNS 430 (COM, GPS, VOR, GS)
  • Garmin GI-106A VOR with GS slope
  • Garmin 340 audio panel
  • Garmin GTX 327 transponder/encoder
  • Bendix/king KX 155 NAV COM
  • Bendix/king KI 209 VOR with GS

[edit] References/ External Links




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