Basic Information

Category Helicopter Type Transport
Year Commissioned 1982 Year Decommissioned 0
Agility 1 Damage Points (DP) 10
Empty Weight 15071 kg Max Weight 33300 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 16000 kg Crew 3 people

Aircraft Capabilities

HIFR Capable Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Probe Refueling

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APN-217 Radar, Navigation 0.20 - 35.00 nm 2 sec Early 1980s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APN-217 SB1, SB2, SMF1, PB1, PB2, PMF2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 2.97 nm 7.59 nm 2.97 nm
Visual Classification Range 1.39 nm 3.52 nm 2.31 nm
Infrared Detection Range 2.97 nm 9.13 nm 13.09 nm
Infrared Classification Range 1.64 nm 4.14 nm 1.64 nm
Radar, A-D Band (30-2000 MHz) 6.6 dBsm (4.57 m²) 8.9 dBsm (7.76 m²) 6.6 dBsm (4.57 m²)
Radar, E-M Band (2-100 GHz) 6.6 dBsm (4.57 m²) 8.9 dBsm (7.76 m²) 6.6 dBsm (4.57 m²)

Default Configuration

Model Comments
12.7mm/72 GAU-15 MG [2400 rnds] -
12.7mm/72 GAU-15 MG [2400 rnds] -

Datalink

Type Model Range Channels
Radio AN/ARC-94 HF Communications 100 nm 0
Radio AN/ARC-114A VHF Communications 100 nm 0
Radio AN/ARC-159 UHF Communications 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
3x T64-GE-416A Helo Turboshaft 3 4380 - 0.47 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 3015